- temperatureCoupled temperature
C++ Type:std::vector<VariableName>
Unit:(no unit assumed)
Controllable:No
Description:Coupled temperature
ZryThermal
Computes the thermal conductivity and the specific heat, under constant pressure, for zirconium alloy cladding based on either the MATPRO or IAEA models.
Description
The ZryThermal
material model computes the thermal conductivity and specific heat capacity for zirconium alloy cladding. Two different sets of thermal properties models are available: one based on the MATPRO relations (Allison et al., 1993) and a second set based on IAEA relations (IAEA, 2006). The MATPRO models are the default behavior in BISON.
Thermal Conductivity
Both the MATPRO model and the IAEA model for thermal conductivity used experimental data from Zircaloy-2 and Zircaloy-4.
MATPRO Model
The correlation for thermal conductivity of zirconium alloy (Allison et al., 1993) is given by: k (W/m-K)=7.511+2.088×10−2T−1.450×10−5T2+7.668×10−9T3 where T the temperature in Kelvin. This correlation is valid up to 2098 K.
IAEA Model
The IAEA thermal conductivity of zirconium alloy is (IAEA, 2006): k (W/m-K)=12.767−5.4348×10−4T+8.9818×10−6T2 where T is the temperature in K. The IAEA model is valid for temperatures between 300K and 1800K.
Specific Heat Capacity
The MATPRO and the IAEA models for specific heat capacity for zirconium alloy are both based on experimental data for Zircaloy-2 and applied to Zircaloy-4; no information on the specific heat capacity of Zircaloy-4 is available in the open literature.
MATPRO Specific Heat Capacity Model
The specific heat capacity for Zircaloy alloys is based upon the tabulated data show in Table 1. Linear interpolation is used between the tabulated values.
Table 1: Temperature dependent specific heat capacity of Zircaloy (Allison et al., 1993)
Temperature (K) | Specific Heat Capacity (J/kg-K) | Temperature (K) | Specific Heat Capacity (J/kg-K) |
---|---|---|---|
300.0 | 281 | 1153.0 | 719 |
400.0 | 302 | 1173.0 | 816 |
640.0 | 331 | 1193.0 | 770 |
1090.0 | 375 | 1213.0 | 619 |
1093.0 | 502 | 1233.0 | 469 |
1113.0 | 590 | 1248.0 | 356 |
1133.0 | 615 |
IAEA Specific Heat Capacity Model
The IAEA model (IAEA, 2006) for specific heat capacity of zirconium alloy is a piece wise function that explicitly accounts for mixed α and β phases as the zirconium alloy undergoes a phase transition with temperature. The piecewise function is constructed to weight the specific heat capacity calculation based on whether the α or β phase is more previlant. cP=⎩⎨⎧255.66+0.1024T255.66+0.1024T+1058.4exp(719.61−[T−1213.8]2)597.1−0.4088T+1.565×10−4T2+1058.4exp(719.61−[T−1213.8]2)597.1−0.4088T+1.565×10−4T2 for 273K<T<1100K for 1100<T<1214K for 1214<T<1320K for 1320<T<2000K(1) where T is the temperature in K, and the calculated specific heat capacity Cp has units of (J/kg-K). The IAEA heat capacity model is valid for temperatures between 273K and 2000K.
The ThermalZry model for heat capacity from the IAEA report, Eq. (1), includes two negative signs in the exponential terms, used to calculate the heat capacity for the mixed α and β phases between 1100K and 1320K, which do not appear in the cited literature. This correction to the heat capacity equation is necessary to capture the Zircaloy-2 heat capacity data which demonstrates a local peak near 1200K. Without this correction the equation becomes asymptotic at 1200K.
Example Input Syntax
[Materials]
[thermal_clad]
type = ZryThermal
temperature = T
zry_thermal_properties_model = IAEA
[]
[]
Input Parameters
- base_nameOptional parameter that allows the user to define multiple material systems on the same block, e.g. for multiple phases.
C++ Type:std::string
Controllable:No
Description:Optional parameter that allows the user to define multiple material systems on the same block, e.g. for multiple phases.
- blockThe list of blocks (ids or names) that this object will be applied
C++ Type:std::vector<SubdomainName>
Controllable:No
Description:The list of blocks (ids or names) that this object will be applied
- boundaryThe list of boundaries (ids or names) from the mesh where this object applies
C++ Type:std::vector<BoundaryName>
Controllable:No
Description:The list of boundaries (ids or names) from the mesh where this object applies
- computeTrueWhen false, MOOSE will not call compute methods on this material. The user must call computeProperties() after retrieving the MaterialBase via MaterialBasePropertyInterface::getMaterialBase(). Non-computed MaterialBases are not sorted for dependencies.
Default:True
C++ Type:bool
Controllable:No
Description:When false, MOOSE will not call compute methods on this material. The user must call computeProperties() after retrieving the MaterialBase via MaterialBasePropertyInterface::getMaterialBase(). Non-computed MaterialBases are not sorted for dependencies.
- constant_onNONEWhen ELEMENT, MOOSE will only call computeQpProperties() for the 0th quadrature point, and then copy that value to the other qps.When SUBDOMAIN, MOOSE will only call computeQpProperties() for the 0th quadrature point, and then copy that value to the other qps. Evaluations on element qps will be skipped
Default:NONE
C++ Type:MooseEnum
Options:NONE, ELEMENT, SUBDOMAIN
Controllable:No
Description:When ELEMENT, MOOSE will only call computeQpProperties() for the 0th quadrature point, and then copy that value to the other qps.When SUBDOMAIN, MOOSE will only call computeQpProperties() for the 0th quadrature point, and then copy that value to the other qps. Evaluations on element qps will be skipped
- declare_suffixAn optional suffix parameter that can be appended to any declared properties. The suffix will be prepended with a '_' character.
C++ Type:MaterialPropertyName
Unit:(no unit assumed)
Controllable:No
Description:An optional suffix parameter that can be appended to any declared properties. The suffix will be prepended with a '_' character.
- zry_thermal_properties_modelMATPROReference source for the set of thermal property calculations to use: MATPRO IAEA
Default:MATPRO
C++ Type:MooseEnum
Options:MATPRO, IAEA
Controllable:No
Description:Reference source for the set of thermal property calculations to use: MATPRO IAEA
Optional Parameters
- control_tagsAdds user-defined labels for accessing object parameters via control logic.
C++ Type:std::vector<std::string>
Controllable:No
Description:Adds user-defined labels for accessing object parameters via control logic.
- enableTrueSet the enabled status of the MooseObject.
Default:True
C++ Type:bool
Controllable:Yes
Description:Set the enabled status of the MooseObject.
- implicitTrueDetermines whether this object is calculated using an implicit or explicit form
Default:True
C++ Type:bool
Controllable:No
Description:Determines whether this object is calculated using an implicit or explicit form
- seed0The seed for the master random number generator
Default:0
C++ Type:unsigned int
Controllable:No
Description:The seed for the master random number generator
- use_displaced_meshFalseWhether or not this object should use the displaced mesh for computation. Note that in the case this is true but no displacements are provided in the Mesh block the undisplaced mesh will still be used.
Default:False
C++ Type:bool
Controllable:No
Description:Whether or not this object should use the displaced mesh for computation. Note that in the case this is true but no displacements are provided in the Mesh block the undisplaced mesh will still be used.
Advanced Parameters
- output_propertiesList of material properties, from this material, to output (outputs must also be defined to an output type)
C++ Type:std::vector<std::string>
Controllable:No
Description:List of material properties, from this material, to output (outputs must also be defined to an output type)
- outputsnone Vector of output names where you would like to restrict the output of variables(s) associated with this object
Default:none
C++ Type:std::vector<OutputName>
Controllable:No
Description:Vector of output names where you would like to restrict the output of variables(s) associated with this object
Outputs Parameters
- prop_getter_suffixAn optional suffix parameter that can be appended to any attempt to retrieve/get material properties. The suffix will be prepended with a '_' character.
C++ Type:MaterialPropertyName
Unit:(no unit assumed)
Controllable:No
Description:An optional suffix parameter that can be appended to any attempt to retrieve/get material properties. The suffix will be prepended with a '_' character.
- use_interpolated_stateFalseFor the old and older state use projected material properties interpolated at the quadrature points. To set up projection use the ProjectedStatefulMaterialStorageAction.
Default:False
C++ Type:bool
Controllable:No
Description:For the old and older state use projected material properties interpolated at the quadrature points. To set up projection use the ProjectedStatefulMaterialStorageAction.
Material Property Retrieval Parameters
- specific_heat_scale_factor1The scaling factor on the specific heat.
Default:1
C++ Type:double
Unit:(no unit assumed)
Controllable:No
Description:The scaling factor on the specific heat.
- thermal_conductivity_scale_factor1The scaling factor on the thermal conductivity.
Default:1
C++ Type:double
Unit:(no unit assumed)
Controllable:No
Description:The scaling factor on the thermal conductivity.
Advanced: Scaling Factors Parameters
Input Files
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-26/puzry-26_aniso.i)
- (assessment/LWR/validation/RIA_CABRI_REP_Na/analysis/REP_Na_2/REP_Na_2.i)
- (assessment/LWR/validation/RIA_NSRR_FK/analysis/FK2/FK02.i)
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-30/puzry-30.i)
- (test/tests/thermalZry/thermal_test_IAEA.i)
- (assessment/LWR/validation/Super_Ramp/analysis/PK62/PK62_weighted_gap_VCP.i)
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-19/puzry-19.i)
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-23/puzry-23.i)
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-03/puzry-03.i)
- (assessment/LWR/validation/LOCA_ANL_cladding_burst_tests/analysis/OCL11/OCL11_aniso.i)
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-31/puzry-31_aniso.i)
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-07/puzry-07.i)
- (assessment/LWR/validation/LOCA_REBEKA_cladding_burst_tests/analysis/rebeka_2d_01MPa/rebeka_singlerod_2d_01MPa_aniso.i)
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-31/puzry-31.i)
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-25/puzry-25.i)
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-16/puzry-16.i)
- (assessment/LWR/validation/LOCA_REBEKA_cladding_burst_tests/analysis/rebeka_2d_14MPa/rebeka_singlerod_2d_14MPa_aniso.i)
- (assessment/LWR/validation/LOCA_IFA_650/analysis/IFA_650_9/IFA_650_9_part1.i)
- (assessment/LWR/validation/LOCA_IFA_650/analysis/IFA_650_9/IFA_650_9_part2.i)
- (assessment/LWR/validation/LOCA_ORNL_cladding_burst_tests/analysis/Zr4_1/ornl_zr4_1_ad_hill.i)
- (assessment/LWR/validation/LOCA_Studsvik/analysis/rod_191/Studsvik_191_part1.i)
- (assessment/LWR/validation/LOCA_REBEKA_cladding_burst_tests/analysis/rebeka_2d_08MPa/rebeka_singlerod_2d_08MPa_aniso.i)
- (test/tests/zry_oxidation_cladding/alt_oxidation_cladding_zry.i)
- (assessment/LWR/validation/LOCA_Studsvik/analysis/rod_191/Studsvik_191_part1_1p5d_fr_frd.i)
- (assessment/LWR/validation/LOCA_ANL_cladding_burst_tests/analysis/OCL11/OCL11.i)
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-27/puzry-27.i)
- (assessment/LWR/validation/LOCA_Hardy_cladding_test/analysis/0pt3MPa/100C_sec/100C_sec_Hardy_Tube_Test_0pt3MPa.i)
- (assessment/LWR/validation/RIA_CABRI_REP_Na4/analysis/REP_Na_4/REP_Na_4.i)
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-19/puzry-19_aniso.i)
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-30/puzry-30_aniso.i)
- (test/tests/xfem/level_set_xfem_oxidation/ls_xfem_zry_oxidation_default.i)
- (assessment/LWR/validation/LOCA_ORNL_cladding_burst_tests/analysis/Zr4_1/ornl_zr4_1_ad_hill_aniso.i)
- (test/tests/phase_transition_zircaloy/test_zrphase.i)
- (assessment/LWR/validation/LOCA_REBEKA_cladding_burst_tests/analysis/rebeka_2d_10MPa/rebeka_singlerod_2d_10MPa_aniso.i)
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-06/puzry-06.i)
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-29/puzry-29_aniso.i)
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-03/puzry-03_aniso.i)
- (assessment/LWR/validation/RIA_CABRI_REP_Na/analysis/REP_Na_10/REP_Na_10_RIA.i)
- (test/tests/zry_oxidation_cladding/zryoxidation.i)
- (assessment/LWR/validation/LOCA_Hardy_cladding_test/analysis/5pt5MPa/25C_sec/25C_sec_Hardy_Tube_Test_5pt5MPa.i)
- (test/tests/standard_lwr_outputs_action/clad_only.i)
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-15/puzry-15.i)
- (assessment/LWR/validation/RIA_NSRR_FK/analysis/FK5/FK05.i)
- (assessment/LWR/validation/LOCA_ANL_cladding_burst_tests/analysis/OCL11/OCL11_ad.i)
- (assessment/LWR/validation/LOCA_REBEKA_cladding_burst_tests/analysis/rebeka_2d_12MPa/rebeka_singlerod_2d_12MPa_aniso.i)
- (assessment/LWR/validation/LOCA_REBEKA_cladding_burst_tests/analysis/rebeka_2d_10MPa/rebeka_singlerod_2d_10MPa_1pt5_aniso.i)
- (assessment/LWR/validation/LOCA_IFA_650/analysis/IFA_650_4/IFA_650_4_part2.i)
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-26/puzry-26.i)
- (assessment/LWR/validation/RIA_CABRI_REP_Na/analysis/REP_Na_2/REP_Na_2_1pt5.i)
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-02/puzry-02_aniso.i)
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-16/puzry-16_aniso.i)
- (test/tests/thermalZry/thermal_zry_negative_temperature_exception.i)
- (assessment/LWR/validation/LOCA_REBEKA_cladding_burst_tests/analysis/rebeka_2d_10MPa/rebeka_singlerod_2d_10MPa_aniso_hunt.i)
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-13/puzry-13_aniso.i)
- (assessment/LWR/validation/LOCA_REBEKA_cladding_burst_tests/analysis/rebeka_2d_06MPa/rebeka_singlerod_2d_06MPa.i)
- (assessment/LWR/validation/Super_Ramp/analysis/Super_Ramp_Base.i)
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-24/puzry-24.i)
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-21/puzry-21_aniso.i)
- (examples/accident_tolerant_fuel/uo2_coated_zircaloy/uo2_coated_zircaloy.i)
- (assessment/LWR/validation/LOCA_ANL_cladding_burst_tests/analysis/OCL5_8/OCL5_8_ad.i)
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-14/puzry-14.i)
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-04/puzry-04.i)
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-28/puzry-28.i)
- (test/tests/zry_oxidation_cladding/oxide_coolant_couple.i)
- (assessment/LWR/validation/RIA_CABRI_REP_Na4/analysis/REP_Na_4/RIA/REP_Na_4_RIA.i)
- (assessment/LWR/validation/LOCA_ORNL_cladding_burst_tests/analysis/Zr2_1/ornl_zr2_1_aniso.i)
- (assessment/LWR/validation/LOCA_REBEKA_cladding_burst_tests/analysis/rebeka_2d_01MPa/rebeka_singlerod_2d_01MPa.i)
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-05/puzry-05_aniso.i)
- (assessment/LWR/validation/LOCA_ANL_cladding_burst_tests/analysis/OCL5_8/OCL5_8_aniso.i)
- (assessment/LWR/validation/LOCA_Studsvik/analysis/rod_191/Studsvik_191_part2_1p5d_fr_frd.i)
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-23/puzry-23_aniso.i)
- (examples/multiapp/pin1.i)
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-04/puzry-04_aniso.i)
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-08/puzry-08_aniso.i)
- (assessment/LWR/validation/LOCA_Hardy_cladding_test/analysis/13pt8MPa/25C_sec/25C_sec_Hardy_Tube_Test_13pt8MPa.i)
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-10/puzry-10.i)
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-12/puzry-12.i)
- (assessment/LWR/validation/RIA_NSRR_FK/analysis/FK9/FK09.i)
- (assessment/LWR/validation/LOCA_REBEKA_cladding_burst_tests/analysis/rebeka_2d_04MPa/rebeka_singlerod_2d_04MPa.i)
- (assessment/LWR/validation/LOCA_Studsvik/analysis/rod_196/Studsvik_196_part1_1p5d_fr_ffrd.i)
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-01/puzry-01.i)
- (assessment/LWR/validation/LOCA_Hardy_cladding_test/analysis/2pt8MPa/25C_sec/25C_sec_Hardy_Tube_Test_2pt8MPa.i)
- (assessment/LWR/validation/LOCA_Studsvik/analysis/rod_196/Studsvik_196_part2.i)
- (assessment/LWR/validation/LOCA_REBEKA_cladding_burst_tests/analysis/rebeka_3d_10MPa_01Kpers_90deg/rebeka_singlerod_3d_10MPa_90deg.i)
- (test/tests/thermalZry/thermal_test.i)
- (examples/accident_tolerant_fuel/u3si2_zircaloy/u3si2_zircaloy.i)
- (assessment/LWR/validation/RIA_NSRR_FK/analysis/FK3/FK03.i)
- (test/tests/zry_oxidation_cladding/oxidation_cladding_zry.i)
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-11/puzry-11.i)
- (assessment/LWR/validation/LOCA_Hardy_cladding_test/analysis/5pt5MPa/100C_sec/100C_sec_Hardy_Tube_Test_5pt5MPa.i)
- (assessment/LWR/validation/LOCA_REBEKA_cladding_burst_tests/analysis/rebeka_2d_12MPa/rebeka_singlerod_2d_12MPa.i)
- (assessment/LWR/validation/RIA_NSRR_FK/analysis/FK6/FK06.i)
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-09/puzry-09_aniso.i)
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-07/puzry-07_aniso.i)
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-17/puzry-17_aniso.i)
- (assessment/LWR/validation/LOCA_Studsvik/analysis/rod_191/Studsvik_191_part2.i)
- (assessment/LWR/validation/LOCA_IFA_650/analysis/IFA_650_2/IFA_650_2.i)
- (assessment/LWR/validation/LOCA_REBEKA_cladding_burst_tests/analysis/rebeka_2d_10MPa/rebeka_singlerod_2d_10MPa_1pt5.i)
- (assessment/LWR/validation/LOCA_ORNL_cladding_burst_tests/analysis/Zr2_2/ornl_zr2_2_aniso.i)
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-15/puzry-15_aniso.i)
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-09/puzry-09.i)
- (assessment/LWR/validation/LOCA_ORNL_cladding_burst_tests/analysis/Zr2_1/ornl_zr2_1_ad.i)
- (test/tests/standard_lwr_outputs_action/clad_nonstandard_names.i)
- (test/tests/solid_mechanics/zry_mechanics/elastic_modulus_zry.i)
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-22/puzry-22.i)
- (assessment/LWR/validation/IFA_677/analysis/IFA_677_Base.i)
- (assessment/LWR/validation/LOCA_Hardy_cladding_test/analysis/2pt1MPa/25C_sec/25C_sec_Hardy_Tube_Test_2pt1MPa.i)
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-24/puzry-24_aniso.i)
- (assessment/LWR/validation/LOCA_Hardy_cladding_test/analysis/3pt8MPa/25C_sec/25C_sec_Hardy_Tube_Test_3pt8MPa.i)
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-01/puzry-01_aniso.i)
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-27/puzry-27_aniso.i)
- (assessment/LWR/validation/LOCA_REBEKA_cladding_burst_tests/analysis/rebeka_2d_10MPa/rebeka_singlerod_2d_10MPa.i)
- (assessment/LWR/validation/LOCA_Hardy_cladding_test/analysis/base_input/Hardy_Tube_Test.i)
- (test/tests/zry_oxidation_cladding/adZryoxidation.i)
- (assessment/LWR/validation/RIA_NSRR_FK/analysis/FK3/FK03_ccm.i)
- (assessment/LWR/validation/LOCA_ORNL_cladding_burst_tests/analysis/Zr4_1/ornl_zr4_1.i)
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-18/puzry-18.i)
- (assessment/LWR/validation/LOCA_IFA_650/analysis/IFA_650_4/IFA_650_4_part1.i)
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-25/puzry-25_aniso.i)
- (test/tests/phase_transition_zircaloy/ad_test_zrphase.i)
- (assessment/LWR/validation/RIA_CABRI_REP_Na/analysis/REP_Na_10/REP_Na_10.i)
- (assessment/LWR/validation/RIA_CABRI_REP_Na/analysis/REP_Na_2/REP_Na_2_RIA.i)
- (assessment/LWR/validation/LOCA_REBEKA_cladding_burst_tests/analysis/rebeka_2d_06MPa/rebeka_singlerod_2d_06MPa_aniso.i)
- (assessment/LWR/validation/LOCA_REBEKA_cladding_burst_tests/analysis/rebeka_2d_04MPa/rebeka_singlerod_2d_04MPa_aniso.i)
- (test/tests/zry_oxidation_cladding/zryoxidation_pingeo.i)
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-21/puzry-21.i)
- (assessment/LWR/validation/LOCA_Hardy_cladding_test/analysis/1pt4MPa/25C_sec/25C_sec_Hardy_Tube_Test_1pt4MPa.i)
- (assessment/LWR/validation/LOCA_Hardy_cladding_test/analysis/0pt7MPa/25C_sec/25C_sec_Hardy_Tube_Test_0pt7MPa.i)
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-29/puzry-29.i)
- (assessment/LWR/validation/LOCA_Hardy_cladding_test/analysis/2pt1MPa/100C_sec/100C_sec_Hardy_Tube_Test_2pt1MPa.i)
- (test/tests/solid_mechanics/zry_mechanics/elastic_modulus_zry_errorcheck.i)
- (assessment/LWR/validation/LOCA_Hardy_cladding_test/analysis/3pt8MPa/100C_sec/100C_sec_Hardy_Tube_Test_3pt8MPa.i)
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-05/puzry-05.i)
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-18/puzry-18_aniso.i)
- (assessment/LWR/benchmark/RIA_benchmark/analysis/RIA_benchmark.i)
- (assessment/LWR/validation/LOCA_Hardy_cladding_test/analysis/0pt7MPa/100C_sec/Hardy_Tube_Test_0pt7MPa.i)
- (assessment/LWR/validation/LOCA_REBEKA_cladding_burst_tests/analysis/rebeka_2d_02MPa/rebeka_singlerod_2d_02MPa_aniso.i)
- (assessment/LWR/validation/LOCA_Hardy_cladding_test/analysis/1pt4MPa/100C_sec/100C_sec_Hardy_Tube_Test_1pt4MPa.i)
- (assessment/LWR/validation/LOCA_Hardy_cladding_test/analysis/0pt5MPa/25C_sec/25C_sec_Hardy_Tube_Test_0pt5MPa.i)
- (assessment/LWR/validation/RIA_NSRR_FK/analysis/FK1/FK01.i)
- (assessment/LWR/validation/LOCA_Hardy_cladding_test/analysis/0pt3MPa/25C_sec/25C_sec_Hardy_Tube_Test_0pt3MPa.i)
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-11/puzry-11_aniso.i)
- (assessment/LWR/validation/LOCA_Studsvik/analysis/rod_196/Studsvik_196_part1.i)
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-20/puzry-20.i)
- (assessment/LWR/validation/RIA_NSRR_FK/analysis/FK7/FK07.i)
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-22/puzry-22_aniso.i)
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-13/puzry-13.i)
- (assessment/LWR/validation/RIA_NSRR_FK/analysis/FK8/FK08.i)
- (assessment/LWR/validation/LOCA_REBEKA_cladding_burst_tests/analysis/rebeka_2d_08MPa/rebeka_singlerod_2d_08MPa.i)
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-17/puzry-17.i)
- (assessment/LWR/validation/LOCA_ANL_cladding_burst_tests/analysis/OCL5_8/OCL5_8.i)
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-10/puzry-10_aniso.i)
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-14/puzry-14_aniso.i)
- (assessment/LWR/validation/LOCA_ORNL_cladding_burst_tests/analysis/Zr2_2/ornl_zr2_2_ad.i)
- (assessment/LWR/validation/LOCA_REBEKA_cladding_burst_tests/analysis/rebeka_2d_14MPa/rebeka_singlerod_2d_14MPa.i)
- (assessment/LWR/validation/RIA_NSRR_FK/analysis/FK4/FK04.i)
- (assessment/LWR/validation/LOCA_REBEKA_cladding_burst_tests/analysis/rebeka_2d_02MPa/rebeka_singlerod_2d_02MPa.i)
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-12/puzry-12_aniso.i)
- (assessment/LWR/validation/LOCA_ORNL_cladding_burst_tests/analysis/Zr2_1/ornl_zr2_1.i)
- (assessment/LWR/validation/LOCA_Hardy_cladding_test/analysis/1pt0MPa/25C_sec/25C_sec_Hardy_Tube_Test_1pt0MPa.i)
- (assessment/LWR/validation/RIA_CABRI_REP_Na/analysis/REP_Na_3/REP_Na_3_RIA.i)
- (examples/multiapp/pin2.i)
- (assessment/LWR/validation/RIA_CABRI_REP_Na/analysis/REP_Na_5/REP_Na_5_RIA.i)
- (assessment/LWR/validation/RIA_CABRI_REP_Na/analysis/REP_Na_5/REP_Na_5.i)
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-20/puzry-20_aniso.i)
- (assessment/LWR/validation/RIA_CABRI_REP_Na/analysis/REP_Na_3/REP_Na_3.i)
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-02/puzry-02.i)
- (assessment/LWR/validation/LOCA_ORNL_cladding_burst_tests/analysis/Zr2_2/ornl_zr2_2.i)
- (assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-08/puzry-08.i)
- (assessment/LWR/validation/LOCA_Studsvik/analysis/rod_196/Studsvik_196_part2_1p5d_fr_ffrd.i)
References
- C. M. Allison, G. A. Berna, R. Chambers, E. W. Coryell, K. L. Davis, D. L. Hagrman, D. T. Hagrman, N. L. Hampton, J. K. Hohorst, R. E. Mason, M. L. McComas, K. A. McNeil, R. L. Miller, C. S. Olsen, G. A. Reymann, and L. J. Siefken.
SCDAP/RELAP5/MOD3.1 code manual, volume IV: MATPRO-A library of materials properties for light-water-reactor accident analysis.
Technical Report NUREG/CR-6150, EGG-2720, Idaho National Engineering Laboratory, 1993.[BibTeX]
@TECHREPORT{hagrman93, author = "Allison, C. M. and Berna, G. A. and Chambers, R. and Coryell, E. W. and Davis, K. L. and Hagrman, D. L. and Hagrman, D. T. and Hampton, N. L. and Hohorst, J. K. and Mason, R. E. and McComas, M. L. and McNeil, K. A. and Miller, R. L. and Olsen, C. S. and Reymann, G. A. and Siefken, L. J.", editor = "Hagrman, D. T.", title = "{SCDAP/RELAP5/MOD3.1} Code Manual, Volume {IV}: {MATPRO}-{A} Library of Materials Properties for Light-Water-Reactor Accident Analysis", institution = "Idaho National Engineering Laboratory", year = "1993", number = "NUREG/CR-6150, EGG-2720" }
- IAEA.
Thermophysical properties database of materials for light water reactors and heavy water reactors: final report of a coordinated research project 1999-2005.
Technical Report IAEA-TECDOC-1496, IAEA, 2006.[BibTeX]
@TECHREPORT{IAEA_tecdoc1496, author = "IAEA", title = "Thermophysical properties database of materials for light water reactors and heavy water reactors: Final report of a coordinated research project 1999-2005", institution = "IAEA", number = "IAEA-TECDOC-1496", year = "2006" }
(test/tests/thermalZry/thermal_test_IAEA.i)
# The mesh is a 1x1x1 cube (single element).
# The temperature is ramped on all faces of the cube from 300 K to 1200K
# over 100 Ms.
#
# Thermal conductivity and specific heat are computed using the pure Zry
# thermal model with the equations from the IAEA report IAEA-TECDOC-1496.
#
# The thermal conductivity and specific heat computed by BISON for the
# temperatures shown below and compared with analytical solution.
#
# The results are as follows:
# Thermal Conductivity Specific Heat
# ------------------------- ---------------------
# Analytical BISON Analytical BISON
# Temp(K) (W/m-K) (W/m-K) J/(kgK) J/(kgK)
# 300 13.412 13.412 286.38 286.38
# 608 15.757 15.757 317.92 317.92
# 905 19.631 19.631 348.33 1348.33
# 1202 25.091 25.091 1663.09 1663.09
# 1400 29.61 29.61 331.52 331.52
[Mesh]
[mesh]
type = GeneratedMeshGenerator
dim = 3
[]
[]
[Variables]
[T]
order = FIRST
family = LAGRANGE
initial_condition = 300
[]
[]
[AuxVariables]
[th_cond]
order = CONSTANT
family = MONOMIAL
[]
[cp]
order = CONSTANT
family = MONOMIAL
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = T
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = T
[]
[]
[AuxKernels]
[th_cond]
type = MaterialRealAux
variable = th_cond
property = thermal_conductivity
execute_on = 'initial linear'
[]
[cp]
type = MaterialRealAux
variable = cp
property = specific_heat
execute_on = 'initial linear'
[]
[]
[Functions]
[temp_ramp]
type = PiecewiseLinear
x = '0.0 100.e6'
y = '300 1400'
[]
[]
[BCs]
[VariableT]
type = FunctionDirichletBC
boundary = 'left right front back bottom top'
variable = T
function = temp_ramp
[]
[]
[Materials]
[thermal_clad]
type = ZryThermal
temperature = T
zry_thermal_properties_model = IAEA
[]
[density]
type = Density
density = 1200.0
[]
[]
[Executioner]
type = Transient
solve_type = PJFNK
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-ksp_gmres_restart'
petsc_options_value = '101'
line_search = 'none'
l_max_its = 100
nl_max_its = 100
nl_rel_tol = 1e-4
nl_abs_tol = 1e-6
l_tol = 1e-5
start_time = 0.0
end_time = 100.e6
dt = 1.0e6
[]
[Postprocessors]
[ave_temp_interior]
type = SideAverageValue
boundary = 'left right top bottom front back'
variable = T
execute_on = 'initial timestep_end'
[]
[avg_th_cond]
type = ElementAverageValue
variable = th_cond
execute_on = 'initial timestep_end'
[]
[avg_cp]
type = ElementAverageValue
variable = cp
execute_on = 'initial timestep_end'
[]
[average_fuel_T]
type = ElementAverageValue
variable = T
execute_on = 'initial timestep_end'
[]
[]
[Outputs]
exodus = true
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-26/puzry-26_aniso.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-26.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 2000. '
y = '1.e+05 1.e+05 1.203e+07' # Linear increase at 0.1193 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 2000. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
# Circumferential steady-state creep test and analysis of Zircaloy-4 fuel cladding
# Nuclear Engineering and Design, 53, 2312-2322 (2021)
[F]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.738 0.738 0.57'
[]
[G]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.174 0.174 0.45'
[]
[H]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.588 0.588 0.48'
[]
[L]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[M]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[N]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = TaylorExpansion
use_automatic_differentiation = true
[]
[]
[]
[]
[Kernels]
[heat]
type = ADHeatConduction
variable = temperature
[]
[heat_ie]
type = ADHeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = ADMaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = ADMaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = ADMaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = ADMaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = ADMaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = ADFunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = ADDirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = ADDirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ADZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1.e+11
poissons_ratio = 0.3
block = 1
[]
[hill_constants]
type = ADHillConstants
hill_constants = "0.738 0.174 0.588 1.0 1.0 1.0"
function_names = "F G H L M N"
temperature = temperature
[]
[creep_update]
type = ADZryAnisoCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 1.5e-05
temperature = temperature
temperature_standard_thermal_creep_end = 700
temperature_loca_creep_begin = 900.
fract_beta_phase_name = 'fract_beta_phase'
max_integration_error = 1000000.0
absolute_tolerance = 1e-13
relative_tolerance = 1e-11
[]
[creep]
type = ADComputeMultipleInelasticStress
block = 1
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ADZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = ADDensity
block = 1
[]
[phase]
type = ADZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ADZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = NEWTON
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-07
start_time = 0.
n_startup_steps = 1
end_time = 2500.
dtmax = 1.
dtmin = 1.0e-9
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-26_aniso_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/RIA_CABRI_REP_Na/analysis/REP_Na_2/REP_Na_2.i)
# REP Na 2 Base Irradiation
[GlobalParams]
density = 10344.71
displacements = 'disp_x disp_y'
temperature = temp
order = SECOND
family = LAGRANGE
energy_per_fission = 3.2e-11
volumetric_locking_correction = false
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
acceptable_iterations = 30
acceptable_multiplier = 10
[]
[Mesh]
coord_type = RZ
[smeared_pellet_mesh]
type = FuelPinMeshGenerator
clad_mesh_density = customize
pellet_mesh_density = customize
nx_p = 11
ny_p = 336
ny_cu = 3
ny_c = 350
ny_cl = 3
nx_c = 4
clad_thickness = 0.000637
pellet_outer_radius = 0.0040248
pellet_quantity = 84
pellet_height = 0.0119888
clad_top_gap_height = 0.041077
clad_bot_gap_height = 0.003
clad_gap_width = 93.0e-6
bottom_clad_height = 0.0015
top_clad_height = 0.0015
elem_type = QUAD8
[]
patch_size = 40
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temp]
initial_condition = 293.15
[]
[]
[AuxVariables]
[fast_neutron_flux]
block = 1
[]
[fast_neutron_fluence]
block = 1
[]
[grain_radius]
block = 3
initial_condition = 5.0e-6
[]
[gap_cond]
order = CONSTANT
family = MONOMIAL
[]
[fuel_cond]
order = CONSTANT
family = MONOMIAL
[]
[swelling_strain]
order = CONSTANT
family = MONOMIAL
block = 3
[]
[total_hoop_strain]
order = CONSTANT
family = MONOMIAL
[]
[total_axial_strain]
order = CONSTANT
family = MONOMIAL
[]
[clad_coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[coolant_temp]
order = CONSTANT
family = MONOMIAL
[]
[clad_coolant_flux]
order = CONSTANT
family = MONOMIAL
[]
[coolant_channel_hmode]
order = CONSTANT
family = MONOMIAL
[]
[coolant_channel_htype]
order = CONSTANT
family = MONOMIAL
[]
[critical_heat_flux]
order = CONSTANT
family = MONOMIAL
[]
[oxide_thickness]
order = CONSTANT
family = MONOMIAL
[]
[SED]
order = CONSTANT
family = MONOMIAL
block = 1
[]
[oxywtfract_total]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfgain_total]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[]
[Functions]
[power_profile]
type = PiecewiseLinear
data_file = REPNa2_power_history_Full.csv
format = columns
[]
[axial_peaking_factors]
type = PiecewiseBilinear
data_file = REPNa2_axial_peaking_Full.csv
axis = 1
[]
[pressure_ramp]
type = PiecewiseLinear
xy_data = '0 101325
8640 13999808
57067200 13999808
57110400 101325
57542410 101325
57542450 500008
57542700 500008
57542800 101325
57542900 101325'
[]
[temp_ramp]
type = PiecewiseLinear
xy_data = '0 293.15
8640 543.15
57067200 543.15
57110400 293.15
57542410 293.15
57542450 553.15
57542700 553.15
57542800 293.15
57542900 293.15'
[]
[Fuel_CTE_function] #Fuel CTE as a function of temp from MATPRO data
type = PiecewiseLinear
xy_data = ' 0 1.000E-05
300 1.000E-05
350 1.000E-05
400 1.000E-05
450 1.000E-05
500 1.001E-05
550 1.002E-05
600 1.003E-05
650 1.005E-05
700 1.008E-05
750 1.011E-05
800 1.015E-05
850 1.020E-05
900 1.026E-05
950 1.032E-05
1000 1.039E-05
1050 1.046E-05
1100 1.053E-05
1150 1.061E-05
1200 1.069E-05
1250 1.077E-05
1300 1.085E-05
1350 1.094E-05
1400 1.102E-05
1450 1.111E-05
1500 1.119E-05
1550 1.127E-05
1600 1.135E-05
1650 1.143E-05
1700 1.151E-05
1750 1.158E-05
1800 1.166E-05
1850 1.173E-05
1900 1.180E-05
1950 1.187E-05
2000 1.193E-05
2050 1.199E-05
2100 1.205E-05
2150 1.211E-05
2200 1.217E-05
2250 1.222E-05
2300 1.227E-05
2350 1.232E-05
2400 1.237E-05
2450 1.242E-05
2500 1.246E-05
2550 1.250E-05
2600 1.254E-05
2650 1.258E-05
2700 1.262E-05
2750 1.265E-05
2800 1.268E-05
2850 1.271E-05
2900 1.274E-05
2950 1.277E-05
3000 1.280E-05
3050 1.282E-05
3100 1.285E-05'
[]
[burnup_GWd]
type = ParsedFunction
expression = bu*950
symbol_names = 'bu'
symbol_values = 'average_burnup'
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[fuel]
block = 3
strain = FINITE
incremental = true
eigenstrain_names = 'fuel_relocation_eigenstrain fuel_thermal_eigenstrain
fuel_volumetric_swelling_eigenstrain'
extra_vector_tags = 'ref'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz'
[]
[clad]
block = 1
strain = FINITE
incremental = true
eigenstrain_names = 'clad_irradiation_growth_eigenstrain
clad_thermal_eigenstrain'
extra_vector_tags = 'ref'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz plastic_strain_xx plastic_strain_yy plastic_strain_zz
creep_strain_xx creep_strain_yy creep_strain_zz elastic_strain_xx
elastic_strain_yy elastic_strain_zz hoop_stress'
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temp
extra_vector_tags = 'ref'
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temp
extra_vector_tags = 'ref'
[]
[heat_source_fuel]
type = NeutronHeatSource
variable = temp
block = 3
burnup_function = burnup
extra_vector_tags = 'ref'
[]
[]
[Burnup]
[burnup]
block = 3
rod_ave_lin_pow = power_profile
axial_power_profile = axial_peaking_factors
num_radial = 80
num_axial = 85
a_upper = 1.0115592
a_lower = 0.0045
fuel_inner_radius = 0
fuel_outer_radius = 0.0040248
fuel_volume_ratio = 1
isotopes = 'U235 U238 Pu239 Pu240 Pu241 Pu242'
isotope_fractions = '0.0685 0.9315 0 0 0 0'
RPF = RPF
order = CONSTANT
family = MONOMIAL
[]
[]
[AuxKernels]
[fast_neutron_flux]
type = FastNeutronFluxAux
variable = fast_neutron_flux
block = 1
axial_power_profile = axial_peaking_factors
rod_ave_lin_pow = power_profile
factor = 3e13 #n/m2-s
execute_on = timestep_begin
[]
[fast_neutron_fluence]
type = FastNeutronFluenceAux
variable = fast_neutron_fluence
fast_neutron_flux = fast_neutron_flux
block = 1
execute_on = timestep_begin
[]
[grain_radius]
type = GrainRadiusAux
block = 3
variable = grain_radius
temperature = temp
execute_on = linear
[]
[gap_conductance]
type = MaterialRealAux
property = gap_conductance
variable = gap_cond
boundary = 10
[]
[fuel_conductance]
type = MaterialRealAux
property = thermal_conductivity
variable = fuel_cond
block = 3
[]
[swelling_strain]
type = MaterialRealAux
property = volumetric_swelling_strain
variable = swelling_strain
block = 3
[]
[total_hoop_strain]
type = RankTwoScalarAux
rank_two_tensor = total_strain
variable = total_hoop_strain
scalar_type = HoopStress
execute_on = timestep_end
block = 1
[]
[total_axial_strain]
type = RankTwoScalarAux
rank_two_tensor = total_strain
variable = total_axial_strain
scalar_type = AxialStress
execute_on = timestep_end
block = 1
[]
[clad_coolant_htc]
type = MaterialRealAux
property = coolant_channel_htc
variable = clad_coolant_htc
boundary = 2
[]
[coolant_temp]
type = MaterialRealAux
property = coolant_temperature
variable = coolant_temp
boundary = 2
[]
[clad_coolant_flux]
type = MaterialRealAux
property = output_heat_flux
variable = clad_coolant_flux
boundary = 2
[]
[coolant_channel_hmode]
type = MaterialRealAux
property = coolant_channel_hmode
variable = coolant_channel_hmode
boundary = 2
[]
[coolant_channel_htype]
type = MaterialRealAux
property = coolant_channel_htype
variable = coolant_channel_htype
boundary = 2
[]
[critical_heat_flux]
type = MaterialRealAux
property = critical_heat_flux
variable = critical_heat_flux
boundary = 2
[]
[oxide]
type = MaterialRealAux
property = oxide_scale_thickness
variable = oxide_thickness
boundary = 2
[]
[SED]
type = MaterialRealAux
variable = SED
property = strain_energy_density
execute_on = timestep_end
[]
[ofract_total]
type = MaterialRealAux
variable = oxywtfract_total
property = current_oxygen_weight_frac_total
execute_on = timestep_end
boundary = 2
[]
[ofgain_total]
type = MaterialRealAux
variable = oxywtfgain_total
property = oxygen_weight_frac_gained_total
execute_on = timestep_end
boundary = 2
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
block = 1
[]
[]
[Contact]
[pellet_clad_mechanical]
primary = 5
secondary = 10
penalty = 1e10
formulation = penalty
normalize_penalty = false
model = frictionless
normal_smoothing_distance = 0.1
[]
[]
[ThermalContact]
[thermal_contact]
type = GasGapHeatTransfer
variable = temp
primary = 5
secondary = 10
initial_moles = initial_moles
gas_released = fission_gas_released
jump_distance_model = LANNING
plenum_pressure = plenum_pressure
contact_pressure = contact_pressure
roughness_primary = 2.0e-6
roughness_secondary = 0.5e-6
roughness_coef = 3.2
normal_smoothing_distance = 0.1
quadrature = true
emissivity_primary = 0.797698
emissivity_secondary = 0.325
refab_time = 57456000
refab_gas_types = He
refab_fractions = 1
[]
[]
[BCs]
[no_x_all]
type = DirichletBC
variable = disp_x
boundary = 12
value = 0.0
[]
[no_y_clad_bottom]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[]
[no_y_fuel_bottom]
type = DirichletBC
variable = disp_y
boundary = 20
value = 0.0
[]
[Pressure]
[coolantPressure]
boundary = '1 2 3'
function = pressure_ramp
[]
[]
[PlenumPressure]
[plenumPressure]
boundary = 9
initial_temperature = 293.15
initial_pressure = 1.70e6
startup_time = 0
R = 8.3143
output_initial_moles = initial_moles
temperature = plenum_temperature
volume = plenum_volume
material_input = fission_gas_released
output = plenum_pressure
refab_time = 57456000
refab_pressure = 0.1e6
refab_temperature = 293.15
refab_volume = 2.3e-6
[]
[]
[]
[CoolantChannel]
[convective_clad_surface]
boundary = '1 2 3'
variable = temp
inlet_temperature = temp_ramp # K
inlet_pressure = pressure_ramp # Pa
inlet_massflux = 1779 # kg/m^2-sec
rod_diameter = 0.0095096 # m
rod_pitch = 1.265e-2 # m
coolant_material = 'water'
compute_enthalpy = true
oxide_thickness = oxide_thickness
[]
[]
[Materials]
[swelling]
type = UO2VolumetricSwellingEigenstrain
block = 3
burnup_function = burnup
initial_fuel_density = 10344.71
include_solid_swelling = true
include_densification = true
total_densification = 0.00676
initial_porosity = 0.057
eigenstrain_name = 'fuel_volumetric_swelling_eigenstrain'
[]
[fuel_thermal]
type = UO2Thermal
block = 3
thermal_conductivity_model = NFIR
temperature = temp
burnup_function = burnup
initial_porosity = 0.057
[]
[fuel_elastic_stress]
type = ComputeFiniteStrainElasticStress
block = 3
[]
[fuel_elasticity_tensor]
type = UO2ElasticityTensor
block = 3
[]
[fuel_thermal_expansion]
type = ComputeInstantaneousThermalExpansionFunctionEigenstrain
block = 3
stress_free_temperature = 293.15
thermal_expansion_function = Fuel_CTE_function
eigenstrain_name = 'fuel_thermal_eigenstrain'
[]
[fuel_relocation]
type = UO2RelocationEigenstrain
block = 3
burnup_function = burnup
diameter = 0.0080496
rod_ave_lin_pow = power_profile
axial_power_profile = axial_peaking_factors
diametral_gap =186.0e-6
burnup_relocation_stop = 0.024
relocation_activation1 = 5000
eigenstrain_name = 'fuel_relocation_eigenstrain'
[]
[clad_thermal]
type = ZryThermal
block = 1
temperature = temp
[]
[clad_zrycreep]
type = ZryCreepLimbackHoppeUpdate
block = 1
fast_neutron_flux = fast_neutron_flux
fast_neutron_fluence = fast_neutron_fluence
zircaloy_material_type = stress_relief_annealed
max_inelastic_increment = 5.0e-3
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = 1
fast_neutron_fluence = fast_neutron_fluence
cold_work_factor = 0.5
oxygen_concentration = 0.0
matpro_poissons_ratio = false
matpro_youngs_modulus = true
[]
[clad_inelastic_stress]
type = ComputeMultipleInelasticStress
block = 1
tangent_operator = elastic
inelastic_models = 'clad_zrycreep plasticity'
[]
[clad_thermal_eigenstrain]
type = ZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 293.15
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[clad_irradiation_eigenstrain]
type = ZryIrradiationGrowthEigenstrain
block = 1
fast_neutron_fluence = fast_neutron_fluence
zircaloy_material_type = stress_relief_annealed
eigenstrain_name = 'clad_irradiation_growth_eigenstrain'
[]
[plasticity]
type = ZryPlasticityUpdate
block = 1
cold_work_factor = 0.5
fast_neutron_fluence = fast_neutron_fluence
fast_neutron_flux = fast_neutron_flux
plasticity_model_type = MATPRO
oxygen_concentration = 0.0
max_inelastic_increment = 5.0e-3
[]
[density_clad]
type = Density
block = 1
density = 6550
[]
[density_fuel]
type = Density
block = 3
[]
[fission_gas_release]
type = UO2Sifgrs
block = 3
temperature = temp
burnup_function = burnup
initial_porosity = 0.057
grain_radius = grain_radius
gbs_model = true
transient_option = NO_TRANSIENT
[]
[ZryOxidation]
type = ZryOxidation
boundary = 2
clad_inner_radius = 0.0041178
clad_outer_radius = 0.0047549
use_coolant_channel = true
fast_neutron_flux = fast_neutron_flux
[]
[phase]
type = ZrPhase
block = 1
numerical_method = 2
[]
[strain_energy_density]
type = StrainEnergyDensity
incremental = true
[]
[]
[Dampers]
[BoundingValueNodalDamper]
type = BoundingValueNodalDamper
max_value = 3200
min_value = 200
variable = temp
[]
[contact_slip]
type = ContactSlipDamper
primary = 5
secondary = 10
min_damping_factor = 0.05
[]
[]
[Preconditioning]
[SMP]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-3
nl_max_its = 40
nl_rel_tol = 1e-4
nl_abs_tol = 1e-10
start_time = 0
end_time = 57542400
dtmax = 1e6
dtmin = 1e-7
[TimeStepper]
type = IterationAdaptiveDT
dt = 1.0e3
optimal_iterations = 100
iteration_window = 4
linear_iteration_ratio = 100
timestep_limiting_function = power_profile
max_function_change = 1e6
force_step_every_function_point = true
timestep_limiting_postprocessor = material_timestep_control
time_t = '57542410 57542420 57542430 57542440 57542450 57542460 57542470 57542480 57542500 57542500.01 57542500.02 57542500.03 57542500.04 57542500.05 57542500.06 57542500.07'
time_dt = '10 10 10 10 10 10 10 10 0.001 0.001 0.001 0.001 0.001 0.001 0.001 0.001'
[]
[Quadrature]
order = FIFTH
side_order = SEVENTH
[]
[]
[Postprocessors]
[fis_gas_grain]
type = ElementIntegralFisGasGrainSifgrs
block = 3
outputs = exodus
[]
[fis_gas_boundary]
type = ElementIntegralFisGasBoundarySifgrs
block = 3
outputs = exodus
[]
[rod_input_power]
type = FunctionValuePostprocessor
function = power_profile
[]
[burnup_GWd]
type = FunctionValuePostprocessor
function = burnup_GWd
[]
#######################################
[penetration]
type = NodalVariableValue
variable = penetration
nodeid = 11625
use_displaced_mesh = 1
[]
[contact_pressure]
type = NodalVariableValue
variable = contact_pressure
nodeid = 11625
use_displaced_mesh = 1
[]
[gap_cond]
type = ElementalVariableValue
variable = gap_cond
elementid = 3502
use_displaced_mesh = 1
[]
[creep_hoop_strain]
type = ElementalVariableValue
variable = creep_strain_zz
elementid = 780
use_displaced_mesh = 1
[]
[elastic_hoop_strain]
type = ElementalVariableValue
variable = elastic_strain_zz
elementid = 780
use_displaced_mesh = 1
[]
[plastic_hoop_strain]
type = ElementalVariableValue
variable = plastic_strain_zz
elementid = 780
use_displaced_mesh = 1
[]
[total_hoop_strain]
type = ElementalVariableValue
variable = total_hoop_strain
elementid = 780
use_displaced_mesh = 1
[]
[clad_hoop_stress]
type = ElementalVariableValue
variable = hoop_stress
elementid = 780
use_displaced_mesh = 1
[]
[clad_axial_elongation]
type = NodalVariableValue
variable = disp_y
nodeid = 5111
use_displaced_mesh = 1
[]
[clad_oxide_thickness]
type = ElementalVariableValue
variable = oxide_thickness
elementid = 780
use_displaced_mesh = 1
[]
[clad_coolant_htc]
type = ElementalVariableValue
variable = clad_coolant_htc
elementid = 780
use_displaced_mesh = 1
[]
[coolant_temp]
type = ElementalVariableValue
variable = coolant_temp
elementid = 780
use_displaced_mesh = 1
[]
[fuel_centerline_temp]
type = NodalVariableValue
variable = temp
nodeid = 11594
[]
[fuel_surface_temp]
type = NodalVariableValue
variable = temp
nodeid = 11625
[]
[clad_inner_surface_temp]
type = NodalVariableValue
variable = temp
nodeid = 2721
[]
[clad_outer_surface_temp]
type = NodalVariableValue
variable = temp
nodeid = 2731
[]
[fuel_axial_elongation]
type = NodalVariableValue
variable = disp_y
nodeid = 17015
[]
[clad_radial_elongation]
type = NodalVariableValue
variable = disp_x
nodeid = 2731
[]
[fuel_radial_elongation]
type = NodalVariableValue
variable = disp_x
nodeid = 11625
[]
[SED_PPN_O]
type = ElementalVariableValue
variable = SED
elementid = 780
use_displaced_mesh = 1
[]
[SED_PPN_I]
type = ElementalVariableValue
variable = SED
elementid = 777
use_displaced_mesh = 1
[]
[OFract_PPN_O]
type = ElementalVariableValue
variable = oxywtfract_total
elementid = 780
use_displaced_mesh = 1
[]
[OGain_PPN_O]
type = ElementalVariableValue
variable = oxywtfgain_total
elementid = 780
use_displaced_mesh = 1
[]
#######################################
[max_fuel_temp]
type = NodalExtremeValue
block = 3
variable = temp
[]
[max_clad_temp]
type = NodalExtremeValue
block = 1
variable = temp
[]
[max_clad_SED]
type = ElementExtremeValue
block = 1
variable = SED
value_type = max
[]
[RAE]
type = RadialAverageEnthalpy
vector_postprocessor = rad_temp
radial_direction = x
axial_direction = y
axial_position = 0.55
temperature_name = temp
[]
[material_timestep_control]
type = MaterialTimeStepPostprocessor
block = 1
[]
[peak_RAE]
type = TimeExtremeValue
postprocessor = RAE
[]
[]
[VectorPostprocessors]
[ox_thick]
type = SideValueSampler
variable = oxide_thickness
boundary = 2
sort_by = y
outputs = 'outfile_oxide_thickness'
[]
[rad_temp]
type = NodalValueSampler
block = 3
sort_by = y
variable = temp
execute_on = timestep_end
outputs = 'outfile_radial_temp'
[]
[]
[StandardLWRFuelRodOutputs]
fuel_pellet_blocks = 3
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
csv = true
color = true
[outfile_oxide_thickness]
type = CSV
sync_times = '57542400 57542900'
sync_only = true
[]
[outfile_radial_temp]
type = CSV
enable = false
[]
[console]
type = Console
output_linear = true
max_rows = 10
[]
[checkpoint]
type = Checkpoint
num_files = 2
file_base = recover_files
sync_times = '57542400'
sync_only = true
[]
[chkfile]
type = CSV
show = 'plenum_temperature fission_gas_released_percentage
average_centerline_fuel_temperature average_burnup peak_RAE'
execute_on = 'FINAL'
[]
[exodus]
type = Exodus
time_step_interval = 4
end_time = 57542500
[]
[exodus_RIA]
type = Exodus
time_step_interval = 2
start_time = 57542495
[]
[]
(assessment/LWR/validation/RIA_NSRR_FK/analysis/FK2/FK02.i)
# This file was created using BIF with the following inputs:
# FK02.var - md5sum: 123016ae8f3283a45bae816a366f93b1
# ../pulse_rev1.tpl - md5sum: 8d6b8b4bce1dd830dea2d8522009e514
[GlobalParams]
density = 10020.6066633
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
energy_per_fission = 3.2e-11
a_lower = 0.01822
a_upper = 0.12422
temperature = temp
volumetric_locking_correction = false
[]
[Mesh]
coord_type = RZ
[smeared_pellet_mesh]
type = FuelPinMeshGenerator
clad_mesh_density = customize
pellet_mesh_density = customize
elem_type = QUAD8
ny_p = 100
nx_c = 4
ny_c = 100
nx_p = 12
ny_cu = 3
ny_cl = 3
bx_p = 0.75
clad_bot_gap_height = 0.00152
bottom_clad_height = 0.0167
top_clad_height = 0.0167
clad_thickness = 0.00086
pellet_outer_radius = 0.00527
clad_top_gap_height = 0.03481
pellet_height = 0.106
clad_gap_width = 1e-05
pellet_quantity = 1
[]
patch_size = 5
patch_update_strategy = auto
partitioner = centroid
centroid_partitioner_direction = y
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
[]
[Variables]
[temp]
initial_condition = 293
[]
[]
[AuxVariables]
[BuTC]
[]
[gap]
order = CONSTANT
family = MONOMIAL
[]
[fast_neutron_flux]
block = 1
[]
[fast_neutron_fluence]
block = 1
[]
[buavg]
order = CONSTANT
family = MONOMIAL
[]
[fission_rate]
initial_condition = 0
[]
[grain_radius]
block = 3
initial_condition = 5.96e-6
[]
[integral_burnup]
order = CONSTANT
family = MONOMIAL
[]
[pellet_id]
order = CONSTANT
family = MONOMIAL
block = 3
[]
[gap_conductivity]
order = CONSTANT
family = MONOMIAL
[]
[porosity]
order = CONSTANT
family = MONOMIAL
initial_condition = 0.085711070864
[]
[SED]
order = CONSTANT
family = MONOMIAL
[]
[]
[Functions]
[linear_heat_rate_profile]
type = PiecewiseLinear
data_file = pulse.csv
format = columns
[]
[flux]
type = ConstantFunction
value = 0.0
[]
[axial_peaking_factors]
type = ConstantFunction
value = 1
[]
[coolant_pressure_ramp]
type = ConstantFunction
value = 101325
[]
[linear_heat_generation_rate]
type = CompositeFunction
functions = 'linear_heat_rate_profile axial_peaking_factors'
[]
[axial_flux]
type = CompositeFunction
functions = 'flux axial_peaking_factors'
[]
[burnup_thermal_conductivity]
type = ConstantFunction
value = 0.0473684210526 # should be burnup / 950
[]
[radial_power_profile]
type = PiecewiseBilinear
data_file = RadialPowerProfile.csv
axis = 0
[]
[radial_burnup_profile]
type = PiecewiseBilinear
data_file = RadialBurnupProfile.csv
axis = 0
[]
[initial_burnup]
type = CompositeFunction
functions = 'burnup_thermal_conductivity radial_burnup_profile'
[]
[]
[Burnup]
[burnup]
block = 3
rod_ave_lin_pow = linear_heat_rate_profile
axial_power_profile = axial_peaking_factors
rpf_input = radial_power_profile
num_radial = 80
num_axial = 49
fuel_inner_radius = 0.0
fuel_outer_radius = 0.00527
fuel_volume_ratio = 1.0
isotopes = 'U235 U238 Pu239 Pu240 Pu241 Pu242'
isotope_fractions = '0.039 0.961 0.0 0.0 0.0 0.0'
[]
[]
[Physics/SolidMechanics/QuasiStatic]
add_variables = true
[fuel]
block = 3
strain = FINITE
incremental = true
eigenstrain_names = 'fuel_thermal_eigenstrain
fuel_volumetric_swelling_eigenstrain'
extra_vector_tags = 'ref'
generate_output = 'vonmises_stress hydrostatic_stress elastic_strain_xx
elastic_strain_yy elastic_strain_zz stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz'
decomposition_method = EigenSolution
[]
[clad]
block = 1
strain = FINITE
incremental = true
eigenstrain_names = 'clad_thermal_eigenstrain'
extra_vector_tags = 'ref'
generate_output = 'vonmises_stress elastic_strain_xx
elastic_strain_yy elastic_strain_zz stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz creep_strain_xx creep_strain_yy creep_strain_zz'
decomposition_method = EigenSolution
[]
[]
[Kernels]
[gravity]
type = Gravity
variable = disp_y
value = -9.81
extra_vector_tags = 'ref'
[]
[heat]
type = HeatConduction
variable = temp
extra_vector_tags = 'ref'
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temp
extra_vector_tags = 'ref'
[]
[heat_source]
type = NeutronHeatSource
fission_rate = fission_rate
variable = temp
block = 3
extra_vector_tags = 'ref'
[]
[]
[AuxKernels]
[BuTC]
type = FunctionAux
block = 3
variable = BuTC
function = initial_burnup
[]
[pelletid]
type = PelletIdAux
block = 3
variable = pellet_id
number_pellets = 1
execute_on = initial
[]
[gap]
type = SpatialUserObjectAux
block = 3
variable = gap
execute_on = timestep_end
user_object = avg_gap
[]
[buavg]
type = SpatialUserObjectAux
block = 3
variable = buavg
execute_on = timestep_end
user_object = integral_burnup
[]
[fast_neutron_flux]
type = FastNeutronFluxAux
variable = fast_neutron_flux
function = axial_flux
block = 1
execute_on = timestep_begin
[]
[fast_neutron_fluence]
type = FastNeutronFluenceAux
variable = fast_neutron_fluence
block = 1
fast_neutron_flux = fast_neutron_flux
execute_on = timestep_begin
[]
[fuel_porosity]
type = PorosityAuxUO2
block = 3
variable = porosity
execute_on = timestep_begin
[]
[grain_radius]
type = GrainRadiusAux
block = 3
variable = grain_radius
temperature = temp
execute_on = timestep_begin
[]
[gap_conductance]
type = MaterialRealAux
property = gap_conductance
variable = gap_conductivity
boundary = 10
[]
[SED]
type = MaterialRealAux
variable = SED
property = strain_energy_density
execute_on = timestep_end
block = 1
[]
[]
[Contact]
[pellet_clad_mechanical]
primary = 5
secondary = 10
penalty = 1e14
normalize_penalty = true
model = frictionless
friction_coefficient = 2.5
normal_smoothing_distance = 0.1
formulation = penalty
[]
[]
[ThermalContact]
[thermal_contact]
type = GasGapHeatTransfer
variable = temp
primary = 5
secondary = 10
roughness_coef = 3.2
roughness_primary = 1.5e-6
roughness_secondary = 1.75e-6
jump_distance_model = LANNING
plenum_pressure = plenum_pressure
contact_pressure = contact_pressure
initial_moles = initial_moles
gas_released = fission_gas_released
tangential_tolerance = 1.0e-6
quadrature = true
[]
[]
[BCs]
[no_x_all]
type = DirichletBC
variable = disp_x
boundary = 12
value = 0.0
[]
[no_y_fuel_bottom]
type = DirichletBC
variable = disp_y
boundary = 20
value = 0.0
[]
[no_y_clad_bottom]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[]
[coolant_temp]
type = DirichletBC
boundary = '1 2 3'
variable = temp
value = 293
[]
[Pressure]
[coolantPressure]
boundary = '1 2 3'
factor = 1
function = coolant_pressure_ramp
[]
[]
[PlenumPressure]
[plenumPressure]
boundary = '10 5'
initial_pressure = 0.3e6
startup_time = 0
R = 8.314462
output_initial_moles = initial_moles
temperature = plenum_temperature
volume = plenum_volume
material_input = fission_gas_released
output = plenum_pressure
initial_temperature = 293
[]
[]
[]
[Materials]
[fuel_swelling]
type = UO2VolumetricSwellingEigenstrain
block = 3
burnup = burnup
initial_fuel_density = 10020.6066633
total_densification = 0.006
gas_swelling_model_type = SIFGRS
eigenstrain_name = 'fuel_volumetric_swelling_eigenstrain'
[]
[fuel_thermal]
type = UO2Thermal
thermal_conductivity_model = NFIR
block = 3
temperature = temp
burnup = BuTC
initial_porosity = 0.085711070864
[]
[fuel_elasticity_tensor]
type = UO2ElasticityTensor
block = 3
[]
[fuel_thermal_expansion]
type = UO2ThermalExpansionMartinEigenstrain
block = 3
stress_free_temperature = 293
eigenstrain_name = 'fuel_thermal_eigenstrain'
[]
[fuel_elastic_stress]
type = ComputeFiniteStrainElasticStress
block = '3'
[]
[clad_thermal]
type = ZryThermal
block = 1
temperature = temp
[]
## TODO: Creep is not active, but is transfered from the SM version.
## Adding creep causes the Peak Hoop strain to best match the FALCON
## results given by R. Montgomery and D. Sunderland. Only retaining
## plasticity matches the results from Wenfeng Liu, John Alvis, Robert Montgomery, and Ken Yueh
[clad_creep_stress]
type = ZryCreepLimbackHoppeUpdate
block = 1
fast_neutron_flux = fast_neutron_flux
fast_neutron_fluence = fast_neutron_fluence
initial_fast_fluence = 8.40e25
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = 1
fast_neutron_fluence = fast_neutron_fluence
initial_fast_fluence = 8.40e25
cold_work_factor = 0.01
matpro_youngs_modulus = true
matpro_poissons_ratio = true
[]
[clad_thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 293.0
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[clad_inelastic_stress]
type = ComputeMultipleInelasticStress
block = 1
tangent_operator = elastic
inelastic_models ='plasticity'
[]
[plasticity]
type = ZryPlasticityUpdate
block = 1
initial_fast_fluence = 8.40e25
fast_neutron_flux = fast_neutron_flux
fast_neutron_fluence = fast_neutron_fluence
cold_work_factor = 0.01
plasticity_model_type = MATPRO
output_properties = yield_stress
outputs = all
zircaloy_alloy_type = 4
[]
[fission_gas_release]
type = UO2Sifgrs
block = 3
temperature = temp
fission_rate = fission_rate
grain_radius = grain_radius
gbs_model = true
burnup = BuTC
transient_option = MICROCRACKING
[]
[clad_density]
type = Density
block = 1
density = 6551
[]
[fuel_density]
type = Density
block = 3
[]
[strain_energy_density]
type = StrainEnergyDensity
incremental = true
[]
[]
[UserObjects]
[avg_gap]
type = LayeredAverage
block = 3
variable = penetration
direction = y
num_layers = 48
[]
[pbz]
type = PelletBrittleZone
block = 3
pellet_id = pellet_id
temperature = temp
pellet_radius = 0.00527
number_pellets = 1
execute_on = timestep_begin
[]
[integral_burnup]
type = LayeredAverage
block = 3
variable = burnup
direction = y
num_layers = 1
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
l_max_its = 40
l_tol = 8e-3
nl_max_its = 40
nl_rel_tol = 1e-3
nl_abs_tol = 1e-10
dtmin = 0.00001
dtmax = 1.0
start_time = 0
end_time = 100
[TimeStepper]
type = IterationAdaptiveDT
dt = 0.0001
optimal_iterations = 200
linear_iteration_ratio = 100
timestep_limiting_function = linear_heat_rate_profile
max_function_change = 500000
force_step_every_function_point = true
[]
[]
[Dampers]
[limitT]
type = MaxIncrement
max_increment = 100.0
variable = temp
[]
[limitX]
type = MaxIncrement
max_increment = 1e-5
variable = disp_x
[]
[contactslip]
type = ContactSlipDamper
primary = 5
secondary = 8
min_damping_factor = 0.05
[]
[]
[Postprocessors]
[max_hoop_strain]
type = ElementExtremeValue
variable = strain_zz
block = 1
[]
[max_SED]
type = ElementExtremeValue
variable = SED
block = 1
[]
[average_grain_radius]
type = ElementAverageValue
block = 3
outputs = 'exodus'
variable = grain_radius
[]
[clad_inner_vol]
type = InternalVolume
boundary = 7
outputs = 'exodus'
execute_on = 'timestep_begin initial'
[]
[flux_from_clad]
type = SideDiffusiveFluxIntegral
variable = temp
boundary = 5
diffusivity = thermal_conductivity
outputs = 'exodus'
[]
[flux_from_fuel]
type = SideDiffusiveFluxIntegral
variable = temp
boundary = 10
diffusivity = thermal_conductivity
outputs = 'exodus'
[]
[rod_total_power]
type = ElementIntegralPower
variable = temp
fission_rate = fission_rate
block = 3
[]
[rod_input_power]
type = FunctionValuePostprocessor
function = linear_heat_rate_profile
scale_factor = 0.106
[]
[average_fission_rate]
type = ElementAverageValue
variable = fission_rate
block = '3'
[]
[RAE]
type = RadialAverageEnthalpy
vector_postprocessor = rad_temp
radial_direction = x
axial_direction = y
axial_position = 0.0503
temperature_name = temp
[]
[peak_RAE]
type = TimeExtremeValue
postprocessor = RAE
[]
[]
[VectorPostprocessors]
[rad_temp]
type = NodalValueSampler
block = 3
sort_by = y
variable = temp
execute_on = timestep_end
outputs = dummy
[]
[]
[StandardLWRFuelRodOutputs]
fuel_pellet_blocks = 3
cladding_blocks = 1
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[chkfile]
type = CSV
show = 'average_centerline_fuel_temperature average_fission_rate fission_gas_released_percentage peak_RAE rod_total_power'
execute_on = 'FINAL'
[]
[console]
type = Console
max_rows = 25
output_linear = true
[]
[dummy]
type = CSV
enable = false
[]
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-30/puzry-30.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-30.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 1300. '
y = '1.e+05 1.e+05 7.99e+06' # Linear increase at 0.2630 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 1300. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = EigenSolution
[]
[]
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = MaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = FunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = DirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = DirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1.e+11
poissons_ratio = 0.3
block = 1
[]
[creep_update]
type = ZryCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 1.e-04
temperature = temperature
temperature_standard_thermal_creep_end = 700
temperature_loca_creep_begin = 900.
[]
[creep]
type = ComputeMultipleInelasticStress
block = 1
tangent_operator = elastic
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = Density
block = 1
[]
[phase]
type = ZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
active = 'smp'
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0.
n_startup_steps = 1
end_time = 1300.
dtmax = 1.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-30_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(test/tests/thermalZry/thermal_test_IAEA.i)
# The mesh is a 1x1x1 cube (single element).
# The temperature is ramped on all faces of the cube from 300 K to 1200K
# over 100 Ms.
#
# Thermal conductivity and specific heat are computed using the pure Zry
# thermal model with the equations from the IAEA report IAEA-TECDOC-1496.
#
# The thermal conductivity and specific heat computed by BISON for the
# temperatures shown below and compared with analytical solution.
#
# The results are as follows:
# Thermal Conductivity Specific Heat
# ------------------------- ---------------------
# Analytical BISON Analytical BISON
# Temp(K) (W/m-K) (W/m-K) J/(kgK) J/(kgK)
# 300 13.412 13.412 286.38 286.38
# 608 15.757 15.757 317.92 317.92
# 905 19.631 19.631 348.33 1348.33
# 1202 25.091 25.091 1663.09 1663.09
# 1400 29.61 29.61 331.52 331.52
[Mesh]
[mesh]
type = GeneratedMeshGenerator
dim = 3
[]
[]
[Variables]
[T]
order = FIRST
family = LAGRANGE
initial_condition = 300
[]
[]
[AuxVariables]
[th_cond]
order = CONSTANT
family = MONOMIAL
[]
[cp]
order = CONSTANT
family = MONOMIAL
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = T
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = T
[]
[]
[AuxKernels]
[th_cond]
type = MaterialRealAux
variable = th_cond
property = thermal_conductivity
execute_on = 'initial linear'
[]
[cp]
type = MaterialRealAux
variable = cp
property = specific_heat
execute_on = 'initial linear'
[]
[]
[Functions]
[temp_ramp]
type = PiecewiseLinear
x = '0.0 100.e6'
y = '300 1400'
[]
[]
[BCs]
[VariableT]
type = FunctionDirichletBC
boundary = 'left right front back bottom top'
variable = T
function = temp_ramp
[]
[]
[Materials]
[thermal_clad]
type = ZryThermal
temperature = T
zry_thermal_properties_model = IAEA
[]
[density]
type = Density
density = 1200.0
[]
[]
[Executioner]
type = Transient
solve_type = PJFNK
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-ksp_gmres_restart'
petsc_options_value = '101'
line_search = 'none'
l_max_its = 100
nl_max_its = 100
nl_rel_tol = 1e-4
nl_abs_tol = 1e-6
l_tol = 1e-5
start_time = 0.0
end_time = 100.e6
dt = 1.0e6
[]
[Postprocessors]
[ave_temp_interior]
type = SideAverageValue
boundary = 'left right top bottom front back'
variable = T
execute_on = 'initial timestep_end'
[]
[avg_th_cond]
type = ElementAverageValue
variable = th_cond
execute_on = 'initial timestep_end'
[]
[avg_cp]
type = ElementAverageValue
variable = cp
execute_on = 'initial timestep_end'
[]
[average_fuel_T]
type = ElementAverageValue
variable = T
execute_on = 'initial timestep_end'
[]
[]
[Outputs]
exodus = true
[]
(assessment/LWR/validation/Super_Ramp/analysis/PK62/PK62_weighted_gap_VCP.i)
# This assessment case requires increasing the default automatic differentiation
# vector (AD size). At the time of writing, the default size is 50. This test
# requires, at least, 56. The minimum size required for a test to run can be
# specified in the 'assesment' file via "min_ad_size". To configure MOOSE
# to increase the AD vector size, one can use the command below in the MOOSE
# folder to expand this size, e.g., to 200:
#
# ./configure --with-derivative-type=sparse --with-ad-indexing-type=global --with-derivative-size=200
# physical constants
R = 8.3143 # J/mol*K -- THIS SHOULD BE EDITED TO USE PHYSICALCONSTANTS' VALUE
# fuel isotope fractions and fission energy
energy_per_fission = 3.28451e-11 # J/fission
isotope_fraction_U235 = 0.02985
isotope_fraction_U238 = 0.97015
isotope_fraction_Pu239 = 0.0
isotope_fraction_Pu240 = 0.0
isotope_fraction_Pu241 = 0.0
isotope_fraction_Pu242 = 0.0
# rod geometry
pellet_quantity = 29 # (-)
pellet_height = 0.010862 # m
pellet_outer_radius = 4.57e-3 # m
clad_gap_width = 75.0e-6 # m
clad_thickness = 0.725e-3 # m
clad_bot_gap_height = 1.0e-3 # m
bottom_clad_height = 15.5e-3 # m
top_clad_height = 15.5e-3 # m
clad_top_gap_height = 32.5e-3 # m
fuel_volume_ratio = 1.0 # (-)
rod_input_power_scale_factor = 0.376004 # m (rod height)
# variable and kernel initial values
initial_temperature = 293.15 # K
gravity_constant = -9.81 # m/s^2
# fuel/cladding contact
c_normal = 1e+05 # (-)
jump_distance_model = 'LANNING'
roughness_primary = 2e-6 # (-)
roughness_secondary = 1e-6 # (-)
roughness_coef = 3.2 # (-)
relocation_activation1 = 5000 # W/m
max_relocation_recovery_fraction = 0.5 # (-)
relocation_scaling_factor = 1 # (-)
# plenum parameters
initial_plenum_pressure = 2.25e6 # Pa
startup_time = 0 # s
# fuel/clad material properties
initial_fuel_density = 10420.0 # kg/m^3
initial_fuel_porosity = 0.049 # (-)
initial_grain_radius = 17.16e-6 # m
fuel_cracking_stress = 1.68e8 # Pa
fuel_shear_retention_factor = 0.1 # (-)
fuel_max_stress_correction = 0 # (-)
stress_free_temperature = 293.15 # K
cladding_density = 6550.0 # kg/m^3
# numerical options
damper_max_temperature_increment = 150.0 # K (was 30 K)
l_max_its = 35
l_tol = 1e-5
nl_max_its = 30
nl_rel_tol = 2e-6
nl_abs_tol = 1e-5
start_time = 0.0 # s
n_startup_steps = 1
dtmax = 1.0e6 # s
dtmin = 1.0 # s
Timestepper_dt = 100 # s
Timestepper_optimal_iterations = 15
Timestepper_iteration_window = 3
# irradiation history
end_time = 76630068.0 # s
# data files
power_history_data_file = 'alhr_history.csv'
axial_power_factors_data_file = 'axial_lhr_factors.csv'
clad_out_temp_data_file = 'temp_outer_clad_history.csv'
axial_temp_factors_data_file = 'axial_temp_factors.csv'
coolant_pressure_data_file = 'pressure_coolant.csv'
fast_neutron_flux_data_file = 'fast_neutron_flux.csv'
[GlobalParams]
density = ${initial_fuel_density}
displacements = 'disp_x disp_y'
order = FIRST
family = LAGRANGE
energy_per_fission = ${energy_per_fission}
volumetric_locking_correction = true
initial_porosity = ${initial_fuel_porosity}
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
[]
[Mesh]
coord_type = RZ
patch_size = 80
patch_update_strategy = iteration
[smeared_pellet_mesh]
type = FuelPinMeshGenerator
pellet_quantity = ${pellet_quantity}
pellet_height = ${pellet_height}
pellet_outer_radius = ${pellet_outer_radius}
pellet_mesh_density = customize
nx_p = 11
ny_p = 168
clad_mesh_density = customize
nx_c = 4
ny_c = 84
clad_gap_width = ${clad_gap_width}
clad_thickness = ${clad_thickness}
clad_bot_gap_height = ${clad_bot_gap_height}
bottom_clad_height = ${bottom_clad_height}
top_clad_height = ${top_clad_height}
clad_top_gap_height = ${clad_top_gap_height}
ny_cu = 3
ny_cl = 3
elem_type = QUAD4
[]
partitioner = centroid
centroid_partitioner_direction = y
[]
[Variables]
[temperature]
initial_condition = ${initial_temperature}
block = '1 3'
[]
[disp_x]
order = FIRST
family = LAGRANGE
block = '1 3'
scaling = 1.0e3
[]
[disp_y]
order = FIRST
family = LAGRANGE
block = '1 3'
scaling = 1.0e3
[]
[]
[Functions]
[power_history]
type = PiecewiseLinear
data_file = ${power_history_data_file}
format = columns
[]
[axial_power_factors]
type = PiecewiseBilinear
data_file = ${axial_power_factors_data_file}
axis = 1
[]
[clad_out_temp]
type = PiecewiseLinear
data_file = ${clad_out_temp_data_file}
format = columns
[]
[axial_temp_factors]
type = PiecewiseBilinear
data_file = ${axial_temp_factors_data_file}
axis = 1
[]
[clad_temp_bc]
type = CompositeFunction
functions = 'clad_out_temp axial_temp_factors'
[]
[coolant_pressure]
type = PiecewiseLinear
data_file = ${coolant_pressure_data_file}
format = columns
[]
[fast_flux]
type = PiecewiseLinear
data_file = ${fast_neutron_flux_data_file}
format = columns
[]
[axial_power_constant]
type = ConstantFunction
value = 1
[]
[]
[AuxVariables]
[fast_neutron_flux]
block = clad
[]
[fast_neutron_fluence]
block = clad
[]
[grain_radius]
block = pellet
initial_condition = ${initial_grain_radius}
[]
[porosity]
order = CONSTANT
family = MONOMIAL
block = pellet
initial_condition = ${initial_fuel_porosity}
[]
[pellet_id]
order = CONSTANT
family = MONOMIAL
block = pellet
[]
[oxide_thickness]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
block = clad
[]
[gas_gen_3]
order = CONSTANT
family = MONOMIAL
block = pellet
[]
[gas_grn_3]
order = CONSTANT
family = MONOMIAL
block = pellet
[]
[gas_bdr_3]
order = CONSTANT
family = MONOMIAL
block = pellet
[]
[gas_rel_3]
order = CONSTANT
family = MONOMIAL
block = pellet
[]
[bbl_bdr_2]
order = CONSTANT
family = MONOMIAL
block = pellet
[]
[prs_bbl_bdr]
order = CONSTANT
family = MONOMIAL
block = pellet
[]
[prseq_bbl_bdr]
order = CONSTANT
family = MONOMIAL
block = pellet
[]
[rad_bbl_bdr]
order = CONSTANT
family = MONOMIAL
block = pellet
[]
[GBCoverage]
order = CONSTANT
family = MONOMIAL
block = pellet
[]
[sat_coverage]
order = CONSTANT
family = MONOMIAL
block = pellet
[]
[eff_diff_coeff]
order = CONSTANT
family = MONOMIAL
block = pellet
[]
[deltav_v0_bd]
order = CONSTANT
family = MONOMIAL
block = pellet
[]
[gaseous_porosity]
order = CONSTANT
family = MONOMIAL
block = pellet
[]
[thermal_conductivity]
order = CONSTANT
family = MONOMIAL
block = pellet
[]
[gap_cond]
order = CONSTANT
family = MONOMIAL
[]
[layered_average_contact_pressure]
order = CONSTANT
family = MONOMIAL
[]
[volumetric_swelling_strain]
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[pellets]
block = pellet
temperature = temperature
strain = FINITE
eigenstrain_names = 'fuel_relocation_strain fuel_thermal_strain
fuel_volumetric_strain'
generate_output = 'vonmises_stress hydrostatic_stress stress_xx stress_yy
stress_zz strain_xx strain_yy strain_zz'
extra_vector_tags = 'ref'
[]
[clad]
block = clad
temperature = temperature
strain = FINITE
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
eigenstrain_names = 'clad_thermal_eigenstrain clad_irradiation_strain'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz
creep_strain_xx creep_strain_yy creep_strain_xy creep_strain_zz strain_xx
strain_yy strain_zz hoop_stress'
extra_vector_tags = 'ref'
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
extra_vector_tags = 'ref'
block = '1 3'
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
extra_vector_tags = 'ref'
block = '1 3'
[]
[heat_source]
type = NeutronHeatSource
variable = temperature
block = pellet
burnup_function = burnup
extra_vector_tags = 'ref'
[]
[gravity]
type = Gravity
variable = disp_y
value = ${gravity_constant}
[]
[]
[AuxKernels]
[fast_neutron_flux]
type = FastNeutronFluxAux
variable = fast_neutron_flux
block = clad
function = fast_flux
execute_on = timestep_begin
[]
[fast_neutron_fluence]
block = clad
type = FastNeutronFluenceAux
variable = fast_neutron_fluence
fast_neutron_flux = fast_neutron_flux
execute_on = timestep_begin
[]
[grain_radius]
type = GrainRadiusAux
block = pellet
variable = grain_radius
temperature = temperature
execute_on = linear
[]
[porosity]
type = PorosityAuxUO2
block = pellet
variable = porosity
execute_on = linear
[]
[pelletid]
type = PelletIdAux
block = pellet
variable = pellet_id
fuel_pin_geometry = pin_geometry
number_pellets = ${pellet_quantity}
execute_on = initial
[]
[oxi_thickness]
type = MaterialRealAux
variable = oxide_thickness
property = oxide_scale_thickness
boundary = 2
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fggen]
type = MaterialRealAux
variable = gas_gen_3
property = gas_concentration_generated_total
[]
[fggrn]
type = MaterialRealAux
variable = gas_grn_3
property = gas_concentration_intra_total
[]
[fgbdr]
type = MaterialRealAux
variable = gas_bdr_3
property = gas_concentration_GB_bubble_volume
[]
[fgrel]
type = MaterialRealAux
variable = gas_rel_3
property = gas_concentration_release_total
[]
[nbbl2]
type = MaterialRealAux
variable = bbl_bdr_2
property = bubble_GB_surface_density
[]
[prsbbl]
type = MaterialRealAux
variable = prs_bbl_bdr
property = bubble_GB_pressure
[]
[prseqbbl]
type = MaterialRealAux
variable = prseq_bbl_bdr
property = bubble_GB_pressure_equilibrium
[]
[radbbl]
type = MaterialRealAux
variable = rad_bbl_bdr
property = bubble_radius_GB
[]
[frcvrg]
type = MaterialRealAux
variable = GBCoverage
property = GBCoverage
[]
[stcvrg]
type = MaterialRealAux
variable = sat_coverage
property = sat_coverage
[]
[diffc]
type = MaterialRealAux
variable = eff_diff_coeff
property = eff_diff_coeff
[]
[dvv0bd]
type = MaterialRealAux
variable = deltav_v0_bd
property = deltav_v0_bubble_GB
[]
[gaspor]
type = MaterialRealAux
variable = gaseous_porosity
property = gaseous_porosity
[]
[fuel_conductivity]
type = MaterialRealAux
variable = thermal_conductivity
property = thermal_conductivity
[]
[layered_average_contact_pressure]
type = SpatialUserObjectAux
block = pellet
variable = layered_average_contact_pressure
execute_on = nonlinear
user_object = layered_average_contact_pressure
[]
[volumetric_swelling_strain]
type = MaterialRealAux
variable = volumetric_swelling_strain
property = volumetric_swelling_strain
block = pellet
execute_on = nonlinear
[]
[]
[Burnup]
[burnup]
block = pellet
fuel_volume_ratio = ${fuel_volume_ratio}
rod_ave_lin_pow = power_history
axial_power_profile = axial_power_factors
num_radial = 80
num_axial = 20
isotopes = 'U235 U238 Pu239 Pu240 Pu241 Pu242'
isotope_fractions = '${isotope_fraction_U235} ${isotope_fraction_U238} ${isotope_fraction_Pu239} ${isotope_fraction_Pu240} ${isotope_fraction_Pu241} ${isotope_fraction_Pu242}'
RPF = RPF
fuel_pin_geometry = pin_geometry
[]
[]
[Contact]
[mechanical]
model = frictionless
formulation = mortar
primary = 5
secondary = 10
c_normal = ${c_normal}
[]
[]
[ThermalContactMortar]
[thermal]
secondary_variable = temperature
primary_boundary = 5
secondary_boundary = 10
initial_moles = initial_moles
gas_released = fission_gas_released
jump_distance_model = ${jump_distance_model}
plenum_pressure = plenum_pressure
roughness_primary = ${roughness_primary}
roughness_secondary = ${roughness_secondary}
roughness_coef = ${roughness_coef}
contact_pressure = mechanical_normal_lm
layer_thickness = layer_thickness_action
[]
[]
[PlenumTemperature]
[plenum_temp]
boundary = 5
inner_surfaces = 5
outer_surfaces = 10
temperature = temperature
[]
[]
[BCs]
[no_x_all]
type = DirichletBC
variable = disp_x
boundary = 12
value = 0.0
[]
[no_y_clad_bottom]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[]
[no_y_fuel_bottom]
type = DirichletBC
variable = disp_y
boundary = 1020
value = 0.0
[]
[temp]
type = FunctionDirichletBC
boundary = '1 2 3'
variable = temperature
function = clad_temp_bc
[]
[Pressure]
[coolantPressure]
boundary = '1 2 3'
function = coolant_pressure
[]
[]
[PlenumPressure]
[plenumPressure]
boundary = 9
initial_pressure = ${initial_plenum_pressure}
startup_time = ${startup_time}
R = ${R}
output_initial_moles = initial_moles
temperature = plenum_temp
volume = plenum_volume
material_input = fission_gas_released
output = plenum_pressure
[]
[]
[]
[Materials]
[fuel_thermal]
type = UO2Thermal
block = pellet
thermal_conductivity_model = NFIR
temperature = temperature
burnup_function = burnup
[]
[fuel_volumetric_swelling]
type = UO2VolumetricSwellingEigenstrain
gas_swelling_model_type = SIFGRS
block = pellet
temperature = temperature
burnup_function = burnup
initial_fuel_density = ${initial_fuel_density}
eigenstrain_name = fuel_volumetric_strain
[]
[fuel_elasticity_tensor]
type = UO2ElasticityTensor
block = pellet
density = ${initial_fuel_density}
temperature = temperature
matpro_youngs_modulus = true
matpro_poissons_ratio = true
[]
[fuel_creep]
type = UO2CreepUpdate
block = pellet
temperature = temperature
burnup_function = burnup
initial_grain_radius = ${initial_grain_radius}
[]
[fuel_stress]
type = ComputeSmearedCrackingStress
block = pellet
cracking_stress = ${fuel_cracking_stress}
inelastic_models = 'fuel_creep'
softening_models = exponential_softening
shear_retention_factor = ${fuel_shear_retention_factor}
max_stress_correction = ${fuel_max_stress_correction}
cracked_elasticity_type = DIAGONAL
output_properties = crack_damage
outputs = exodus
[]
[exponential_softening]
type = ExponentialSoftening
[]
[fuel_relocation]
type = UO2RelocationEigenstrain
block = pellet
burnup_function = burnup
rod_ave_lin_pow = power_history
axial_power_profile = axial_power_factors
relocation_activation1 = ${relocation_activation1}
relocation_model = ESCORE_modified
eigenstrain_name = fuel_relocation_strain
fuel_pin_geometry = pin_geometry
model_relocation_recovery = true
max_relocation_recovery_fraction = ${max_relocation_recovery_fraction}
relocation_scaling_factor = ${relocation_scaling_factor}
volumetric_swelling_increment = vol_swell_increment
layered_average_contact_pressure = layered_average_contact_pressure
outputs = all
output_properties = 'relocation_strain recovered_relocation_strain'
[]
[fuel_thermal_expansion]
type = UO2ThermalExpansionMATPROEigenstrain
block = pellet
temperature = temperature
stress_free_temperature = ${stress_free_temperature}
eigenstrain_name = fuel_thermal_strain
[]
[fission_gas_release]
type = UO2Sifgrs
block = pellet
hydrostatic_stress = hydrostatic_stress
diff_coeff_option = TURNBULL_D1_4D2_D3
transient_option = MICROCRACKING_BURNUP
res_param_option = HETEROGENEOUS_WHITE
ig_bubble_model = NUCLEATION_RESOLUTION
ig_diff_algorithm = polypole2
temperature = temperature
burnup_function = burnup
grain_radius = grain_radius
gbs_model = true
pellet_id = pellet_id
pellet_brittle_zone = pbz
ath_model = true
rod_ave_lin_pow = power_history
axial_power_profile = axial_power_factors
[]
[fuel_density]
type = Density
block = pellet
[]
[clad_thermal]
type = ZryThermal
block = clad
temperature = temperature
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = clad
fast_neutron_fluence = fast_neutron_fluence
temperature = temperature
matpro_youngs_modulus = true
matpro_poissons_ratio = true
[]
[clad_stress]
type = ComputeMultipleInelasticStress
tangent_operator = nonlinear
inelastic_models = 'clad_zrycreep'
block = clad
[]
[clad_zrycreep]
type = ZryCreepLimbackHoppeUpdate
block = clad
temperature = temperature
fast_neutron_flux = fast_neutron_flux
fast_neutron_fluence = fast_neutron_fluence
model_irradiation_creep = true
model_primary_creep = true
model_thermal_creep = true
[]
[thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = clad
temperature = temperature
stress_free_temperature = ${stress_free_temperature}
eigenstrain_name = clad_thermal_eigenstrain
[]
[irradiation_swelling]
type = ZryIrradiationGrowthEigenstrain
block = clad
fast_neutron_fluence = fast_neutron_fluence
zircaloy_material_type = stress_relief_annealed
eigenstrain_name = clad_irradiation_strain
[]
[clad_density]
type = Density
block = clad
density = ${cladding_density}
[]
[clad_oxidation]
type = ZryOxidation
boundary = 2
temperature = temperature
normal_operating_temperature_model = epri_kwu_ce
high_temperature_model = leistikow
fuel_pin_geometry = pin_geometry
[]
[]
#### This is the part where VCP is set up
[Preconditioning]
[vcp]
type = VCP
full = true
# condense out the normal LM from mechanical contact and the LM from thermal contact
lm_variable = 'mechanical_normal_lm thermal_thermal_lm'
primary_variable = 'disp_x temperature'
# we use LU to solve the system after condensation
# AMG and other solver types have shown convergence for simpler mechanical/thermo-mechanical contact problems but has not luck with this one
preconditioner = 'LU'
is_lm_coupling_diagonal = true
adaptive_condensation = true
[]
[]
[Dampers]
[maxincrement]
type = MaxIncrement
max_increment = ${damper_max_temperature_increment}
variable = temperature
[]
[]
[Debug]
show_var_residual_norms = true
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_converged_reason -ksp_converged_reason'
# IMPORTANT: we should not specify the pc_type below, otherwise the VCP setting will be overriden
petsc_options_iname = ' -mat_mffd_err -pc_factor_shift_type -pc_factor_shift_amount'
petsc_options_value = ' 1e-5 NONZERO 1e-15'
snesmf_reuse_base = false
line_search = 'none'
verbose = true
l_max_its = ${l_max_its}
l_tol = ${l_tol}
nl_max_its = ${nl_max_its}
nl_rel_tol = ${nl_rel_tol}
nl_abs_tol = ${nl_abs_tol}
start_time = ${start_time}
n_startup_steps = ${n_startup_steps}
end_time = ${end_time}
dtmax = ${dtmax}
dtmin = ${dtmin}
[TimeStepper]
type = IterationAdaptiveDT
dt = ${Timestepper_dt}
optimal_iterations = ${Timestepper_optimal_iterations}
iteration_window = ${Timestepper_iteration_window}
timestep_limiting_function = power_history
force_step_every_function_point = true
[]
[]
[Postprocessors]
[avg_gap_conductance]
type = SideAverageValue
boundary = 10
variable = gap_cond
execute_on = 'initial timestep_end'
[]
[max_fuel_temp]
type = NodalExtremeValue
block = pellet
value_type = max
variable = temperature
execute_on = 'initial timestep_end'
[]
[max_clad_temp]
type = NodalExtremeValue
block = clad
value_type = max
variable = temperature
execute_on = 'initial timestep_end'
[]
[total_rod_integral_power]
type = ElementIntegralPower
variable = temperature
burnup_function = burnup
block = pellet
[]
[total_rod_input_power]
type = FunctionValuePostprocessor
function = power_history
scale_factor = ${rod_input_power_scale_factor}
[]
[vol_swell_increment]
type = SideAverageIncrementTensorComponent
boundary = 10
variable = volumetric_swelling_strain
execute_on = nonlinear
[]
[contact_dof]
type = ContactDOFSetSize
variable = 'mechanical_normal_lm'
subdomain = 'secondary_lower'
execute_on = 'nonlinear timestep_end'
[]
[nl_its]
type = NumNonlinearIterations
[]
[total_nl_its]
type = CumulativeValuePostprocessor
postprocessor = nl_its
[]
[l_its]
type = NumLinearIterations
[]
[total_l_its]
type = CumulativeValuePostprocessor
postprocessor = l_its
[]
[]
[StandardLWRFuelRodOutputs]
fuel_pellet_blocks = 3
[]
[Outputs]
perf_graph = true
csv = true
exodus = true
color = false
[console]
type = Console
max_rows = 25
[]
[chkfile]
type = CSV
show = 'average_burnup fission_gas_released_percentage'
execute_on = 'FINAL'
[]
[]
[VectorPostprocessors]
[temperature_post]
type = NodalValueSampler
variable = temperature
boundary = '10'
sort_by = y
[]
[contact_post]
type = NodalValueSampler
variable = mechanical_normal_lm
boundary = '10'
sort_by = y
[]
[disp_x]
type = NodalValueSampler
variable = disp_x
boundary = '10'
sort_by = y
[]
[disp_y]
type = NodalValueSampler
variable = disp_y
boundary = '10'
sort_by = y
[]
[]
[UserObjects]
[pin_geometry]
type = FuelPinGeometry
[]
[pbz]
type = PelletBrittleZone
block = pellet
pellet_id = pellet_id
temperature = temperature
fuel_pin_geometry = pin_geometry
number_pellets = ${pellet_quantity}
execute_on = 'initial linear'
[]
[layered_average_contact_pressure]
type = LayeredSideAverage
variable = mechanical_normal_lm
direction = y
num_layers = 1
execute_on = timestep_end
boundary = 10
[]
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-19/puzry-19.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-19.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 2000. '
y = '1.e+05 1.e+05 2.53e+06' # Linear increase at 0.0243 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 2000. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = EigenSolution
[]
[]
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = MaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = FunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = DirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = DirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1.e+11
poissons_ratio = 0.3
block = 1
[]
[creep_update]
type = ZryCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 1.e-04
temperature = temperature
temperature_standard_thermal_creep_end = 700
temperature_loca_creep_begin = 900.
[]
[creep]
type = ComputeMultipleInelasticStress
block = 1
tangent_operator = elastic
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = Density
block = 1
[]
[phase]
type = ZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
active = 'smp'
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0.
n_startup_steps = 1
end_time = 2000.
dtmax = 1.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-19_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-23/puzry-23.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-23.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 2500. '
y = '1.e+05 1.e+05 1.0855e+07' # Linear increase at 0.0717 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 2500. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = EigenSolution
[]
[]
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = MaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = FunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = DirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = DirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1.e+11
poissons_ratio = 0.3
block = 1
[]
[creep_update]
type = ZryCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 1.e-04
temperature = temperature
temperature_standard_thermal_creep_end = 700
temperature_loca_creep_begin = 900.
[]
[creep]
type = ComputeMultipleInelasticStress
block = 1
tangent_operator = elastic
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = Density
block = 1
[]
[phase]
type = ZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
active = 'smp'
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0.
n_startup_steps = 1
end_time = 2500.
dtmax = 1.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-23_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-03/puzry-03.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-03.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 2000. '
y = '1.e+05 1.e+05 7.3e+05' # Linear increase at 0.0063 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 2000. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = EigenSolution
[]
[]
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = MaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = FunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = DirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = DirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1.e+11
poissons_ratio = 0.3
block = 1
[]
[creep_update]
type = ZryCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 1.e-04
temperature = temperature
temperature_standard_thermal_creep_end = 700
temperature_loca_creep_begin = 900.
[]
[creep]
type = ComputeMultipleInelasticStress
block = 1
tangent_operator = elastic
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = Density
block = 1
[]
[phase]
type = ZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
active = 'smp'
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0.
n_startup_steps = 1
end_time = 2000.
dtmax = 1.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-03_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/LOCA_ANL_cladding_burst_tests/analysis/OCL11/OCL11_aniso.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
displacements = 'disp_x disp_y'
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
[]
[Mesh]
coord_type = RZ
[smeared_pellet_mesh]
type = FuelPinMeshGenerator
pellet_quantity = 1
pellet_height = 0.270
pellet_outer_radius = 4.78e-3
clad_bot_gap_height = 0.001
clad_top_gap_height = 0.013
clad_thickness = 0.71e-3
clad_gap_width = 0.1e-3
pellet_mesh_density = coarse
clad_mesh_density = coarse
elem_type = QUAD8
[]
patch_size = 10
patch_update_strategy = auto
partitioner = centroid
centroid_partitioner_direction = y
[]
[Variables]
[temperature]
initial_condition = 300.0
[]
[]
[Functions]
[temperature_func]
type = PiecewiseLinear
x = '0 496.02 520.74 528.12 545.94 551.28 671.52 885.3 1195.74 1410.36 1657.86 1680 1690 1700 1710 1720 1730 1740 1750 1760 1770 1780 1790 1800 1810 1820 1830 1840 1848'
y = '300 300 405.465 482.048 583.351 632.287 634.297 632.825 630.378 631.059 632.59 633 683 733 783 833 883 933 983 1033 1083 1133 1183 1233 1283 1333 1383 1433 1477'
[]
[temperature_profile]
type = PiecewiseBilinear
data_file = 'temp_profile.csv'
axis = 1
[]
[cladding_temperature]
type = CompositeFunction
functions = 'temperature_func temperature_profile'
[]
# Circumferential steady-state creep test and analysis of Zircaloy-4 fuelcladding
# Nuclear Engineering and Design, 53, 2312-2322 (2021)
[F]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.738 0.57 0.57'
[]
[G]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.174 0.45 0.45'
[]
[H]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.588 0.48 0.48'
[]
[L]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[M]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[N]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[pellets]
block = pellet
use_automatic_differentiation = true
add_variables = true
strain = FINITE
decomposition_method = TaylorExpansion
eigenstrain_names = 'fuel_thermal_strain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
generate_output = 'vonmises_stress hydrostatic_stress stress_xx stress_yy
stress_zz strain_xx strain_yy strain_zz hoop_stress'
extra_vector_tags = 'ref'
[]
[clad]
block = clad
use_automatic_differentiation = true
add_variables = true
strain = FINITE
decomposition_method = TaylorExpansion
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz hoop_stress'
extra_vector_tags = 'ref'
[]
[]
[AuxVariables]
[creep_rate_aux]
order = CONSTANT
family = MONOMIAL
block = clad
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
block = clad
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
block = clad
[]
[scale_thickness]
order = CONSTANT
family = MONOMIAL
block = clad
[]
[oxywtfract_total]
order = CONSTANT
family = MONOMIAL
block = clad
[]
[oxywtfgain_total]
order = CONSTANT
family = MONOMIAL
block = clad
[]
[burst_stress]
order = CONSTANT
family = MONOMIAL
block = clad
[]
[burst]
order = CONSTANT
family = MONOMIAL
block = clad
[]
[]
[Kernels]
[heat]
type = ADHeatConduction
variable = temperature
extra_vector_tags = 'ref'
[]
[heat_ie]
type = ADHeatConductionTimeDerivative
variable = temperature
extra_vector_tags = 'ref'
[]
[]
[AuxKernels]
[creep_rate_aux]
type = ADMaterialRealAux
variable = creep_rate_aux
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = ADMaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
block = clad
[]
[scl_thickness]
type = ADMaterialRealAux
variable = scale_thickness
property = oxide_scale_thickness
boundary = clad_outside_right
[]
[ofract_total]
type = ADMaterialRealAux
variable = oxywtfract_total
property = current_oxygen_weight_frac_total
boundary = clad_outside_right
[]
[ofgain_total]
type = ADMaterialRealAux
boundary = clad_outside_right
variable = oxywtfgain_total
property = oxygen_weight_frac_gained_total
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = clad_outside_right
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = clad_outside_right
execute_on = timestep_end
[]
[]
[ThermalContact]
[thermal_contact]
type = GapHeatTransfer
primary = 5
secondary = 10
variable = temperature
gap_conductivity = 0.15 # k of He per Netzsch
[]
[]
[BCs]
[clad_surface_temperature]
type = ADFunctionDirichletBC
variable = temperature
boundary = '2'
function = cladding_temperature
[]
[no_x_all]
type = ADDirichletBC
variable = disp_x
boundary = 12
value = 0.0
[]
[no_y_clad_bottom]
type = ADDirichletBC
variable = disp_y
boundary = '1'
value = 0.0
[]
[no_y_fuel_bottom]
type = ADDirichletBC
variable = disp_y
boundary = '1020'
value = 0.0
[]
[Pressure]
[outer_pressure]
boundary = '1 2 3'
factor = 101325
[]
[inner_pressure]
boundary = '4 5 6'
factor = 8.28e6
[]
[]
[]
[PlenumTemperature]
[plenum_temp]
boundary = 5
inner_surfaces = '5'
outer_surfaces = '10'
temperature = temperature
[]
[]
[CoolantChannel]
[convective_clad_surface]
boundary = 2
variable = temperature
inlet_temperature = 473.0
inlet_pressure = 101325
inlet_massflux = 1.0 # kg/m^2-sec # almost stagnant steam
rod_diameter = 0.01118
rod_pitch = 1.26e-02 # default
oxide_thickness = scale_thickness
thermal_conductivity = reg_thermal_conductivity
[]
[]
[Materials]
[fuel_thermal]
type = ADHeatConductionMaterial
block = pellet
thermal_conductivity = 3.5
specific_heat = 330.0
[]
[fuel_converter]
type = MaterialADConverter
block = pellet
ad_props_in = 'thermal_conductivity'
reg_props_out = 'reg_thermal_conductivity'
[]
[fuel_elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
block = pellet
youngs_modulus = 2.0e11
poissons_ratio = 0.345
[]
[fuel_elastic_stress]
type = ADComputeFiniteStrainElasticStress
block = pellet
[]
[fuel_thermal_expansion]
type = ADComputeThermalExpansionEigenstrain
block = pellet
thermal_expansion_coeff = 10.0e-6
temperature = temperature
stress_free_temperature = 300.0
eigenstrain_name = fuel_thermal_strain
[]
[fuel_density]
type = ADDensity
block = pellet
density = 10980.0 #perfectly dense UO2
[]
[clad_thermal]
type = ADZryThermal
block = clad
temperature = temperature
[]
[clad_converter]
type = MaterialADConverter
block = clad
ad_props_in = 'thermal_conductivity'
reg_props_out = 'reg_thermal_conductivity'
[]
[clad_elasticity_tensor]
type = ADZryElasticityTensor
block = clad
matpro_youngs_modulus = false
matpro_poissons_ratio = false
[]
[clad_stress]
type = ADComputeMultipleInelasticStress
inelastic_models = 'clad_zrycreep'
block = clad
[]
[hill_constants]
type = ADHillConstants
#hill_constants = "0.5 0.5 0.5 1.0 1.0 1.0"
hill_constants = "0.738 0.174 0.588 1.0 1.0 1.0"
function_names = "F G H L M N"
[]
[clad_zrycreep]
type = ADZryAnisoCreepLOCAUpdate
block = clad
temperature = temperature
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
temperature_loca_creep_begin = 501
temperature_standard_thermal_creep_end = 500
fract_beta_phase_name = 'ad_fract_beta_phase'
[]
[thermal_expansion]
type = ADZryThermalExpansionMATPROEigenstrain
block = clad
temperature = temperature
stress_free_temperature = 300.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[clad_density]
type = ADDensity
block = clad
density = 6550.0
[]
[phase]
type = ZrPhase
block = clad
temperature = temperature
numerical_method = 2
[]
[phase_converter]
type = MaterialADConverter
block = clad
reg_props_in = 'fract_beta_phase'
ad_props_out = 'ad_fract_beta_phase'
[]
[oxidation]
type = ADZryOxidation
boundary = clad_outside_right
temperature = temperature
clad_inner_radius = 4.88e-3 #checked
clad_outer_radius = 5.59e-3 #checked
normal_operating_temperature_model = epri_kwu_ce
high_temperature_model = leistikow
use_coolant_channel = true
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = clad_outside_right
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate_aux
temperature = temperature
fraction_beta_phase = fract_beta_phase
fraction_oxygen_gain = oxywtfgain_total
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
verbose = true
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.0e-04
nl_abs_tol = 1.0e-08
start_time = 0
n_startup_steps = 1
end_time = 1800.0
dtmax = 100
dtmin = 0.0001
[TimeStepper]
type = IterationAdaptiveDT
timestep_limiting_postprocessor = material_timestep
dt = 10.0
time_dt = '100 10'
time_t = '10 400'
[]
[]
[Postprocessors]
[ave_clad_temp]
type = SideAverageValue
boundary = clad_outside_right
variable = temperature
[]
[gas_volume]
type = InternalVolume
boundary = 9
execute_on = 'initial linear'
[]
[max_clad_temp]
type = NodalExtremeValue
block = clad
value_type = max
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = clad
[]
[max_oxygen_fract]
type = ElementExtremeValue
block = clad
value_type = max
variable = oxywtfract_total
[]
[max_betaph_fract]
type = ElementExtremeValue
block = clad
value_type = max
variable = fract_beta_phase
[]
[max_hoop_stress]
type = ElementExtremeValue
block = clad
value_type = max
variable = hoop_stress
[]
[vonmises_stress_clad]
type = ElementAverageValue
block = clad
variable = vonmises_stress
[]
[min_burst_stress]
type = ElementExtremeValue
block = clad
value_type = min
variable = burst_stress
[]
[burst]
type = ElementExtremeValue
block = clad
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = clad
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[oxide_thickness]
type = ElementAverageValue
block = clad
variable = scale_thickness
execute_on = TIMESTEP_END
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
[]
[PerformanceMetricOutputs]
[]
[Outputs]
exodus = true
csv = true
color = false
perf_graph = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
show = 'max_clad_temp max_hoop_stress vonmises_stress_clad'
execute_on = 'FINAL'
[]
[]
[UserObjects]
[terminator1]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
[]
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-31/puzry-31_aniso.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-31.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 1400. '
y = '1.e+05 1.e+05 7.944e+06' # Linear increase at 0.1961 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 1400. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
# Circumferential steady-state creep test and analysis of Zircaloy-4 fuel cladding
# Nuclear Engineering and Design, 53, 2312-2322 (2021)
[F]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.738 0.738 0.57'
[]
[G]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.174 0.174 0.45'
[]
[H]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.588 0.588 0.48'
[]
[L]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[M]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[N]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = TaylorExpansion
use_automatic_differentiation = true
[]
[]
[]
[]
[Kernels]
[heat]
type = ADHeatConduction
variable = temperature
[]
[heat_ie]
type = ADHeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = ADMaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = ADMaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = ADMaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = ADMaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = ADMaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = ADFunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = ADDirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = ADDirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ADZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1.e+11
poissons_ratio = 0.3
block = 1
[]
[hill_constants]
type = ADHillConstants
hill_constants = "0.738 0.174 0.588 1.0 1.0 1.0"
function_names = "F G H L M N"
temperature = temperature
[]
[creep_update]
type = ADZryAnisoCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 1.5e-05
temperature = temperature
temperature_standard_thermal_creep_end = 700
temperature_loca_creep_begin = 900.
fract_beta_phase_name = 'fract_beta_phase'
max_integration_error = 1000000.0
absolute_tolerance = 1e-13
relative_tolerance = 1e-11
[]
[creep]
type = ADComputeMultipleInelasticStress
block = 1
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ADZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = ADDensity
block = 1
[]
[phase]
type = ADZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ADZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = NEWTON
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-07
start_time = 0.
n_startup_steps = 1
end_time = 2500.
dtmax = 1.
dtmin = 1.0e-9
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-31_aniso_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-07/puzry-07.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-07.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 1300. '
y = '1.e+05 1.e+05 2.377e+06' # Linear increase at 0.0759 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 1300. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = EigenSolution
[]
[]
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = MaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = FunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = DirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = DirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1.e+11
poissons_ratio = 0.3
block = 1
[]
[creep_update]
type = ZryCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 1.e-04
temperature = temperature
temperature_standard_thermal_creep_end = 700
temperature_loca_creep_begin = 900.
[]
[creep]
type = ComputeMultipleInelasticStress
block = 1
tangent_operator = elastic
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = Density
block = 1
[]
[phase]
type = ZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
active = 'smp'
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0.
n_startup_steps = 1
end_time = 1300.
dtmax = 1.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-07_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/LOCA_REBEKA_cladding_burst_tests/analysis/rebeka_2d_01MPa/rebeka_singlerod_2d_01MPa_aniso.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
order = SECOND
family = LAGRANGE
displacements = 'disp_x disp_y'
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = rebeka_singlerod.e
[]
[]
[Variables]
[temperature]
initial_condition = 573.0
[]
[]
[Functions]
[temperature_func]
type = PiecewiseLinear
x = '0. 700. '
y = '573. 1273.' # From 300 to 1000 C at 1 K/s
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 700. '
y = '1.e+06 1.e+06' # 10 bar
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 700. '
y = '1.e+05 1.e+05' # atmospheric pressure
[]
# Circumferential steady-state creep test and analysis of Zircaloy-4 fuel cladding
# Nuclear Engineering and Design, 53, 2312-2322 (2021)
[F]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.738 0.738 0.57'
[]
[G]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.174 0.174 0.45'
[]
[H]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.588 0.588 0.48'
[]
[L]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[M]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[N]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[clad]
block = cladding
add_variables = true
strain = FINITE
decomposition_method = TaylorExpansion
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz hoop_stress'
use_automatic_differentiation = true
[]
[]
[AuxVariables]
[creep_rate_aux]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[scale_thickness]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfract_total]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfgain_total]
order = CONSTANT
family = MONOMIAL
[]
[burst_stress]
order = CONSTANT
family = MONOMIAL
[]
[burst]
order = CONSTANT
family = MONOMIAL
[]
[]
[Kernels]
[heat]
type = ADHeatConduction
variable = temperature
[]
[heat_ie]
type = ADHeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate_aux]
type = ADMaterialRealAux
variable = creep_rate_aux
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = ADMaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = ADMaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[scl_thickness]
type = ADMaterialRealAux
variable = scale_thickness
property = oxide_scale_thickness
boundary = 2
[]
[ofract_total]
type = ADMaterialRealAux
variable = oxywtfract_total
property = current_oxygen_weight_frac_total
boundary = 2
[]
[ofgain_total]
type = ADMaterialRealAux
boundary = 2
variable = oxywtfgain_total
property = oxygen_weight_frac_gained_total
[]
[sigmaburst]
type = ADMaterialRealAux
variable = burst_stress
property = burst_stress
boundary = 2
[]
[hasburst]
type = ADMaterialRealAux
variable = burst
property = failed
boundary = 2
execute_on = timestep_end
[]
[]
[BCs]
[inner_temperature]
type = REBEKADirichletBC
variable = temperature
function_tempm = temperature_func
minimum_temperature = 573.
translation = 0.1625
boundary = 4
[]
[no_y_midsection]
type = ADDirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply steam pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 101 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[CoolantChannel]
[convective_clad_surface]
boundary = 2
variable = temperature
inlet_temperature = 473.
inlet_pressure = 1.e+05
inlet_massflux = 1.0 # kg/m^2-sec # almost stagnant steam
rod_diameter = 10.75e-03
rod_pitch = 1.26e-02 # default
oxide_thickness = scale_thickness
number_axial_zone = 15
use_ad = true
[]
[]
[Materials]
[thermal]
type = ADZryThermal
block = cladding
temperature = temperature
[]
[clad_elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
block = cladding
youngs_modulus = 1.0e11
poissons_ratio = 0.3
[]
[clad_stress]
type = ADComputeMultipleInelasticStress
inelastic_models = 'clad_zrycreep'
block = cladding
[]
[hill_constants]
type = ADHillConstants
hill_constants = "0.738 0.174 0.588 1.0 1.0 1.0"
function_names = "F G H L M N"
temperature = temperature
[]
[clad_zrycreep]
type = ADZryAnisoCreepLOCAUpdate
block = cladding
temperature = temperature
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
temperature_loca_creep_begin = 501
temperature_standard_thermal_creep_end = 500
fract_beta_phase_name = 'fract_beta_phase'
[]
[thermal_expansion]
type = ADZryThermalExpansionMATPROEigenstrain
block = cladding
temperature = temperature
stress_free_temperature = 573.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[density]
type = ADDensity
block = cladding
[]
[phase]
type = ADZrPhase
block = cladding
temperature = temperature
numerical_method = 2
[]
[oxidation]
type = ADZryOxidation
boundary = 2
temperature = temperature
clad_inner_radius = 0.00465
clad_outer_radius = 0.005375
normal_operating_temperature_model = epri_kwu_ce
high_temperature_model = leistikow
use_coolant_channel = true
[]
[clad_failure_criterion]
type = ADZryCladdingFailure
boundary = 2
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate_aux
temperature = temperature
fraction_beta_phase = fract_beta_phase
fraction_oxygen_gain = oxywtfgain_total
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = NEWTON
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-06
nl_abs_tol = 1.e-08
start_time = 0
n_startup_steps = 1
end_time = 700.
dtmax = 1.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[Postprocessors]
[ave_clad_exterior_temp]
type = SideAverageValue
boundary = 2
variable = temperature
[]
[max_clad_temp]
type = NodalExtremeValue
block = cladding
value_type = max
variable = temperature
[]
[min_clad_temp]
type = NodalExtremeValue
block = cladding
value_type = min
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = cladding
[]
[max_oxygen_fract]
type = ElementExtremeValue
block = cladding
value_type = max
variable = oxywtfract_total
[]
[max_betaph_fract]
type = ElementExtremeValue
block = cladding
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
block = cladding
value_type = max
variable = creep_rate_aux
[]
[max_creep_strain_mag]
type = ElementExtremeValue
block = cladding
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
block = cladding
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
block = cladding
value_type = max
variable = hoop_stress
[]
[vonmises_stress_clad]
type = ElementAverageValue
block = cladding
variable = vonmises_stress
[]
[min_burst_stress]
type = ElementExtremeValue
block = cladding
value_type = min
variable = burst_stress
[]
[burst]
type = ElementExtremeValue
block = cladding
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = cladding
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[top_disp_r_clad] # this is mid height
type = NodalVariableValue
variable = disp_x
nodeid = 0 #coords (0.005375, 0.1625)
[]
[top_disp_r_clad_slice] # this is mid height matched to the 1.5d
type = NodalVariableValue
variable = disp_x
nodeid = 3 #coords (0.005375, 0.1625)
[]
[top_disp_z_clad]
type = NodalVariableValue
variable = disp_y
nodeid = 0 #coords (0.005375, 0.1625)
[]
[stress_xx] # stess in the top Element
type = ElementalVariableValue
variable = stress_xx
elementid = 0
[]
[stress_yy] # stess in the top Element
type = ElementalVariableValue
variable = stress_yy
elementid = 0
[]
[stress_zz] # stess in the top Element
type = ElementalVariableValue
variable = stress_zz
elementid = 0
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = cladding
plenum_boundary_name = 4
external_clad_boundary_name = 2
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = rebeka_2d_01MPa_aniso_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-31/puzry-31.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-31.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 1400. '
y = '1.e+05 1.e+05 7.944e+06' # Linear increase at 0.1961 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 1400. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = EigenSolution
[]
[]
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = MaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = FunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = DirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = DirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1.e+11
poissons_ratio = 0.3
block = 1
[]
[creep_update]
type = ZryCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 1.e-04
temperature = temperature
temperature_standard_thermal_creep_end = 700
temperature_loca_creep_begin = 900.
[]
[creep]
type = ComputeMultipleInelasticStress
block = 1
tangent_operator = elastic
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = Density
block = 1
[]
[phase]
type = ZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
active = 'smp'
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0.
n_startup_steps = 1
end_time = 1400.
dtmax = 1.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-31_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-25/puzry-25.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-25.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 6000. '
y = '1.e+05 1.e+05 8.75e+06' # Linear increase at 0.0173 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 6000. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = EigenSolution
[]
[]
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = MaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = FunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = DirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = DirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1.e+11
poissons_ratio = 0.3
block = 1
[]
[creep_update]
type = ZryCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 1.e-04
temperature = temperature
temperature_standard_thermal_creep_end = 700
temperature_loca_creep_begin = 900.
[]
[creep]
type = ComputeMultipleInelasticStress
block = 1
tangent_operator = elastic
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = Density
block = 1
[]
[phase]
type = ZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
active = 'smp'
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0.
n_startup_steps = 1
end_time = 6000.
dtmax = 1.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-25_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-16/puzry-16.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-16.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 2000. '
y = '1.e+05 1.e+05 1.234e+07' # Linear increase at 0.1224 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 2000. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = EigenSolution
[]
[]
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = MaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = FunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = DirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = DirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1.e+11
poissons_ratio = 0.3
block = 1
[]
[creep_update]
type = ZryCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 1.e-04
temperature = temperature
temperature_standard_thermal_creep_end = 700
temperature_loca_creep_begin = 900.
[]
[creep]
type = ComputeMultipleInelasticStress
block = 1
tangent_operator = elastic
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = Density
block = 1
[]
[phase]
type = ZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
active = 'smp'
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0.
n_startup_steps = 1
end_time = 2000.
dtmax = 1.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-16_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/LOCA_REBEKA_cladding_burst_tests/analysis/rebeka_2d_14MPa/rebeka_singlerod_2d_14MPa_aniso.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
order = SECOND
family = LAGRANGE
displacements = 'disp_x disp_y'
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = rebeka_singlerod.e
[]
[]
[Variables]
[temperature]
initial_condition = 573.0
[]
[]
[Functions]
[temperature_func]
type = PiecewiseLinear
x = '0. 700. '
y = '573. 1273.' # From 300 to 1000 C at 1 K/s
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 700. '
y = '14.e+06 14.e+06' # 140 bar
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 700. '
y = '1.e+05 1.e+05' # atmospheric pressure
[]
# Circumferential steady-state creep test and analysis of Zircaloy-4 fuel cladding
# Nuclear Engineering and Design, 53, 2312-2322 (2021)
[F]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.738 0.738 0.57'
[]
[G]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.174 0.174 0.45'
[]
[H]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.588 0.588 0.48'
[]
[L]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[M]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[N]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[clad]
block = cladding
add_variables = true
strain = FINITE
decomposition_method = TaylorExpansion
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz hoop_stress'
use_automatic_differentiation = true
[]
[]
[AuxVariables]
[creep_rate_aux]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[scale_thickness]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfract_total]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfgain_total]
order = CONSTANT
family = MONOMIAL
[]
[burst_stress]
order = CONSTANT
family = MONOMIAL
[]
[burst]
order = CONSTANT
family = MONOMIAL
[]
[]
[Kernels]
[heat]
type = ADHeatConduction
variable = temperature
[]
[heat_ie]
type = ADHeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate_aux]
type = ADMaterialRealAux
variable = creep_rate_aux
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = ADMaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[scl_thickness]
type = ADMaterialRealAux
variable = scale_thickness
property = oxide_scale_thickness
boundary = 2
[]
[ofract_total]
type = ADMaterialRealAux
variable = oxywtfract_total
property = current_oxygen_weight_frac_total
boundary = 2
[]
[ofgain_total]
type = ADMaterialRealAux
boundary = 2
variable = oxywtfgain_total
property = oxygen_weight_frac_gained_total
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = 2
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = 2
execute_on = timestep_end
[]
[]
[BCs]
[inner_temperature]
type = REBEKADirichletBC
variable = temperature
function_tempm = temperature_func
minimum_temperature = 573.
translation = 0.1625
boundary = 4
[]
[no_y_midsection]
type = ADDirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply steam pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 101 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[CoolantChannel]
[convective_clad_surface]
boundary = 2
variable = temperature
inlet_temperature = 473.
inlet_pressure = 1.e+05
inlet_massflux = 1.0 # kg/m^2-sec # almost stagnant steam
rod_diameter = 10.75e-03
rod_pitch = 1.26e-02 # default
oxide_thickness = scale_thickness
number_axial_zone = 15
use_ad = true
[]
[]
[Materials]
[converter]
type = MaterialADConverter
reg_props_in = 'fract_beta_phase'
ad_props_out = 'ad_fract_beta_phase'
[]
[thermal]
type = ADZryThermal
block = cladding
temperature = temperature
[]
[clad_elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
block = cladding
youngs_modulus = 1.0e11
poissons_ratio = 0.3
[]
[clad_stress]
type = ADComputeMultipleInelasticStress
inelastic_models = 'clad_zrycreep'
block = cladding
[]
[hill_constants]
type = ADHillConstants
hill_constants = "0.738 0.174 0.588 1.0 1.0 1.0"
function_names = "F G H L M N"
temperature = temperature
[]
[clad_zrycreep]
type = ADZryAnisoCreepLOCAUpdate
block = cladding
temperature = temperature
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
temperature_loca_creep_begin = 501
temperature_standard_thermal_creep_end = 500
fract_beta_phase_name = 'ad_fract_beta_phase'
[]
[thermal_expansion]
type = ADZryThermalExpansionMATPROEigenstrain
block = cladding
temperature = temperature
stress_free_temperature = 573.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[density]
type = ADDensity
block = cladding
[]
[phase]
type = ZrPhase
block = cladding
temperature = temperature
numerical_method = 2
[]
[oxidation]
type = ADZryOxidation
boundary = 2
temperature = temperature
clad_inner_radius = 0.00465
clad_outer_radius = 0.005375
normal_operating_temperature_model = epri_kwu_ce
high_temperature_model = leistikow
use_coolant_channel = true
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = 2
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate_aux
temperature = temperature
fraction_beta_phase = fract_beta_phase
fraction_oxygen_gain = oxywtfgain_total
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-06
nl_abs_tol = 1.e-08
start_time = 0
n_startup_steps = 1
end_time = 700.
dtmax = 1.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[Postprocessors]
[ave_clad_exterior_temp]
type = SideAverageValue
boundary = 2
variable = temperature
[]
[max_clad_temp]
type = NodalExtremeValue
block = cladding
value_type = max
variable = temperature
[]
[min_clad_temp]
type = NodalExtremeValue
block = cladding
value_type = min
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = cladding
[]
[max_oxygen_fract]
type = ElementExtremeValue
block = cladding
value_type = max
variable = oxywtfract_total
[]
[max_betaph_fract]
type = ElementExtremeValue
block = cladding
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
block = cladding
value_type = max
variable = creep_rate_aux
[]
[max_creep_strain_mag]
type = ElementExtremeValue
block = cladding
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
block = cladding
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
block = cladding
value_type = max
variable = hoop_stress
[]
[vonmises_stress_clad]
type = ElementAverageValue
block = cladding
variable = vonmises_stress
[]
[min_burst_stress]
type = ElementExtremeValue
block = cladding
value_type = min
variable = burst_stress
[]
[burst]
type = ElementExtremeValue
block = cladding
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = cladding
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[top_disp_r_clad] # this is mid height
type = NodalVariableValue
variable = disp_x
nodeid = 0 #coords (0.005375, 0.1625)
[]
[top_disp_r_clad_slice] # this is mid height matched to the 1.5d
type = NodalVariableValue
variable = disp_x
nodeid = 3 #coords (0.005375, 0.1625)
[]
[top_disp_z_clad]
type = NodalVariableValue
variable = disp_y
nodeid = 0 #coords (0.005375, 0.1625)
[]
[stress_xx] # stess in the top Element
type = ElementalVariableValue
variable = stress_xx
elementid = 0
[]
[stress_yy] # stess in the top Element
type = ElementalVariableValue
variable = stress_yy
elementid = 0
[]
[stress_zz] # stess in the top Element
type = ElementalVariableValue
variable = stress_zz
elementid = 0
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = cladding
plenum_boundary_name = 4
external_clad_boundary_name = 2
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = rebeka_2d_14MPa_aniso_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
(assessment/LWR/validation/LOCA_IFA_650/analysis/IFA_650_9/IFA_650_9_part1.i)
[GlobalParams]
density = 10430.0
initial_porosity = 0.048
order = SECOND
family = LAGRANGE
displacements = disp_x
temperature = temperature
energy_per_fission = 3.2e-11 #J/fission
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
acceptable_multiplier = 10
[]
[Mesh]
coord_type = RZ
[layered1D_mesh]
type = Layered1DMeshGenerator
slices_per_block = 30
pellet_outer_radius = 4.565e-3
clad_gap_width = 0.085e-3
clad_thickness = 0.725e-3
fuel_height = 0.480
plenum_height = 0.262416
pellet_mesh_density = customize
clad_mesh_density = customize
nx_p = 11
nx_c = 5
[]
patch_update_strategy = auto
partitioner = centroid
centroid_partitioner_direction = y
[]
[Variables]
[disp_x]
[]
[temperature]
initial_condition = 295.0
[]
[]
[Functions]
[power_history]
type = PiecewiseLinear
data_file = power_history.csv
scale_factor = 1.0
format = columns
[]
[axial_peaking_factors]
type = PiecewiseBilinear
data_file = axial_peaking_factors.csv
axis = 1
scale_factor = 1
[]
[pressure_ramp]
type = PiecewiseLinear
data_file = coolant_pressure.csv
scale_factor = 1
format = columns
[]
[average_htc]
type = PiecewiseBilinear
data_file = average_coolant_htc.csv
axis = 1
scale_factor = 1
[]
[forced_times]
type = PiecewiseLinear
data_file = timestep_limiting.csv
scale_factor = 1
format = columns
[]
[heat_sink_temperature]
type = PiecewiseBilinear
data_file = heater_temp.csv
scale_factor = 1
axis = 1
[]
[clad_outer_temperature]
type = PiecewiseBilinear
data_file = clad_surface_temp.csv
scale_factor = 1
axis = 1
[]
[heat_transfer_mode]
type = PiecewiseConstant
x = '-200 200412461 200413048'
y = '9 9 8 '
direction = 'right'
[]
[clad_axial_pressure]
type = CladdingAxialPressureFunction
plenum_pressure = plenum_pressure
coolant_pressure = pressure_ramp
coolant_pressure_scaling_factor = 1.0
fuel_pin_geometry = fuel_pin_geometry
[]
[fuel_axial_pressure]
type = ParsedFunction
expression = plenum_pressure
symbol_names = plenum_pressure
symbol_values = plenum_pressure
[]
[]
[AuxVariables]
[disp_y]
[]
[disp_z]
[]
[fast_neutron_flux]
block = clad
[]
[fast_neutron_fluence]
block = clad
[]
[grain_radius]
block = fuel
initial_condition = 5.0e-6
[]
[effective_creep_strain]
block = clad
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[oxide_thickness]
order = CONSTANT
family = MONOMIAL
[]
[burst]
order = CONSTANT
family = MONOMIAL
[]
[gap_conductance]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[layered_maximum_clad_radius]
order = CONSTANT
family = MONOMIAL
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
extra_vector_tags = 'ref'
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
extra_vector_tags = 'ref'
[]
[heat_source]
type = NeutronHeatSource
variable = temperature
block = fuel
burnup_function = burnup
axial_relocation_object = axial_relocation
extra_vector_tags = 'ref'
[]
[]
[Physics]
[SolidMechanics]
[Layered1D]
[fuel]
add_scalar_variables = true
out_of_plane_strain_name = strain_yy
fuel_pin_geometry = fuel_pin_geometry
out_of_plane_pressure_function = fuel_axial_pressure
strain = finite
block = fuel
eigenstrain_names = 'fuel_thermal_strain fuel_swelling_strain
fuel_relocation_strain axial_relocation_eigenstrain'
decomposition_method = EigenSolution
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress
hoop_stress'
extra_vector_tags = 'ref'
group_scalar_vars_in_reference_residual = true
mesh_generator = layered1D_mesh
[]
[clad]
add_scalar_variables = true
out_of_plane_strain_name = strain_yy
fuel_pin_geometry = fuel_pin_geometry
strain = finite
out_of_plane_pressure_function = clad_axial_pressure
block = clad
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
eigenstrain_names = 'clad_thermal_strain clad_irradiation_strain'
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress
strain_zz creep_strain_zz hoop_stress'
decomposition_method = EigenSolution
extra_vector_tags = 'ref'
group_scalar_vars_in_reference_residual = true
mesh_generator = layered1D_mesh
[]
[]
[]
[]
[Burnup]
[burnup]
block = fuel
rod_ave_lin_pow = power_history
axial_power_profile = axial_peaking_factors
num_radial = 80
num_axial = 11
fuel_pin_geometry = fuel_pin_geometry
fuel_volume_ratio = 1.0
order = CONSTANT
family = MONOMIAL
RPF = RPF
isotopes = 'U235 U238 Pu239 Pu240 Pu241 Pu242'
isotope_fractions = '0.035 0.965 0 0 0 0'
[]
[]
[AuxKernels]
[fast_neutron_flux]
type = FastNeutronFluxAux
block = clad
variable = fast_neutron_flux
rod_ave_lin_pow = power_history
axial_power_profile = axial_peaking_factors
factor = 3e13
execute_on = timestep_begin
[]
[fast_neutron_fluence]
type = FastNeutronFluenceAux
block = clad
variable = fast_neutron_fluence
fast_neutron_flux = fast_neutron_flux
execute_on = timestep_begin
[]
[grain_radius]
type = GrainRadiusAux
block = fuel
variable = grain_radius
temperature = temperature
execute_on = linear
[]
[effective_creep_strain]
type = MaterialRealAux
block = clad
variable = effective_creep_strain
property = effective_creep_strain
execute_on = 'timestep_end'
[]
[fract_bphase]
type = MaterialRealAux
block = clad
variable = fract_beta_phase
property = fract_beta_phase
execute_on = 'initial linear'
[]
[oxide_thickness]
type = MaterialRealAux
boundary = 2
variable = oxide_thickness
property = oxide_scale_thickness
execute_on = 'initial linear'
[]
[hasburst]
type = MaterialRealAux
boundary = 2
variable = burst
property = failed
execute_on = timestep_end
[]
[conductance]
type = MaterialRealAux
boundary = 10
property = gap_conductance
variable = gap_conductance
execute_on = 'initial linear'
[]
[coolant_htc]
type = MaterialRealAux
property = coolant_channel_htc
variable = coolant_htc
boundary = 2
execute_on = 'initial linear'
[]
[creep_rate]
type = MaterialRealAux
block = clad
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[]
[AxialRelocation]
[rel]
rod_ave_lin_pow = power_history
axial_direction = y
fuel_blocks = fuel
clad_blocks = clad
contact_pressure_variable = contact_pressure
out_of_plane_strain_variable = strain_yy
penetration_variable = penetration
clad_inner_volume_addition = 0
burnup_variable = burnup
temperature = temperature
gap_thickness_threshold = 0.00039
axial_relocation_output_options = 'MASS_FRACTION'
mesh_generator = layered1D_mesh
[]
[]
[CoolantChannel]
[convective_clad_surface] # apply convective boundary to clad outer surface
boundary = 2
variable = temperature
heat_transfer_mode = heat_transfer_mode
heat_transfer_coefficient = average_htc # Calculated from an initial simulation of the base irradiation using the inlet_pressure, inlet_massflux, and inlet_temperature commented out below.
inlet_temperature = heat_sink_temperature # K
effective_emissivity = 0.75
# inlet_temperature = 580
# inlet_pressure = 15.3e6 # Pa
# inlet_massflux = 3800 # kg/m^2-sec
rod_diameter = 0.01075 # m
rod_pitch = 1.26e-2 # m
compute_enthalpy = false
linear_heat_rate = power_history
axial_power_profile = axial_peaking_factors
output_properties = 'coolant_channel_htype coolant_channel_hmode'
[]
[]
[Contact]
[pellet_clad_mechanical]
primary = 5
secondary = 10
penalty = 1e7
formulation = kinematic
model = frictionless
[]
[]
[ThermalContact]
[thermal_contact]
type = GasGapHeatTransfer
variable = temperature
primary = 5
secondary = 10
initial_moles = initial_moles
gas_released = fis_gas_released
plenum_pressure = plenum_pressure
contact_pressure = contact_pressure
jump_distance_model = LANNING
roughness_coef = 3.2
refab_gas_types = 'He Ar'
refab_fractions = '0.05 0.95'
refab_time = 199159200
refab_type = 0
[]
[]
[BCs]
[no_x_all]
type = DirichletBC
variable = disp_x
boundary = 12
value = 0.0
[]
[Pressure]
[coolantPressure]
boundary = 2
function = pressure_ramp
factor = 1.0
[]
[]
[clad_outer_temp]
type = FunctionDirichletBC
boundary = 2
variable = temperature
function = clad_outer_temperature
[]
[PlenumPressure]
[plenumPressure]
boundary = 9
initial_pressure = 2.0e6
startup_time = 0
R = 8.3143
output_initial_moles = initial_moles
temperature = plenum_temp
volume = 'clad_volume pellet_volume'
material_input = fis_gas_released
output = plenum_pressure
refab_time = 199159200
refab_pressure = 4.0e6
refab_temperature = 295.0
refab_volume = 1.9e-05
[]
[]
[]
[LayeredPlenumTemperature]
[plenum_temp]
boundary = 5
fuel_pin_geometry = fuel_pin_geometry
out_of_plane_strain = strain_yy
inner_surfaces = '5'
outer_surfaces = '10'
temperature = temperature
[]
[]
[Controls]
[period0]
type = TimePeriod
disable_objects = 'BCs/clad_outer_temp'
start_time = -200.0
end_time = 199159200.0
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
execute_on = timestep_end
[]
[]
[Materials]
[fuel_thermal]
type = UO2Thermal
block = fuel
thermal_conductivity_model = STAICU
hbs_porosity_correction = KAMPF
model_hbs_formation = true
temperature = temperature
burnup_function = burnup
axial_relocation_object = axial_relocation
gap_thermal_conductivity = layered_average_gap_conductivity
[]
[relocation]
type = UO2RelocationEigenstrain
block = fuel
burnup_function = burnup
rod_ave_lin_pow = power_history
axial_power_profile = axial_peaking_factors
fuel_pin_geometry = fuel_pin_geometry
burnup_relocation_stop = 0.024
relocation_activation1 = 5000.0
relocation_model = ESCORE_modified
eigenstrain_name = fuel_relocation_strain
[]
[fuel_thermal_strain]
type = ComputeThermalExpansionEigenstrain
block = fuel
thermal_expansion_coeff = 10.0e-6
stress_free_temperature = 295.0
eigenstrain_name = fuel_thermal_strain
[]
[fuel_swelling]
type = UO2VolumetricSwellingEigenstrain
gas_swelling_model_type = SIFGRS
block = fuel
burnup_function = burnup
initial_fuel_density = 10430.0
eigenstrain_name = fuel_swelling_strain
[]
[fission_gas_release]
type = UO2Sifgrs
block = fuel
temperature = temperature
burnup_function = burnup
grain_radius = grain_radius
transient_option = MICROCRACKING_BURNUP
diff_coeff_option = TURNBULL_D1_D2
gbs_model = true
[]
[fuel_elasticity_tensor]
type = UO2IsotropicDamageElasticityTensor
block = fuel
fragmentation_model = BARANI
temperature = temperature
rod_ave_lin_pow = power_history
axial_relocation_object = axial_relocation
crumbling_scale_factor = 0.0001
[]
[fuel_stress]
type = ComputeMultipleInelasticStress
tangent_operator = elastic
inelastic_models = 'fuel_creep'
block = fuel
[]
[fuel_creep]
type = UO2CreepUpdate
block = fuel
temperature = temperature
burnup_function = burnup
initial_grain_radius = 5.0e-6
[]
[HBS]
type = HighBurnupStructureFormation
block = fuel
burnup_function = burnup
temperature = temperature
output_properties = 'hbs_volume_fraction'
outputs = 'exodus'
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = clad
[]
[stress]
type = ComputeMultipleInelasticStress
tangent_operator = elastic
inelastic_models = 'zrycreep'
block = clad
[]
[zrycreep]
type = ZryCreepLOCAUpdate
fast_neutron_flux = fast_neutron_flux
fast_neutron_fluence = fast_neutron_fluence
model_irradiation_creep = true
model_primary_creep = true
model_thermal_creep = true
max_inelastic_increment = 5e-4
zircaloy_material_type = stress_relief_annealed
block = clad
[]
[thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = clad
stress_free_temperature = 295.0
eigenstrain_name = clad_thermal_strain
[]
[irradiation_swelling]
type = ZryIrradiationGrowthEigenstrain
block = clad
fast_neutron_fluence = fast_neutron_fluence
zircaloy_material_type = stress_relief_annealed
eigenstrain_name = clad_irradiation_strain
[]
[clad_phase]
type = ZrPhase
block = clad
temperature = temperature
numerical_method = 2
[]
[clad_oxidation]
type = ZryOxidation
boundary = 2
temperature = temperature
clad_inner_radius = 4.65e-03
clad_outer_radius = 5.375e-03
normal_operating_temperature_model = epri_kwu_ce
high_temperature_model = cathcart
use_coolant_channel = true
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = 2
failure_criterion = plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[clad_thermal]
type = ZryThermal
block = clad
temperature = temperature
[]
[fuel_density]
type = Density
block = fuel
[]
[clad_density]
type = Density
block = clad
density = 6551.0
[]
[]
[Postprocessors]
[ave_temp_interior]
type = LayeredSideAverageValuePostprocessor
boundary = 9
variable = temperature
execute_on = 'initial linear'
fuel_pin_geometry = fuel_pin_geometry
[]
[pellet_volume_2]
type = LayeredInternalVolumePostprocessor
boundary = 8
component = 0
fuel_pin_geometry = fuel_pin_geometry
out_of_plane_strain = strain_yy
execute_on = 'initial linear'
[]
[avg_clad_temp]
type = LayeredSideAverageValuePostprocessor
boundary = 7
variable = temperature
fuel_pin_geometry = fuel_pin_geometry
execute_on = 'initial linear'
[]
[fis_gas_produced]
type = LayeredElementIntegralFisGasGeneratedSifgrsPostprocessor
block = fuel
fuel_pin_geometry = fuel_pin_geometry
[]
[fis_gas_released]
type = LayeredElementIntegralFisGasReleasedSifgrsPostprocessor
block = fuel
fuel_pin_geometry = fuel_pin_geometry
[]
[fis_gas_grain]
type = LayeredElementIntegralFisGasGrainSifgrsPostprocessor
block = fuel
outputs = exodus
fuel_pin_geometry = fuel_pin_geometry
[]
[fis_gas_boundary]
type = LayeredElementIntegralFisGasBoundarySifgrsPostprocessor
block = fuel
outputs = exodus
fuel_pin_geometry = fuel_pin_geometry
[]
[fission_gas_release]
type = FGRPercent
fission_gas_released = fis_gas_released
fission_gas_generated = fis_gas_produced
[]
[average_coolant_htc]
type = LayeredSideAverageValuePostprocessor
boundary = 2
variable = coolant_htc
execute_on = 'initial linear'
fuel_pin_geometry = fuel_pin_geometry
[]
[average_burnup]
type = RodAverageBurnup
burnup_function = burnup
[]
[temp_clad_max]
type = NodalExtremeValue
block = clad
value_type = max
variable = temperature
execute_on = 'initial timestep_end'
[]
[betaph_fract_max]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
block = clad
execute_on = 'initial timestep_end'
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
block = clad
execute_on = 'initial timestep_end'
[]
[timestep_material]
type = MaterialTimeStepPostprocessor
block = clad
execute_on = 'initial timestep_end'
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = clad
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geometry
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[Dampers]
[limitT]
type = BoundingValueNodalDamper
variable = temperature
max_value = 3200.0
min_value = 0.0
[]
[limitX]
type = MaxIncrement
max_increment = 1e-5
variable = disp_x
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package -ksp_gmres_restart'
petsc_options_value = 'lu superlu_dist 51'
line_search = 'none'
l_max_its = 50
l_tol = 1e-3
nl_max_its = 30
nl_rel_tol = 1e-4
nl_abs_tol = 1e-8
dtmax = 5e5
dtmin = 1e-5
start_time = -200.0
end_time = 199159200 # End base irradiation
# end_time = 200412431 # Begin Blowdown
# end_time = 200413048 # End
[TimeStepper]
type = IterationAdaptiveDT
dt = 200
timestep_limiting_postprocessor = timestep_material
optimal_iterations = 20
iteration_window = 4
linear_iteration_ratio = 100
timestep_limiting_function = forced_times
force_step_every_function_point = true
max_function_change = 2000
time_t = '199159200 200312431 200411431 200412431 200412461 200413048'
time_dt = '1.0e04 1.0e04 10.0 5.0 0.5 5.0'
[]
[]
[VectorPostprocessors]
[clad_radial_disp]
type = NodalValueSampler
variable = disp_x
boundary = 2
sort_by = y
outputs = 'outfile_1'
[]
[clad_out_temp]
type = NodalValueSampler
variable = temperature
boundary = 2
sort_by = y
outputs = 'outfile_temp_1'
[]
[mass_fraction]
type = LineValueSampler
start_point = '0 0.01124 0'
end_point = '0 0.47524 0'
num_points = 30
sort_by = y
variable = layered_mass_fraction
outputs = 'outfile_mass_1'
[]
[]
[PerformanceMetricOutputs]
[]
[Outputs]
csv = true
color = false
perf_graph = true
[exodus]
type = Exodus
file_base = IFA_650_9_part1_out
execute_on = 'initial timestep_end'
[]
[checkpoint]
type = Checkpoint
time_step_interval = 1
num_files = 1
[]
[outfile_1]
type = CSV
execute_on = 'FINAL'
create_final_symlink = true
[]
[outfile_temp_1]
type = CSV
execute_on = 'FINAL'
create_final_symlink = true
[]
[outfile_mass_1]
type = CSV
execute_on = 'FINAL'
create_final_symlink = true
[]
[]
(assessment/LWR/validation/LOCA_IFA_650/analysis/IFA_650_9/IFA_650_9_part2.i)
[GlobalParams]
density = 10430.0
initial_porosity = 0.048
order = SECOND
family = LAGRANGE
displacements = disp_x
temperature = temperature
energy_per_fission = 3.2e-11 #J/fission
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
acceptable_multiplier = 10
restart_file_base = 'IFA_650_9_part1_checkpoint_cp/LATEST'
[]
[Mesh]
coord_type = RZ
[layered1D_mesh]
type = Layered1DMeshGenerator
slices_per_block = 30
pellet_outer_radius = 4.565e-3
clad_gap_width = 0.085e-3
clad_thickness = 0.725e-3
fuel_height = 0.480
plenum_height = 0.262416
pellet_mesh_density = customize
clad_mesh_density = customize
nx_p = 11
nx_c = 5
[]
patch_update_strategy = auto
partitioner = centroid
centroid_partitioner_direction = y
[]
[Variables]
[disp_x]
[]
[temperature]
[]
[]
[Functions]
[power_history]
type = PiecewiseLinear
data_file = power_history.csv
scale_factor = 1.0
format = columns
[]
[axial_peaking_factors]
type = PiecewiseBilinear
data_file = axial_peaking_factors.csv
axis = 1
scale_factor = 1
[]
[pressure_ramp]
type = PiecewiseLinear
data_file = coolant_pressure.csv
scale_factor = 1
format = columns
[]
[average_htc]
type = PiecewiseBilinear
data_file = average_coolant_htc.csv
axis = 1
scale_factor = 1
[]
[forced_times]
type = PiecewiseLinear
data_file = timestep_limiting.csv
scale_factor = 1
format = columns
[]
[heat_sink_temperature]
type = PiecewiseBilinear
data_file = heater_temp.csv
scale_factor = 1
axis = 1
[]
[clad_outer_temperature]
type = PiecewiseBilinear
data_file = clad_surface_temp.csv
scale_factor = 1
axis = 1
[]
[heat_transfer_mode]
type = PiecewiseConstant
x = '-200 200412461 200413048'
y = '9 9 8 '
direction = 'right'
[]
[clad_axial_pressure]
type = CladdingAxialPressureFunction
plenum_pressure = plenum_pressure
coolant_pressure = pressure_ramp
coolant_pressure_scaling_factor = 1.0
fuel_pin_geometry = fuel_pin_geometry
[]
[fuel_axial_pressure]
type = ParsedFunction
expression = plenum_pressure
symbol_names = plenum_pressure
symbol_values = plenum_pressure
[]
[]
[AuxVariables]
[disp_y]
[]
[disp_z]
[]
[fast_neutron_flux]
block = clad
[]
[fast_neutron_fluence]
block = clad
[]
[grain_radius]
block = fuel
[]
[effective_creep_strain]
block = clad
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[oxide_thickness]
order = CONSTANT
family = MONOMIAL
[]
[burst]
order = CONSTANT
family = MONOMIAL
[]
[gap_conductance]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[layered_maximum_clad_radius]
order = CONSTANT
family = MONOMIAL
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
extra_vector_tags = 'ref'
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
extra_vector_tags = 'ref'
[]
[heat_source]
type = NeutronHeatSource
variable = temperature
block = fuel
burnup_function = burnup
axial_relocation_object = axial_relocation
extra_vector_tags = 'ref'
[]
[]
[Physics]
[SolidMechanics]
[Layered1D]
[fuel]
add_scalar_variables = true
out_of_plane_strain_name = strain_yy
fuel_pin_geometry = fuel_pin_geometry
out_of_plane_pressure_function = fuel_axial_pressure
strain = finite
block = fuel
eigenstrain_names = 'fuel_thermal_strain fuel_swelling_strain
fuel_relocation_strain axial_relocation_eigenstrain'
decomposition_method = EigenSolution
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress
hoop_stress'
extra_vector_tags = 'ref'
group_scalar_vars_in_reference_residual = true
mesh_generator = layered1D_mesh
[]
[clad]
add_scalar_variables = true
out_of_plane_strain_name = strain_yy
fuel_pin_geometry = fuel_pin_geometry
strain = finite
out_of_plane_pressure_function = clad_axial_pressure
block = clad
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
eigenstrain_names = 'clad_thermal_strain clad_irradiation_strain'
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress
strain_zz creep_strain_zz hoop_stress'
decomposition_method = EigenSolution
extra_vector_tags = 'ref'
group_scalar_vars_in_reference_residual = true
mesh_generator = layered1D_mesh
[]
[]
[]
[]
[Burnup]
[burnup]
block = fuel
rod_ave_lin_pow = power_history
axial_power_profile = axial_peaking_factors
num_radial = 80
num_axial = 11
fuel_pin_geometry = fuel_pin_geometry
fuel_volume_ratio = 1.0
order = CONSTANT
family = MONOMIAL
RPF = RPF
isotopes = 'U235 U238 Pu239 Pu240 Pu241 Pu242'
isotope_fractions = '0.035 0.965 0 0 0 0'
[]
[]
[AuxKernels]
[fast_neutron_flux]
type = FastNeutronFluxAux
block = clad
variable = fast_neutron_flux
rod_ave_lin_pow = power_history
axial_power_profile = axial_peaking_factors
factor = 3e13
execute_on = timestep_begin
[]
[fast_neutron_fluence]
type = FastNeutronFluenceAux
block = clad
variable = fast_neutron_fluence
fast_neutron_flux = fast_neutron_flux
execute_on = timestep_begin
[]
[grain_radius]
type = GrainRadiusAux
block = fuel
variable = grain_radius
temperature = temperature
execute_on = linear
[]
[effective_creep_strain]
type = MaterialRealAux
block = clad
variable = effective_creep_strain
property = effective_creep_strain
execute_on = 'timestep_end'
[]
[fract_bphase]
type = MaterialRealAux
block = clad
variable = fract_beta_phase
property = fract_beta_phase
execute_on = 'initial linear'
[]
[oxide_thickness]
type = MaterialRealAux
boundary = 2
variable = oxide_thickness
property = oxide_scale_thickness
execute_on = 'initial linear'
[]
[hasburst]
type = MaterialRealAux
boundary = 2
variable = burst
property = failed
execute_on = timestep_end
[]
[conductance]
type = MaterialRealAux
boundary = 10
property = gap_conductance
variable = gap_conductance
execute_on = 'initial linear'
[]
[coolant_htc]
type = MaterialRealAux
property = coolant_channel_htc
variable = coolant_htc
boundary = 2
execute_on = 'initial linear'
[]
[creep_rate]
type = MaterialRealAux
block = clad
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[]
[AxialRelocation]
[rel]
rod_ave_lin_pow = power_history
axial_direction = y
fuel_blocks = fuel
clad_blocks = clad
contact_pressure_variable = contact_pressure
out_of_plane_strain_variable = strain_yy
penetration_variable = penetration
clad_inner_volume_addition = 2.73291E-06 # Addition of the volume to bring the starting total volume to 19cm^3 to begin the transient experiment
burnup_variable = burnup
temperature = temperature
gap_thickness_threshold = 0.00039
axial_relocation_output_options = 'MASS_FRACTION'
mesh_generator = layered1D_mesh
[]
[]
[CoolantChannel]
[convective_clad_surface] # apply convective boundary to clad outer surface
boundary = 2
variable = temperature
heat_transfer_mode = heat_transfer_mode
heat_transfer_coefficient = average_htc # Calculated from an initial simulation of the base irradiation using the inlet_pressure, inlet_massflux, and inlet_temperature commented out below.
inlet_temperature = heat_sink_temperature # K
effective_emissivity = 0.75
# inlet_temperature = 580
# inlet_pressure = 15.3e6 # Pa
# inlet_massflux = 3800 # kg/m^2-sec
rod_diameter = 0.01075 # m
rod_pitch = 1.26e-2 # m
compute_enthalpy = false
linear_heat_rate = power_history
axial_power_profile = axial_peaking_factors
output_properties = 'coolant_channel_htype coolant_channel_hmode'
[]
[]
[Contact]
[pellet_clad_mechanical]
primary = 5
secondary = 10
penalty = 1e7
formulation = kinematic
model = frictionless
[]
[]
[ThermalContact]
[thermal_contact]
type = GasGapHeatTransfer
variable = temperature
primary = 5
secondary = 10
initial_moles = initial_moles
gas_released = fis_gas_released
plenum_pressure = plenum_pressure
contact_pressure = contact_pressure
jump_distance_model = LANNING
roughness_coef = 3.2
refab_gas_types = 'He Ar'
refab_fractions = '0.05 0.95'
refab_time = 199159200
refab_type = 0
[]
[]
[BCs]
[no_x_all]
type = DirichletBC
variable = disp_x
boundary = 12
value = 0.0
[]
[Pressure]
[coolantPressure]
boundary = 2
function = pressure_ramp
factor = 1.0
[]
[]
[clad_outer_temp]
type = FunctionDirichletBC
boundary = 2
variable = temperature
function = clad_outer_temperature
[]
[PlenumPressure]
[plenumPressure]
boundary = 9
initial_pressure = 2.0e6
startup_time = 0
R = 8.3143
output_initial_moles = initial_moles
temperature = plenum_temp
volume = 'clad_volume pellet_volume'
material_input = fis_gas_released
output = plenum_pressure
refab_time = 199159200
refab_pressure = 4.0e6
refab_temperature = 295.0
refab_volume = 1.9e-05
[]
[]
[]
[LayeredPlenumTemperature]
[plenum_temp]
boundary = 5
fuel_pin_geometry = fuel_pin_geometry
out_of_plane_strain = strain_yy
inner_surfaces = '5'
outer_surfaces = '10'
temperature = temperature
[]
[]
[Controls]
[period1]
type = TimePeriod
disable_objects = 'BCs/clad_outer_temp'
start_time = 200412431
end_time = 200413048
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
execute_on = timestep_end
[]
[]
[Materials]
[fuel_thermal]
type = UO2Thermal
block = fuel
thermal_conductivity_model = STAICU
hbs_porosity_correction = KAMPF
model_hbs_formation = true
temperature = temperature
burnup_function = burnup
axial_relocation_object = axial_relocation
gap_thermal_conductivity = layered_average_gap_conductivity
[]
[relocation]
type = UO2RelocationEigenstrain
block = fuel
burnup_function = burnup
rod_ave_lin_pow = power_history
axial_power_profile = axial_peaking_factors
fuel_pin_geometry = fuel_pin_geometry
burnup_relocation_stop = 0.024
relocation_activation1 = 5000.0
relocation_model = ESCORE_modified
eigenstrain_name = fuel_relocation_strain
[]
[fuel_thermal_strain]
type = ComputeThermalExpansionEigenstrain
block = fuel
thermal_expansion_coeff = 10.0e-6
stress_free_temperature = 295.0
eigenstrain_name = fuel_thermal_strain
[]
[fuel_swelling]
type = UO2VolumetricSwellingEigenstrain
gas_swelling_model_type = SIFGRS
block = fuel
burnup_function = burnup
initial_fuel_density = 10430.0
eigenstrain_name = fuel_swelling_strain
[]
[fission_gas_release]
type = UO2Sifgrs
block = fuel
temperature = temperature
burnup_function = burnup
grain_radius = grain_radius
transient_option = MICROCRACKING_BURNUP
diff_coeff_option = TURNBULL_D1_D2
gbs_model = true
[]
[fuel_elasticity_tensor]
type = UO2IsotropicDamageElasticityTensor
block = fuel
fragmentation_model = BARANI
temperature = temperature
rod_ave_lin_pow = power_history
# axial_relocation_object = axial_relocation
crumbling_scale_factor = 0.0001
[]
[fuel_stress]
type = ComputeMultipleInelasticStress
tangent_operator = elastic
inelastic_models = 'fuel_creep'
block = fuel
[]
[fuel_creep]
type = UO2CreepUpdate
block = fuel
temperature = temperature
burnup_function = burnup
initial_grain_radius = 5.0e-6
[]
[HBS]
type = HighBurnupStructureFormation
block = fuel
burnup_function = burnup
temperature = temperature
output_properties = 'hbs_volume_fraction'
outputs = 'exodus'
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = clad
[]
[stress]
type = ComputeMultipleInelasticStress
tangent_operator = elastic
inelastic_models = 'zrycreep'
block = clad
[]
[zrycreep]
type = ZryCreepLOCAUpdate
fast_neutron_flux = fast_neutron_flux
fast_neutron_fluence = fast_neutron_fluence
model_irradiation_creep = true
model_primary_creep = true
model_thermal_creep = true
max_inelastic_increment = 1e-3
zircaloy_material_type = stress_relief_annealed
block = clad
[]
[thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = clad
stress_free_temperature = 295.0
eigenstrain_name = clad_thermal_strain
[]
[irradiation_swelling]
type = ZryIrradiationGrowthEigenstrain
block = clad
fast_neutron_fluence = fast_neutron_fluence
zircaloy_material_type = stress_relief_annealed
eigenstrain_name = clad_irradiation_strain
[]
[clad_phase]
type = ZrPhase
block = clad
temperature = temperature
numerical_method = 2
[]
[clad_oxidation]
type = ZryOxidation
boundary = 2
temperature = temperature
clad_inner_radius = 4.65e-03
clad_outer_radius = 5.375e-03
normal_operating_temperature_model = epri_kwu_ce
high_temperature_model = cathcart
use_coolant_channel = true
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = 2
failure_criterion = plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[clad_thermal]
type = ZryThermal
block = clad
temperature = temperature
[]
[fuel_density]
type = Density
block = fuel
[]
[clad_density]
type = Density
block = clad
density = 6551.0
[]
[]
[Postprocessors]
[ave_temp_interior]
type = LayeredSideAverageValuePostprocessor
boundary = 9
variable = temperature
execute_on = 'initial linear'
fuel_pin_geometry = fuel_pin_geometry
[]
[pellet_volume_2]
type = LayeredInternalVolumePostprocessor
boundary = 8
component = 0
fuel_pin_geometry = fuel_pin_geometry
out_of_plane_strain = strain_yy
execute_on = 'initial linear'
[]
[avg_clad_temp]
type = LayeredSideAverageValuePostprocessor
boundary = 7
variable = temperature
fuel_pin_geometry = fuel_pin_geometry
execute_on = 'initial linear'
[]
[fis_gas_produced]
type = LayeredElementIntegralFisGasGeneratedSifgrsPostprocessor
block = fuel
fuel_pin_geometry = fuel_pin_geometry
[]
[fis_gas_released]
type = LayeredElementIntegralFisGasReleasedSifgrsPostprocessor
block = fuel
fuel_pin_geometry = fuel_pin_geometry
[]
[fis_gas_grain]
type = LayeredElementIntegralFisGasGrainSifgrsPostprocessor
block = fuel
outputs = exodus
fuel_pin_geometry = fuel_pin_geometry
[]
[fis_gas_boundary]
type = LayeredElementIntegralFisGasBoundarySifgrsPostprocessor
block = fuel
outputs = exodus
fuel_pin_geometry = fuel_pin_geometry
[]
[fission_gas_release]
type = FGRPercent
fission_gas_released = fis_gas_released
fission_gas_generated = fis_gas_produced
[]
[average_coolant_htc]
type = LayeredSideAverageValuePostprocessor
boundary = 2
variable = coolant_htc
execute_on = 'initial linear'
fuel_pin_geometry = fuel_pin_geometry
[]
[average_burnup]
type = RodAverageBurnup
burnup_function = burnup
[]
[temp_clad_max]
type = NodalExtremeValue
block = clad
value_type = max
variable = temperature
execute_on = 'initial timestep_end'
[]
[betaph_fract_max]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
block = clad
execute_on = 'initial timestep_end'
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
block = clad
execute_on = 'initial timestep_end'
[]
[timestep_material]
type = MaterialTimeStepPostprocessor
block = clad
execute_on = 'initial timestep_end'
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = clad
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geometry
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[Dampers]
[limitT]
type = BoundingValueNodalDamper
variable = temperature
max_value = 3200.0
min_value = 0.0
[]
[limitX]
type = MaxIncrement
max_increment = 1e-5
variable = disp_x
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package -ksp_gmres_restart'
petsc_options_value = 'lu superlu_dist 51'
line_search = 'none'
l_max_its = 50
l_tol = 1e-3
nl_max_its = 100
nl_rel_tol = 1e-4
nl_abs_tol = 1e-8
dtmax = 5e5
dtmin = 1e-5
# end_time = 199159200 # End base irradiation
# end_time = 200412431 # Begin Blowdown
end_time = 200413048 # End
[TimeStepper]
type = IterationAdaptiveDT
dt = 200
timestep_limiting_postprocessor = timestep_material
optimal_iterations = 20
iteration_window = 4
linear_iteration_ratio = 100
timestep_limiting_function = forced_times
force_step_every_function_point = true
max_function_change = 2000
time_t = '199159200 200312431 200411431 200412431 200412461 200413048'
time_dt = '1.0e04 1.0e04 10.0 5.0 0.5 5.0'
[]
[]
[VectorPostprocessors]
[clad_radial_disp]
type = NodalValueSampler
variable = disp_x
boundary = 2
sort_by = y
outputs = 'outfile_2'
[]
[clad_out_temp]
type = NodalValueSampler
variable = temperature
boundary = 2
sort_by = y
outputs = 'outfile_temp_2'
[]
[mass_fraction]
type = LineValueSampler
start_point = '0 0.01124 0'
end_point = '0 0.47524 0'
num_points = 30
sort_by = y
variable = layered_mass_fraction
outputs = 'outfile_mass_2'
[]
[]
[PerformanceMetricOutputs]
[]
[Outputs]
csv = true
color = false
exodus = true
execute_on = 'initial timestep_end'
perf_graph = true
[outfile_2]
type = CSV
execute_on = 'FINAL'
create_final_symlink = true
[]
[outfile_temp_2]
type = CSV
execute_on = 'FINAL'
create_final_symlink = true
[]
[outfile_mass_2]
type = CSV
execute_on = 'FINAL'
create_final_symlink = true
[]
[]
(assessment/LWR/validation/LOCA_ORNL_cladding_burst_tests/analysis/Zr4_1/ornl_zr4_1_ad_hill.i)
# Simulation ORNL burst tests Zr4_1
[GlobalParams]
density = 6550.
order = SECOND
family = LAGRANGE
displacements = 'disp_x disp_y'
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = zr4_ornl_burst_test_mesh.e
[]
[]
[Variables]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func] # only 10 inches of the rod are within the heated zone (cf. Terrani email)
type = PiecewiseBilinear
data_file = temperature_ornl_zr4_1.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
data_file = pressure_inner_ornl_zr4_1.csv
scale_factor = 1.e+06
format = columns
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 373.9'
y = '0.1 0.1 ' # atmospheric pressure
scale_factor = 1.e+06
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[clad]
block = cladding
add_variables = true
strain = FINITE
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
# decomposition_method = EigenSolution
eigenstrain_names = 'clad_thermal_eigenstrain'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz hoop_stress'
use_automatic_differentiation = true
decomposition_method = TaylorExpansion
[]
[]
[AuxVariables]
[creep_rate_aux]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[scale_thickness]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfract_total]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfgain_total]
order = CONSTANT
family = MONOMIAL
[]
[burst_stress]
order = CONSTANT
family = MONOMIAL
[]
[burst]
order = CONSTANT
family = MONOMIAL
[]
[]
[Kernels]
[heat]
type = ADHeatConduction
variable = temperature
[]
[heat_ie]
type = ADHeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate_aux]
type = ADMaterialRealAux
variable = creep_rate_aux
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = ADMaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[scl_thickness]
type = ADMaterialRealAux
variable = scale_thickness
property = oxide_scale_thickness
boundary = 2
[]
[ofract_total]
type = ADMaterialRealAux
variable = oxywtfract_total
property = current_oxygen_weight_frac_total
boundary = 2
[]
[ofgain_total]
type = ADMaterialRealAux
boundary = 2
variable = oxywtfgain_total
property = oxygen_weight_frac_gained_total
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = 2
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = 2
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = ADFunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 4'
preset = false
[]
[no_y_top]
type = ADDirichletBC
variable = disp_y
boundary = 3
value = 0.
preset = false
[]
[Pressure]
[outer_pressure] # apply steam pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[mid_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 98 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[converter]
type = MaterialADConverter
reg_props_in = 'fract_beta_phase'
ad_props_out = 'ad_fract_beta_phase'
[]
[thermal]
type = ADZryThermal
block = cladding
temperature = temperature
[]
[clad_elasticity_tensor]
type = ADZryElasticityTensor
block = cladding
matpro_youngs_modulus = false
matpro_poissons_ratio = false
[]
[clad_stress]
type = ADComputeMultipleInelasticStress
inelastic_models = 'clad_zrycreep'
block = cladding
[]
[hill_constants]
type = ADHillConstants
hill_constants = "0.5 0.5 0.5 1.0 1.0 1.0"
# hill_constants = "0.304 0.240 0.956 1.0 1.0 1.0"
[]
[clad_zrycreep]
type = ADZryAnisoCreepLOCAUpdate
block = cladding
temperature = temperature
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
temperature_loca_creep_begin = 301
temperature_standard_thermal_creep_end = 300
fract_beta_phase_name = 'ad_fract_beta_phase'
[]
[thermal_expansion]
type = ADZryThermalExpansionMATPROEigenstrain
block = cladding
temperature = temperature
stress_free_temperature = 300.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[density]
type = ADDensity
block = cladding
[]
[phase]
type = ZrPhase
block = cladding
temperature = temperature
numerical_method = 2
[]
[oxidation]
type = ADZryOxidation
boundary = 2
temperature = temperature
clad_inner_radius = 0.004175
clad_outer_radius = 0.004750
normal_operating_temperature_model = epri_kwu_ce
high_temperature_model = leistikow
#use_coolant_channel = true
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = 2
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate_aux
temperature = temperature
fraction_beta_phase = fract_beta_phase
fraction_oxygen_gain = oxywtfgain_total
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = PJFNK
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0
n_startup_steps = 1
end_time = 373.9
dtmax = 1.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[Postprocessors]
[pressure_inner]
type = FunctionValuePostprocessor
function = inner_pressure_func
execute_on = 'initial timestep_end'
[]
[pressure_outer]
type = FunctionValuePostprocessor
function = outer_pressure_func
execute_on = 'initial timestep_end'
[]
[ave_clad_temp]
type = SideAverageValue
boundary = 2
variable = temperature
execute_on = 'initial timestep_end'
[]
[max_clad_temp]
type = NodalExtremeValue
block = cladding
value_type = max
variable = temperature
execute_on = 'initial timestep_end'
[]
[min_clad_temp]
type = NodalExtremeValue
block = cladding
value_type = min
variable = temperature
execute_on = 'initial timestep_end'
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = cladding
[]
[max_oxygen_fract]
type = ElementExtremeValue
block = cladding
value_type = max
variable = oxywtfract_total
execute_on = 'initial timestep_end'
[]
[max_betaph_fract]
type = ElementExtremeValue
block = cladding
value_type = max
variable = fract_beta_phase
execute_on = 'initial timestep_end'
[]
[max_creep_rate]
type = ElementExtremeValue
block = cladding
value_type = max
variable = creep_rate_aux
execute_on = 'initial timestep_end'
[]
[max_creep_strain_mag]
type = ElementExtremeValue
block = cladding
value_type = max
variable = creep_strain_mag
execute_on = 'initial timestep_end'
[]
[max_hoop_strain]
type = ElementExtremeValue
block = cladding
value_type = max
variable = strain_zz
execute_on = 'initial timestep_end'
[]
[max_hoop_stress]
type = ElementExtremeValue
block = cladding
value_type = max
variable = hoop_stress
[]
[vonmises_stress_clad]
type = ElementAverageValue
block = cladding
variable = vonmises_stress
execute_on = 'initial timestep_end'
[]
[min_burst_stress]
type = ElementExtremeValue
block = cladding
value_type = min
variable = burst_stress
execute_on = 'initial timestep_end'
[]
[burst]
type = ElementExtremeValue
block = cladding
value_type = max
variable = burst
execute_on = 'initial timestep_end'
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = cladding
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[mid_disp_r_clad]
type = NodalVariableValue
variable = disp_x
nodeid = 22
[]
[stress_xx_midplane] # stress in the mid Element
type = ElementalVariableValue
variable = stress_xx
elementid = 19
[]
[stress_yy_midplane] # stress in the mid Element
type = ElementalVariableValue
variable = stress_yy
elementid = 19
[]
[stress_zz_midplane] # stress in the mid Element
type = ElementalVariableValue
variable = stress_zz
elementid = 19
[]
[strain_zz_midplane] # strain in the mid Element
type = ElementalVariableValue
variable = strain_zz
elementid = 19
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
plenum_boundary_name = 4
cladding_blocks = cladding
[]
[PerformanceMetricOutputs]
[]
[Outputs]
exodus = true
perf_graph = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 20
[]
[chkfile]
type = CSV
file_base = ornl_zr4_1_ad_hill_chkfile
show = 'pressure_inner max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/LOCA_Studsvik/analysis/rod_191/Studsvik_191_part1.i)
[GlobalParams]
density = 10431.0
initial_porosity = 0.05
order = SECOND
family = LAGRANGE
energy_per_fission = 3.2e-11 # J/fission
volumetric_locking_correction = false
displacements = 'disp_x disp_y'
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
[]
[Mesh]
coord_type = RZ
[smeared_mesh]
type = FuelPinMeshGenerator
clad_top_gap_height = 0.021861442
pellet_height = 0.265388558
pellet_quantity = 1
clad_bot_gap_height = 0.01275
pellet_outer_radius = 4.1e-3
clad_gap_width = 80e-6
clad_thickness = 0.57e-3
clad_mesh_density = customize
pellet_mesh_density = customize
nx_c = 5
ny_c = 50
nx_p = 11
ny_p = 60
elem_type = QUAD8
[]
patch_update_strategy = auto
patch_size = 10 # For contact algorithm
partitioner = centroid
centroid_partitioner_direction = y
[]
[Variables]
# Define dependent variables and initial conditions
[temperature]
initial_condition = 295.0 # set initial temp to coolant inlet
[]
[]
[AuxVariables]
# Define auxilary variables
[fast_neutron_flux]
block = clad
[]
[fast_neutron_fluence]
block = clad
[]
[grain_radius]
block = pellet
initial_condition = 10e-6
[]
[creep_strain_rate]
order = CONSTANT
family = MONOMIAL
[]
[effective_creep_strain]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[hoop_strain]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[scale_thickness] # ZrO2 scale thickness (m)
order = CONSTANT
family = MONOMIAL
[]
[oxywtfract_total] # Current oxigen weight fraction (oxide+metal) (/)
order = CONSTANT
family = MONOMIAL
[]
[oxywtfgain_total] # Gained oxygen weight fraction (oxide+metal) (/)
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[gap_cond]
order = CONSTANT
family = MONOMIAL
[]
[]
[Functions]
[power_history]
type = PiecewiseLinear
data_file = power_history.csv
format = columns
scale_factor = 1
[]
[axial_peaking_factors]
type = ParsedFunction
expression = 1
[]
[pressure_ramp] # reads and interpolates input data defining amplitude curve for fill gas pressure
type = PiecewiseLinear
x = '-200 0 166755600 166842000'
y = '0.006537 1 1 0.006537'
scale_factor = 15.5e6
[]
[forced_times]
type = PiecewiseLinear
data_file = timestep_limiting.csv
scale_factor = 1
format = columns
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[fuel]
block = pellet
add_variables = true
strain = FINITE
eigenstrain_names = 'fuel_thermal_eigenstrain fuel_relocation_eigenstrain fuel_volumetric_eigenstrain'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz'
decomposition_method = EigenSolution
extra_vector_tags = 'ref'
temperature = temperature
[]
[clad]
block = clad
add_variables = true
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain clad_irradiation_eigenstrain'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz creep_strain_zz strain_zz'
extra_vector_tags = 'ref'
decomposition_method = EigenSolution
temperature = temperature
[]
[]
[Kernels]
[gravity]
type = Gravity
variable = disp_y
value = -9.81
[]
[heat]
type = HeatConduction
variable = temperature
extra_vector_tags = 'ref'
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
extra_vector_tags = 'ref'
[]
[heat_source]
type = NeutronHeatSource
variable = temperature
extra_vector_tags = 'ref'
block = pellet
burnup_function = burnup
[]
[]
[Burnup]
[burnup]
block = pellet
rod_ave_lin_pow = power_history # using the power function defined above
axial_power_profile = axial_peaking_factors # using the axial power profile function defined above
num_radial = 80
num_axial = 11
fuel_pin_geometry = fuel_pin_geometry
fuel_volume_ratio = 1.0 # for use with dished pellets (ratio of actual volume to cylinder volume)
order = CONSTANT
family = MONOMIAL
RPF = RPF
isotopes = 'U235 U238 Pu239 Pu240 Pu241 Pu242'
isotope_fractions = '0.05 0.95 0 0 0 0'
[]
[]
[AuxKernels]
# Define auxilliary kernels for each of the aux variables
[fast_neutron_flux]
type = FastNeutronFluxAux
variable = fast_neutron_flux
block = clad
rod_ave_lin_pow = power_history
axial_power_profile = axial_peaking_factors
factor = 3e13
execute_on = timestep_begin
[]
[fast_neutron_fluence]
type = FastNeutronFluenceAux
variable = fast_neutron_fluence
block = clad
fast_neutron_flux = fast_neutron_flux
execute_on = timestep_begin
[]
[grain_radius]
type = GrainRadiusAux
block = pellet
variable = grain_radius
temperature = temperature
execute_on = linear
[]
[creep_strain_rate]
type = MaterialRealAux
property = creep_rate
variable = creep_strain_rate
block = clad
[]
[effective_creep_strain]
type = MaterialRealAux
property = effective_creep_strain
variable = effective_creep_strain
block = clad
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
block = clad
variable = fract_beta_phase
property = fract_beta_phase
[]
[scl_thickness]
type = MaterialRealAux
boundary = 2
variable = scale_thickness
property = oxide_scale_thickness
[]
[ofract_total]
type = MaterialRealAux
boundary = 2
variable = oxywtfract_total
property = current_oxygen_weight_frac_total
[]
[ofgain_total]
type = MaterialRealAux
boundary = 2
variable = oxywtfgain_total
property = oxygen_weight_frac_gained_total
[]
[sigmaburst]
type = MaterialRealAux
boundary = 2
variable = burst_stress
property = burst_stress
[]
[hasburst]
type = MaterialRealAux
boundary = 2
variable = burst
property = failed
execute_on = timestep_end
[]
[conductance]
type = MaterialRealAux
property = gap_conductance
variable = gap_cond
boundary = 10
execute_on = 'linear'
[]
[]
[Contact]
[pellet_clad_mechanical]
primary = 5
secondary = 10
formulation = kinematic
model = frictionless
penalty = 1e7
[]
[]
[ThermalContact]
[thermal_contact]
type = GasGapHeatTransfer
variable = temperature
primary = 5
secondary = 10
initial_moles = initial_moles
gas_released = fission_gas_released
quadrature = true
contact_pressure = contact_pressure
refab_gas_types = He
refab_fractions = 1
refab_time = 166842000
refab_type = 0
[]
[]
[BCs]
[no_x_all]
type = DirichletBC
variable = disp_x
boundary = 12
value = 0.0
[]
[no_y_clad_bottom]
type = DirichletBC
variable = disp_y
boundary = '1'
value = 0.0
[]
[no_y_fuel_bottom]
type = DirichletBC
variable = disp_y
boundary = '1020'
value = 0.0
[]
[Pressure]
[coolantPressure]
boundary = '1 2 3'
function = pressure_ramp
[]
[]
[PlenumPressure]
[plenumPressure]
boundary = 9
initial_pressure = 3.44738e6
startup_time = 0
R = 8.3143
output_initial_moles = initial_moles
temperature = plenum_temp
volume = plenum_volume
material_input = fission_gas_released
output = plenum_pressure
refab_time = 166842000
refab_pressure = 11e6
refab_temperature = 295.0
refab_volume = 1.04e-05
cladding_failure_status = burst
equilibrium_pressure = equilibrium_pressure
additional_volumes = additional_volume
temperature_of_additional_volumes = addition_temperature
[]
[]
[]
[UserObjects]
[fuel_pin_geometry]
type = FuelPinGeometry
[]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[]
[PlenumTemperature]
[plenum_temp]
boundary = 5
inner_surfaces = '5'
outer_surfaces = '10'
temperature = temperature
[]
[]
[CoolantChannel]
[convective_clad_surface] # apply convective boundary to clad outer surface
boundary = 2
variable = temperature
inlet_temperature = 580
inlet_pressure = 15.5e6 # Pa
inlet_massflux = 3800 # kg/m^2-sec
rod_diameter = 0.0095 # m
rod_pitch = 1.26e-2 # m
compute_enthalpy = false
linear_heat_rate = power_history
axial_power_profile = axial_peaking_factors
output_properties = 'coolant_channel_htype coolant_channel_hmode'
[]
[]
[Materials]
[uo2_pulverization]
type = UO2Pulverization
block = pellet
layered_average_contact_pressure = contact_pressure
temperature = temperature
burnup_function = burnup
output_properties = pulverized
outputs = all
[]
# Define material behavior models and input material property data
[fuel_thermal] # temperature and burnup dependent thermal properties of UO2 (BISON kernel)
type = UO2Thermal
block = pellet
thermal_conductivity_model = NFIR
temperature = temperature
burnup_function = burnup
[]
[fuel_elasticity_tensor]
type = UO2IsotropicDamageElasticityTensor
block = pellet
fragmentation_model = BARANI
temperature = temperature
rod_ave_lin_pow = power_history
[]
[fuel_elastic_stress]
type = ComputeMultipleInelasticStress
tangent_operator = elastic
inelastic_models = 'fuel_creep'
block = pellet
[]
[fuel_creep]
type = UO2CreepUpdate
block = pellet
temperature = temperature
fission_rate = fission_rate
initial_grain_radius = 10.0e-6
oxygen_to_metal_ratio = 2.0
[]
[fuel_relocation]
type = UO2RelocationEigenstrain
block = pellet
burnup_function = burnup
fuel_pin_geometry = fuel_pin_geometry
rod_ave_lin_pow = power_history
axial_power_profile = axial_peaking_factors
burnup_relocation_stop = 0.024
relocation_activation1 = 5000
relocation_model = ESCORE_modified
eigenstrain_name = fuel_relocation_eigenstrain
[]
[fuel_thermal_expansion]
type = ComputeThermalExpansionEigenstrain
block = pellet
thermal_expansion_coeff = 10.0e-6
temperature = temperature
stress_free_temperature = 295.0
eigenstrain_name = fuel_thermal_eigenstrain
[]
[fuel_volumetric_swelling]
type = UO2VolumetricSwellingEigenstrain
gas_swelling_model_type = SIFGRS
block = pellet
temperature = temperature
burnup_function = burnup
initial_fuel_density = 10431.0
eigenstrain_name = fuel_volumetric_eigenstrain
[]
[fission_gas_release]
type = UO2Sifgrs
block = pellet
temperature = temperature
burnup_function = burnup
grain_radius = grain_radius
gbs_model = true
[]
[clad_density]
type = Density
block = clad
density = 6550.
[]
[clad_thermal]
block = clad
type = ZryThermal
temperature = temperature
[]
[clad_thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = clad
temperature = temperature
stress_free_temperature = 295.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = clad
temperature = temperature
[]
[zry_thermal_creep]
type = ZryCreepLOCAUpdate
block = clad
temperature = temperature
model_irradiation_creep = true
model_primary_creep = true
model_thermal_creep = true
max_inelastic_increment = 5e-4
fast_neutron_flux = fast_neutron_flux
fast_neutron_fluence = fast_neutron_fluence
zircaloy_material_type = zirlo
[]
[clad_stress]
type = ComputeMultipleInelasticStress
tangent_operator = elastic
inelastic_models = 'zry_thermal_creep'
block = clad
[]
[clad_irradiation_growth]
type = ZryIrradiationGrowthEigenstrain
block = clad
fast_neutron_fluence = fast_neutron_fluence
zircaloy_material_type = zirlo
eigenstrain_name = clad_irradiation_eigenstrain
[]
[clad_phase]
type = ZrPhase
block = clad
temperature = temperature
numerical_method = 2
[]
[clad_oxidation]
type = ZryOxidation
boundary = 2
temperature = temperature
clad_inner_radius = 4.18e-03
clad_outer_radius = 4.75e-03
normal_operating_temperature_model = epri_kwu_ce
high_temperature_model = leistikow
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = 2
failure_criterion = overstrain
# effective_strain_rate_creep = creep_strain_rate
# failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = stress_zz
hoop_creep_strain = creep_strain_zz
fraction_beta_phase = fract_beta_phase
fraction_oxygen_gain = oxywtfract_total
temperature = temperature
[]
[fuel_density]
type = Density
block = pellet
[]
[]
[Dampers]
[limitT]
type = BoundingValueElementDamper
min_value = 290.0
max_value = 3000.0
variable = temperature
[]
[limitX]
type = MaxIncrement
max_increment = 1e-5
variable = disp_x
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
l_max_its = 50
l_tol = 8e-3
nl_max_its = 15
nl_rel_tol = 1e-4
nl_abs_tol = 1e-8
start_time = -10
n_startup_steps = 1
end_time = 166842000
dtmax = 1e6
dtmin = 1e-6
[TimeStepper]
type = IterationAdaptiveDT
timestep_limiting_postprocessor = material_timestep
dt = 10
optimal_iterations = 20
iteration_window = 4
linear_iteration_ratio = 100
growth_factor = 2
cutback_factor = .5
timestep_limiting_function = forced_times
force_step_every_function_point = true
[]
[Quadrature]
order = FIFTH
side_order = SEVENTH
[]
[]
[Postprocessors]
[ave_temp_interior]
type = SideAverageValue
boundary = 9
variable = temperature
execute_on = 'initial linear'
[]
[clad_inner_vol]
type = InternalVolume
boundary = 7
#outputs = exodus
execute_on = 'initial timestep_end'
[]
[fission_gas_produced] # fission gas produced (moles)
type = ElementIntegralFisGasGeneratedSifgrs
block = pellet
execute_on = 'linear'
[]
[fission_gas_grain]
type = ElementIntegralFisGasGrainSifgrs
block = pellet
outputs = exodus
execute_on = 'linear'
[]
[fission_gas_boundary]
type = ElementIntegralFisGasBoundarySifgrs
block = pellet
outputs = exodus
execute_on = 'linear'
[]
[flux_from_clad] # area integrated heat flux from the cladding
type = SideDiffusiveFluxIntegral
variable = temperature
boundary = 5
diffusivity = thermal_conductivity
[]
[flux_from_fuel] # area integrated heat flux from the fuel
type = SideDiffusiveFluxIntegral
variable = temperature
boundary = 10
diffusivity = thermal_conductivity
[]
[rod_total_power]
type = ElementIntegralPower
variable = temperature
burnup_function = burnup
block = pellet
[]
[rod_input_power]
type = FunctionValuePostprocessor
function = power_history
scale_factor = 0.1186 # rod height
[]
[max_fuel_temp]
type = NodalExtremeValue
block = pellet
value_type = max
variable = temperature
[]
[max_clad_temp]
type = NodalExtremeValue
block = clad
value_type = max
variable = temperature
[]
[max_clad_hoop_strain]
type = ElementExtremeValue
block = clad
value_type = max
variable = strain_zz
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = clad
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
block = clad
execute_on = 'initial timestep_end'
[]
[volume_pulverized]
type = ElementIntegralMaterialProperty
mat_prop = pulverized
block = pellet
[]
[max_fuel_temp_periphery]
type = NodalExtremeValue
value_type = max
variable = temperature
boundary = 10
[]
[additional_volume]
type = FunctionValuePostprocessor
function = 8.5e-6
execute_on = 'initial linear'
[]
[addition_temperature]
type = FunctionValuePostprocessor
function = 300.0
execute_on = 'initial linear'
[]
[equilibrium_pressure]
type = FunctionValuePostprocessor
function = 101325.0
execute_on = 'initial linear'
[]
[]
[PerformanceMetricOutputs]
[]
[StandardLWRFuelRodOutputs]
temperature = temperature
fuel_pellet_blocks = 3
[]
[Outputs]
perf_graph = true
exodus = true
color = false
csv = true
[checkpoint]
type = Checkpoint
num_files = 2
[]
[chkfile]
type = CSV
execute_on = FINAL
show = 'volume_pulverized'
[]
[]
(assessment/LWR/validation/LOCA_REBEKA_cladding_burst_tests/analysis/rebeka_2d_08MPa/rebeka_singlerod_2d_08MPa_aniso.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
order = SECOND
family = LAGRANGE
displacements = 'disp_x disp_y'
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = rebeka_singlerod.e
[]
[]
[Variables]
[temperature]
initial_condition = 573.0
[]
[]
[Functions]
[temperature_func]
type = PiecewiseLinear
x = '0. 700. '
y = '573. 1273.' # From 300 to 1000 C at 1 K/s
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 700. '
y = '8.e+06 8.e+06' # 80 bar
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 700. '
y = '1.e+05 1.e+05' # atmospheric pressure
[]
# Circumferential steady-state creep test and analysis of Zircaloy-4 fuel cladding
# Nuclear Engineering and Design, 53, 2312-2322 (2021)
[F]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.738 0.738 0.57'
[]
[G]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.174 0.174 0.45'
[]
[H]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.588 0.588 0.48'
[]
[L]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[M]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[N]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[clad]
block = cladding
add_variables = true
strain = FINITE
decomposition_method = TaylorExpansion
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz hoop_stress'
use_automatic_differentiation = true
[]
[]
[AuxVariables]
[creep_rate_aux]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[scale_thickness]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfract_total]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfgain_total]
order = CONSTANT
family = MONOMIAL
[]
[burst_stress]
order = CONSTANT
family = MONOMIAL
[]
[burst]
order = CONSTANT
family = MONOMIAL
[]
[]
[Kernels]
[heat]
type = ADHeatConduction
variable = temperature
[]
[heat_ie]
type = ADHeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate_aux]
type = ADMaterialRealAux
variable = creep_rate_aux
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = ADMaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[scl_thickness]
type = ADMaterialRealAux
variable = scale_thickness
property = oxide_scale_thickness
boundary = 2
[]
[ofract_total]
type = ADMaterialRealAux
variable = oxywtfract_total
property = current_oxygen_weight_frac_total
boundary = 2
[]
[ofgain_total]
type = ADMaterialRealAux
boundary = 2
variable = oxywtfgain_total
property = oxygen_weight_frac_gained_total
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = 2
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = 2
execute_on = timestep_end
[]
[]
[BCs]
[inner_temperature]
type = REBEKADirichletBC
variable = temperature
function_tempm = temperature_func
minimum_temperature = 573.
translation = 0.1625
boundary = 4
[]
[no_y_midsection]
type = ADDirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply steam pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 101 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[CoolantChannel]
[convective_clad_surface]
boundary = 2
variable = temperature
inlet_temperature = 473.
inlet_pressure = 1.e+05
inlet_massflux = 1.0 # kg/m^2-sec # almost stagnant steam
rod_diameter = 10.75e-03
rod_pitch = 1.26e-02 # default
oxide_thickness = scale_thickness
number_axial_zone = 15
use_ad = true
[]
[]
[Materials]
[converter]
type = MaterialADConverter
reg_props_in = 'fract_beta_phase'
ad_props_out = 'ad_fract_beta_phase'
[]
[thermal]
type = ADZryThermal
block = cladding
temperature = temperature
[]
[clad_elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
block = cladding
youngs_modulus = 1.0e11
poissons_ratio = 0.3
[]
[clad_stress]
type = ADComputeMultipleInelasticStress
inelastic_models = 'clad_zrycreep'
block = cladding
[]
[hill_constants]
type = ADHillConstants
hill_constants = "0.738 0.174 0.588 1.0 1.0 1.0"
function_names = "F G H L M N"
temperature = temperature
[]
[clad_zrycreep]
type = ADZryAnisoCreepLOCAUpdate
block = cladding
temperature = temperature
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
temperature_loca_creep_begin = 501
temperature_standard_thermal_creep_end = 500
fract_beta_phase_name = 'ad_fract_beta_phase'
[]
[thermal_expansion]
type = ADZryThermalExpansionMATPROEigenstrain
block = cladding
temperature = temperature
stress_free_temperature = 573.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[density]
type = ADDensity
block = cladding
[]
[phase]
type = ZrPhase
block = cladding
temperature = temperature
numerical_method = 2
[]
[oxidation]
type = ADZryOxidation
boundary = 2
temperature = temperature
clad_inner_radius = 0.00465
clad_outer_radius = 0.005375
normal_operating_temperature_model = epri_kwu_ce
high_temperature_model = leistikow
use_coolant_channel = true
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = 2
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate_aux
temperature = temperature
fraction_beta_phase = fract_beta_phase
fraction_oxygen_gain = oxywtfgain_total
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-06
nl_abs_tol = 1.e-08
start_time = 0
n_startup_steps = 1
end_time = 700.
dtmax = 1.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[Postprocessors]
[ave_clad_exterior_temp]
type = SideAverageValue
boundary = 2
variable = temperature
[]
[max_clad_temp]
type = NodalExtremeValue
block = cladding
value_type = max
variable = temperature
[]
[min_clad_temp]
type = NodalExtremeValue
block = cladding
value_type = min
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = cladding
[]
[max_oxygen_fract]
type = ElementExtremeValue
block = cladding
value_type = max
variable = oxywtfract_total
[]
[max_betaph_fract]
type = ElementExtremeValue
block = cladding
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
block = cladding
value_type = max
variable = creep_rate_aux
[]
[max_creep_strain_mag]
type = ElementExtremeValue
block = cladding
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
block = cladding
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
block = cladding
value_type = max
variable = hoop_stress
[]
[vonmises_stress_clad]
type = ElementAverageValue
block = cladding
variable = vonmises_stress
[]
[min_burst_stress]
type = ElementExtremeValue
block = cladding
value_type = min
variable = burst_stress
[]
[burst]
type = ElementExtremeValue
block = cladding
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = cladding
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[top_disp_r_clad] # this is mid height
type = NodalVariableValue
variable = disp_x
nodeid = 0 #coords (0.005375, 0.1625)
[]
[top_disp_r_clad_slice] # this is mid height matched to the 1.5d
type = NodalVariableValue
variable = disp_x
nodeid = 3 #coords (0.005375, 0.1625)
[]
[top_disp_z_clad]
type = NodalVariableValue
variable = disp_y
nodeid = 0 #coords (0.005375, 0.1625)
[]
[stress_xx] # stess in the top Element
type = ElementalVariableValue
variable = stress_xx
elementid = 0
[]
[stress_yy] # stess in the top Element
type = ElementalVariableValue
variable = stress_yy
elementid = 0
[]
[stress_zz] # stess in the top Element
type = ElementalVariableValue
variable = stress_zz
elementid = 0
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = cladding
plenum_boundary_name = 4
external_clad_boundary_name = 2
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = rebeka_2d_08MPa_aniso_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
(test/tests/zry_oxidation_cladding/alt_oxidation_cladding_zry.i)
# This test demonstrates the usage of the model for cladding oxidation from
# normal operating to high temperature (accident) conditions, through the
# epri_sli, Cathcart, and Prater relations.
#
# The mesh is a 1x1 square, with temperature boundary conditions on the right
# (coolant side) ramping from 600K to 1950K, no displacement boundary conditions.
#
# The final oxidation thickness expected is 4.047e-4 m and the final total gained
# oxygen concentration is 7.264e-1 kg/m^3, from hand calculations performed alongside
# the BISON simulation.
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Mesh]
[mesh]
type = GeneratedMeshGenerator
dim = 2
nx = 1
ny = 1
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
elem_type = QUAD4
[]
[]
[Functions]
[out_temp_func]
type = PiecewiseLinear
x = '0. 100000000. 100000010. 100000100. 100000110. 100000200. 100000210. 100000300.'
y = '600. 600. 1100. 1100. 1850. 1850. 1950. 1950. '
[]
[in_temp_func]
type = PiecewiseLinear
x = '0. 100000000. 100000010. 100000100. 100000110. 100000200. 100000210. 100000300.'
y = '800. 800. 1200. 1200. 1850. 1850. 1950. 1950. '
[]
[FNFlux_func]
type = PiecewiseLinear
x = '0. 100000300.'
y = '1.e+17 1.e+17 '
[]
[]
[Variables]
[temp]
order = FIRST
family = LAGRANGE
initial_condition = 600.
[]
[disp_x]
order = FIRST
family = LAGRANGE
[]
[disp_y]
order = FIRST
family = LAGRANGE
[]
[]
[AuxVariables]
[fast_neutron_flux]
order = FIRST
family = LAGRANGE
initial_condition = 1.0e+17
[]
[scale_thickness] # ZrO2 scale thickness (m)
order = CONSTANT
family = MONOMIAL
[]
[oxyconc2_scale] # Oxygen concentration in ZrO2 scale (kg/m**2)
order = CONSTANT
family = MONOMIAL
[]
[oxyconc2_metal] # Oxygen concentration in metal (kg/m**2)
order = CONSTANT
family = MONOMIAL
[]
[oxyconc2_total] # Total oxygen concentration (oxide + metal) (kg/m**2)
order = CONSTANT
family = MONOMIAL
[]
[oxywtfract_metal] # Oxygen weight fraction in metal (/)
order = CONSTANT
family = MONOMIAL
[]
[oxywtfract_total] # Total oxygen weight fraction (oxide+metal) (/)
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[all]
strain = finite
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temp
[]
[]
[AuxKernels]
[fnflux]
type = FastNeutronFluxAux
variable = fast_neutron_flux
#block = 1
function = FNFlux_func
execute_on = timestep_begin
[]
[scl_thickness]
type = MaterialRealAux
variable = scale_thickness
property = oxide_scale_thickness
boundary = 'right'
[]
[oconc_scale]
type = MaterialRealAux
variable = oxyconc2_scale
property = gained_oxygen_concentration_scale
boundary = 'right'
[]
[oconc_metal]
type = MaterialRealAux
variable = oxyconc2_metal
property = gained_oxygen_concentration_metal_wall
boundary = 'right'
[]
[oconc_total]
type = MaterialRealAux
variable = oxyconc2_total
property = gained_oxygen_concentration_total
boundary = 'right'
[]
[ofract_metal]
type = MaterialRealAux
variable = oxywtfract_metal
property = current_oxygen_weight_frac_metal_wall
boundary = 'right'
[]
[ofract_total]
type = MaterialRealAux
variable = oxywtfract_total
property = current_oxygen_weight_frac_total
boundary = 'right'
[]
[]
[BCs]
[right_T]
type = FunctionDirichletBC
variable = temp
boundary = 'right'
function = out_temp_func
[]
[left_du]
type = FunctionDirichletBC
variable = temp
boundary = 'left'
function = in_temp_func
[]
[x_disp]
type = DirichletBC
variable = disp_x
value = 0
boundary = 'left'
[]
[y_disp]
type = DirichletBC
variable = disp_y
value = 0
boundary = 'bottom'
[]
[]
[Materials]
[elasticity_tensor]
type = ZryElasticityTensor
#block = 1
[]
[stress]
type = ComputeFiniteStrainElasticStress
#block = 1
[]
[thermal]
type = ZryThermal
#block = 1
temperature = temp
[]
[oxidation_zry]
type = ZryOxidation
boundary = 'right'
clad_inner_radius = 0.004650
clad_outer_radius = 0.005375
normal_operating_temperature_model = epri_sli
high_temperature_model = cathcart
temperature = temp
fast_neutron_flux = fast_neutron_flux
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = 'lu superlu_dist'
l_tol = 1.e-08
nl_abs_tol = 1.e-08
nl_rel_tol = 1.e-08
start_time = 0.
num_steps = 5000 #5000
end_time = 100000300 #*100
[TimeStepper]
type = IterationAdaptiveDT
dt = 1.e+06
optimal_iterations = 6
iteration_window = 2
linear_iteration_ratio = 100
time_t = '0. 100000000.'
time_dt = '1.e+06 10. '
growth_factor = 1.
[]
[]
[Postprocessors]
[_dt]
type = TimestepSize
[]
[temp]
type = NodalVariableValue
variable = temp
nodeid = 0
execute_on = 'initial timestep_end'
[]
[scale_thickness]
type = ElementalVariableValue
elementid = 0
variable = scale_thickness
[]
[oxyconc2_scale]
type = ElementalVariableValue
elementid = 0
variable = oxyconc2_scale
[]
[oxyconc2_metal]
type = ElementalVariableValue
elementid = 0
variable = oxyconc2_metal
[]
[oxyconc2_total]
type = ElementalVariableValue
elementid = 0
variable = oxyconc2_total
[]
[oxywtfract_metal]
type = ElementalVariableValue
elementid = 0
variable = oxywtfract_metal
[]
[oxywtfract_total]
type = ElementalVariableValue
elementid = 0
variable = oxywtfract_total
[]
[]
[Outputs]
file_base = alt_oxidation_cladding_zry_out
[exodus]
type = Exodus
[]
[]
(assessment/LWR/validation/LOCA_Studsvik/analysis/rod_191/Studsvik_191_part1_1p5d_fr_frd.i)
[GlobalParams]
density = 10431.0
initial_porosity = 0.05
order = SECOND
family = LAGRANGE
energy_per_fission = 3.2e-11 # J/fission
volumetric_locking_correction = false
displacements = 'disp_x'
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
[]
[Mesh]
coord_type = RZ
[layered1D_mesh]
type = Layered1DMeshGenerator
slices_per_block = 10
clad_gap_width = 8.0e-5
clad_thickness = 0.57e-3
fuel_height = 0.265388558
plenum_height = 0.034861442
elem_type = EDGE3
nx_p = 11
pellet_mesh_density = customize
[]
patch_update_strategy = auto
partitioner = centroid
centroid_partitioner_direction = y
[]
[Variables]
# Define dependent variables and initial conditions
[temperature]
initial_condition = 295.0 # set initial temp to coolant inlet
[]
[]
[AuxVariables]
[strain_yy_0]
order = CONSTANT
family = MONOMIAL
[]
# Define auxilary variables
[tangential_contact_pressure_aux]
block = fuel
[]
[fast_neutron_flux]
block = clad
[]
[fast_neutron_fluence]
block = clad
[]
[grain_radius]
block = fuel
initial_condition = 10e-6
[]
[creep_strain_rate]
order = CONSTANT
family = MONOMIAL
[]
[effective_creep_strain]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[hoop_strain]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[scale_thickness] # ZrO2 scale thickness (m)
order = CONSTANT
family = MONOMIAL
[]
[oxywtfract_total] # Current oxigen weight fraction (oxide+metal) (/)
order = CONSTANT
family = MONOMIAL
[]
[oxywtfgain_total] # Gained oxygen weight fraction (oxide+metal) (/)
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[gap_cond]
order = CONSTANT
family = MONOMIAL
[]
[]
[Functions]
[power_history]
type = PiecewiseLinear
data_file = power_history.csv
format = columns
scale_factor = 1
[]
[axial_peaking_factors]
type = ParsedFunction
expression = 1
[]
[pressure_ramp] # reads and interpolates input data defining amplitude curve for fill gas pressure
type = PiecewiseLinear
x = '-200 0 166755600 166842000'
y = '0.006537 1 1 0.006537'
scale_factor = 15.5e6
[]
[forced_times]
type = PiecewiseLinear
data_file = timestep_limiting.csv
scale_factor = 1
format = columns
[]
[clad_axial_pressure]
type = CladdingAxialPressureFunction
plenum_pressure = plenum_pressure
coolant_pressure = pressure_ramp
coolant_pressure_scaling_factor = 1.0
fuel_pin_geometry = fuel_pin_geometry
[]
[fuel_axial_pressure]
type = ParsedFunction
expression = plenum_pressure
symbol_names = plenum_pressure
symbol_values = plenum_pressure
[]
[]
[Physics]
[SolidMechanics]
[Layered1D]
[fuel]
block = fuel
add_variables = true
add_scalar_variables = true
strain = FINITE
out_of_plane_strain_name = strain_yy
eigenstrain_names = 'fuel_thermal_eigenstrain fuel_volumetric_eigenstrain axial_relocation_eigenstrain'
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress strain_xx hoop_stress creep_strain_zz strain_zz'
extra_vector_tags = 'ref'
fuel_pin_geometry = fuel_pin_geometry
group_scalar_vars_in_reference_residual = true
mesh_generator = layered1D_mesh
decomposition_method = EigenSolution
temperature = temperature
layer_friction_user_object = 1DFriction_secondary
out_of_plane_pressure_function = fuel_axial_pressure
[]
[clad]
block = clad
add_variables = true
add_scalar_variables = true
strain = FINITE
out_of_plane_strain_name = strain_yy
eigenstrain_names = 'clad_thermal_eigenstrain clad_irradiation_eigenstrain'
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress strain_xx hoop_stress creep_strain_zz strain_zz'
extra_vector_tags = 'ref'
fuel_pin_geometry = fuel_pin_geometry
group_scalar_vars_in_reference_residual = true
mesh_generator = layered1D_mesh
decomposition_method = EigenSolution
temperature = temperature
layer_friction_user_object = 1DFriction_primary
out_of_plane_pressure_function = clad_axial_pressure
[]
[]
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
extra_vector_tags = 'ref'
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
extra_vector_tags = 'ref'
[]
[heat_source]
type = NeutronHeatSource
variable = temperature
extra_vector_tags = 'ref'
block = fuel
burnup_function = burnup
axial_relocation_object = axial_relocation
[]
[]
[Burnup]
[burnup]
block = fuel
rod_ave_lin_pow = power_history # using the power function defined above
axial_power_profile = axial_peaking_factors # using the axial power profile function defined above
num_radial = 80
num_axial = 11
fuel_pin_geometry = fuel_pin_geometry
fuel_volume_ratio = 1.0 # for use with dished pellets (ratio of actual volume to cylinder volume)
order = CONSTANT
family = MONOMIAL
RPF = RPF
isotopes = 'U235 U238 Pu239 Pu240 Pu241 Pu242'
isotope_fractions = '0.05 0.95 0 0 0 0'
[]
[]
[AuxKernels]
[tangential_contact_pressure_aux]
type = SpatialUserObjectAux
variable = tangential_contact_pressure_aux
user_object = 1DFriction_secondary
block = fuel
execute_on = 'TIMESTEP_END'
[]
# Define auxilliary kernels for each of the aux variables
[fast_neutron_flux]
type = FastNeutronFluxAux
variable = fast_neutron_flux
block = clad
rod_ave_lin_pow = power_history
axial_power_profile = axial_peaking_factors
factor = 3e13
execute_on = timestep_begin
[]
[fast_neutron_fluence]
type = FastNeutronFluenceAux
variable = fast_neutron_fluence
block = clad
fast_neutron_flux = fast_neutron_flux
execute_on = timestep_begin
[]
[grain_radius]
type = GrainRadiusAux
block = fuel
variable = grain_radius
temperature = temperature
execute_on = linear
[]
[creep_strain_rate]
type = MaterialRealAux
property = creep_rate
variable = creep_strain_rate
block = clad
[]
[effective_creep_strain]
type = MaterialRealAux
property = effective_creep_strain
variable = effective_creep_strain
block = clad
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
block = clad
variable = fract_beta_phase
property = fract_beta_phase
[]
[scl_thickness]
type = MaterialRealAux
boundary = 2
variable = scale_thickness
property = oxide_scale_thickness
[]
[ofract_total]
type = MaterialRealAux
boundary = 2
variable = oxywtfract_total
property = current_oxygen_weight_frac_total
[]
[ofgain_total]
type = MaterialRealAux
boundary = 2
variable = oxywtfgain_total
property = oxygen_weight_frac_gained_total
[]
[sigmaburst]
type = MaterialRealAux
boundary = 2
variable = burst_stress
property = burst_stress
[]
[hasburst]
type = MaterialRealAux
boundary = 2
variable = burst
property = failed
execute_on = timestep_end
[]
[conductance]
type = MaterialRealAux
property = gap_conductance
variable = gap_cond
boundary = 10
execute_on = 'linear'
[]
[]
[Contact]
[pellet_clad_mechanical]
primary = 5
secondary = 10
formulation = kinematic
model = frictionless
penalty = 1e7
[]
[]
[ThermalContact]
[thermal_contact]
type = GasGapHeatTransfer
variable = temperature
primary = 5
secondary = 10
initial_moles = initial_moles
gas_released = fission_gas_released
quadrature = true
contact_pressure = contact_pressure
refab_gas_types = He
refab_fractions = 1
refab_time = 166842000
refab_type = 0
[]
[]
[BCs]
[no_x_all]
type = DirichletBC
variable = disp_x
boundary = 12
value = 0.0
[]
[Pressure]
[coolantPressure]
boundary = '2'
function = pressure_ramp
[]
[]
[PlenumPressure]
[plenumPressure]
boundary = 9
initial_pressure = 3.44738e6
startup_time = 0
R = 8.3143
output_initial_moles = initial_moles
temperature = plenum_temp
volume = plenum_volume
material_input = fission_gas_released
output = plenum_pressure
refab_time = 166842000
refab_pressure = 11e6
refab_temperature = 295.0
refab_volume = 1.04e-05
cladding_failure_status = burst
equilibrium_pressure = equilibrium_pressure
additional_volumes = additional_volume
temperature_of_additional_volumes = addition_temperature
[]
[]
[]
[UserObjects]
# Fuel dispersal
[layered_average_hoop_strain]
type = LayeredAverage
block = clad
num_layers = 10
direction = y
variable = strain_zz
[]
[cladding_strain_yy]
type = LayeredAverage
block = clad
num_layers = 11
direction = y
variable = strain_yy
execute_on = 'initial timestep_end'
[]
[fuel_strain_yy]
type = LayeredAverage
block = fuel
num_layers = 10
direction = y
variable = strain_yy
execute_on = 'initial timestep_end'
[]
# We could have two element UOs to obtain interface stress
[1DContactStressOOP_fuel]
type = Layered1DContactInterfaceStress
direction = y
stress_name = stress
num_layers = 10
# If we do not provide the numbers below, it will look at the mesh, in all blocks to set the layer number. Then, it will
# be wrong because the cladding has more height and won't be able to identify layers in the fuel.
direction_min = 0.0165094
direction_max = 0.255359
block = fuel
execute_on = 'LINEAR NONLINEAR'
[]
[1DContactStressOOP_cladding]
type = Layered1DContactInterfaceStress
direction = y
stress_name = stress
num_layers = 10
# If we do not provide the numbers below, it will look at the mesh, in all blocks to set the layer number. Then, it will
# be wrong because the cladding has more height and won't be able to identify layers in the fuel.
direction_min = 0.0165094
direction_max = 0.255359
block = clad
execute_on = 'LINEAR NONLINEAR'
[]
[1DFriction_secondary]
type = Layered1DFrictionalForce
force_postaux = true
contact_pressure = contact_pressure
direction = y
boundary = pellet_outer_radial_surface
num_layers = 10
interface_oop_stress_provider_fuel = 1DContactStressOOP_fuel
interface_oop_stress_provider_cladding = 1DContactStressOOP_cladding
is_secondary_side = true
tangential_pressure = tangential_contact_pressure_aux
friction_coefficient = 0.2
thickness = 0.0265
penalty_factor = 1.0e13
# If we do not provide the numbers below, it will look at the mesh, in all blocks to set the layer number. Then, it will
# be wrong because the cladding has more height and won't be able to identify layers in the fuel.
direction_min = 0.0165094
direction_max = 0.255359
scalar_var_name_base_fuel = scalar_strain_yy_fuel
scalar_num_variable_fuel = 10
scalar_var_name_base_cladding = scalar_strain_yy_clad
scalar_num_variable_cladding = 10
execute_on = 'LINEAR NONLINEAR'
[]
[1DFriction_primary]
type = Layered1DFrictionalForce
force_postaux = true
contact_pressure = contact_pressure
direction = y
boundary = clad_inside_right
num_layers = 10
# If we do not provide the numbers below, it will look at the mesh, in all blocks to set the layer number. Then, it will
# be wrong because the cladding has more height and won't be able to identify layers in the fuel.
direction_min = 0.0165094
direction_max = 0.255359
interface_oop_stress_provider_fuel = 1DContactStressOOP_fuel
interface_oop_stress_provider_cladding = 1DContactStressOOP_cladding
is_secondary_side = false
secondary_side_frictional_user_object = 1DFriction_secondary
friction_coefficient = 0.2
thickness = 0.0265
penalty_factor = 1.0e13
scalar_var_name_base_fuel = scalar_strain_yy_fuel
scalar_num_variable_fuel = 10
scalar_var_name_base_cladding = scalar_strain_yy_clad
scalar_num_variable_cladding = 10
execute_on = 'LINEAR NONLINEAR'
[]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[]
[PlenumTemperature]
[plenum_temp]
boundary = 5
inner_surfaces = '5'
outer_surfaces = '10'
temperature = temperature
[]
[]
[CoolantChannel]
[convective_clad_surface] # apply convective boundary to clad outer surface
boundary = 2
variable = temperature
inlet_temperature = 580
inlet_pressure = 15.5e6 # Pa
inlet_massflux = 3800 # kg/m^2-sec
rod_diameter = 0.0095 # m
rod_pitch = 1.26e-2 # m
compute_enthalpy = false
linear_heat_rate = power_history
axial_power_profile = axial_peaking_factors
output_properties = 'coolant_channel_htype coolant_channel_hmode'
[]
[]
[Materials]
[fuel_dispersal]
type = UO2Dispersal
block = fuel
axial_relocation_object = axial_relocation
layered_average_burnup = layered_average_burnup
layered_average_hoop_strain = layered_average_hoop_strain
dispersal_model = ONE_MM_TWO_PERCENT_STRAIN
[]
# Define material behavior models and input material property data
[fuel_thermal] # temperature and burnup dependent thermal properties of UO2 (BISON kernel)
type = UO2Thermal
block = fuel
thermal_conductivity_model = NFIR
temperature = temperature
burnup_function = burnup
axial_relocation_object = axial_relocation
gap_thermal_conductivity = layered_average_gap_conductivity
[]
[fuel_elasticity_tensor]
type = UO2IsotropicDamageElasticityTensor
block = fuel
fragmentation_model = BARANI
temperature = temperature
rod_ave_lin_pow = power_history
axial_relocation_object = axial_relocation
[]
[fuel_elastic_stress]
type = ComputeMultipleInelasticStress
tangent_operator = elastic
inelastic_models = 'fuel_creep'
block = fuel
[]
[fuel_creep]
type = UO2CreepUpdate
block = fuel
temperature = temperature
fission_rate = fission_rate
initial_grain_radius = 10.0e-6
oxygen_to_metal_ratio = 2.0
[]
[fuel_thermal_expansion]
type = ComputeThermalExpansionEigenstrain
block = fuel
thermal_expansion_coeff = 10.0e-6
temperature = temperature
stress_free_temperature = 295.0
eigenstrain_name = fuel_thermal_eigenstrain
[]
[fuel_volumetric_swelling]
type = UO2VolumetricSwellingEigenstrain
gas_swelling_model_type = SIFGRS
block = fuel
temperature = temperature
burnup_function = burnup
initial_fuel_density = 10431.0
eigenstrain_name = fuel_volumetric_eigenstrain
[]
[fission_gas_release]
type = UO2Sifgrs
block = fuel
temperature = temperature
burnup_function = burnup
grain_radius = grain_radius
gbs_model = true
[]
[clad_density]
type = Density
block = clad
density = 6550.
[]
[clad_thermal]
block = clad
type = ZryThermal
temperature = temperature
[]
[clad_thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = clad
temperature = temperature
stress_free_temperature = 295.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = clad
temperature = temperature
[]
[zry_thermal_creep]
type = ZryCreepLOCAUpdate
block = clad
temperature = temperature
model_irradiation_creep = true
model_primary_creep = true
model_thermal_creep = true
max_inelastic_increment = 5e-4
fast_neutron_flux = fast_neutron_flux
fast_neutron_fluence = fast_neutron_fluence
zircaloy_material_type = zirlo
[]
[clad_stress]
type = ComputeMultipleInelasticStress
tangent_operator = elastic
inelastic_models = 'zry_thermal_creep'
block = clad
[]
[clad_irradiation_growth]
type = ZryIrradiationGrowthEigenstrain
block = clad
fast_neutron_fluence = fast_neutron_fluence
zircaloy_material_type = zirlo
eigenstrain_name = clad_irradiation_eigenstrain
[]
[clad_phase]
type = ZrPhase
block = clad
temperature = temperature
numerical_method = 2
[]
[clad_oxidation]
type = ZryOxidation
boundary = 2
temperature = temperature
clad_inner_radius = 4.18e-03
clad_outer_radius = 4.75e-03
normal_operating_temperature_model = epri_kwu_ce
high_temperature_model = leistikow
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = 2
failure_criterion = overstrain
hoop_stress = hoop_stress
hoop_creep_strain = creep_strain_zz
fraction_beta_phase = fract_beta_phase
fraction_oxygen_gain = oxywtfract_total
temperature = temperature
[]
[fuel_density]
type = Density
block = fuel
[]
[]
[Dampers]
[limitT]
type = BoundingValueElementDamper
min_value = 290.0
max_value = 3000.0
variable = temperature
[]
[limitX]
type = MaxIncrement
max_increment = 1e-5
variable = disp_x
[]
[]
[AxialRelocation]
[relocation]
rod_ave_lin_pow = power_history
axial_direction = y
fuel_blocks = fuel
clad_blocks = clad
contact_pressure_variable = contact_pressure
out_of_plane_strain_variable = strain_yy_0
penetration_variable = penetration
clad_inner_volume_addition = 0
burnup_variable = burnup
temperature = temperature
axial_relocation_output_options = MASS_FRACTION
mesh_generator = layered1D_mesh
# CHANGE
gap_thickness_threshold = 0.000050
[]
[]
[Postprocessors]
[volume_fuel_dispersed]
type = LayeredElementIntegralMaterialProperty
block = fuel
mat_prop = dispersed
fuel_pin_geometry = fuel_pin_geometry
execute_on = 'initial timestep_end'
[]
[mass_fuel_dispersed]
type = ParsedPostprocessor
pp_names = volume_fuel_dispersed
expression = '10431 * volume_fuel_dispersed'
execute_on = 'initial timestep_end'
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
l_max_its = 50
l_tol = 8e-3
nl_max_its = 15
nl_rel_tol = 1e-4
nl_abs_tol = 1e-8
start_time = -10
n_startup_steps = 1
end_time = 166842000
dtmax = 1e6
dtmin = 1e-6
[TimeStepper]
type = IterationAdaptiveDT
timestep_limiting_postprocessor = material_timestep
dt = 10
optimal_iterations = 20
iteration_window = 4
linear_iteration_ratio = 100
growth_factor = 2
cutback_factor = .5
timestep_limiting_function = forced_times
force_step_every_function_point = true
[]
[Quadrature]
order = FIFTH
side_order = SEVENTH
[]
[]
[Postprocessors]
[ave_temp_interior]
type = SideAverageValue
boundary = 9
variable = temperature
execute_on = 'initial linear'
[]
[clad_inner_vol]
type = InternalVolume
boundary = 7
#outputs = exodus
execute_on = 'initial timestep_end'
[]
[fission_gas_produced] # fission gas produced (moles)
type = ElementIntegralFisGasGeneratedSifgrs
block = fuel
execute_on = 'linear'
[]
[fission_gas_grain]
type = ElementIntegralFisGasGrainSifgrs
block = fuel
outputs = exodus
execute_on = 'linear'
[]
[fission_gas_boundary]
type = ElementIntegralFisGasBoundarySifgrs
block = fuel
outputs = exodus
execute_on = 'linear'
[]
[flux_from_clad] # area integrated heat flux from the cladding
type = SideDiffusiveFluxIntegral
variable = temperature
boundary = 5
diffusivity = thermal_conductivity
[]
[flux_from_fuel] # area integrated heat flux from the fuel
type = SideDiffusiveFluxIntegral
variable = temperature
boundary = 10
diffusivity = thermal_conductivity
[]
[rod_total_power]
type = ElementIntegralPower
variable = temperature
burnup_function = burnup
block = fuel
[]
[max_fuel_temp]
type = NodalExtremeValue
block = fuel
value_type = max
variable = temperature
[]
[max_clad_temp]
type = NodalExtremeValue
block = clad
value_type = max
variable = temperature
[]
[max_clad_hoop_strain]
type = ElementExtremeValue
block = clad
value_type = max
variable = strain_zz
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = clad
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
block = clad
execute_on = 'initial timestep_end'
[]
[volume_pulverized]
type = ElementIntegralMaterialProperty
mat_prop = pulverized
block = fuel
[]
[max_fuel_temp_periphery]
type = NodalExtremeValue
value_type = max
variable = temperature
boundary = 10
[]
[additional_volume]
type = FunctionValuePostprocessor
function = 8.5e-6
execute_on = 'initial linear'
[]
[addition_temperature]
type = FunctionValuePostprocessor
function = 300.0
execute_on = 'initial linear'
[]
[equilibrium_pressure]
type = FunctionValuePostprocessor
function = 101325.0
execute_on = 'initial linear'
[]
[]
[VectorPostprocessors]
[cladding_outer]
type = NodalValueSampler
boundary = 5
variable = disp_x
sort_by = y
[]
[]
[PerformanceMetricOutputs]
[]
[StandardLWRFuelRodOutputs]
temperature = temperature
layered = true
fuel_pin_geometry = fuel_pin_geometry
fuel_pellet_blocks = 'fuel'
[]
[Outputs]
perf_graph = true
exodus = true
color = false
csv = true
[checkpoint]
type = Checkpoint
num_files = 2
[]
[chkfile]
type = CSV
execute_on = FINAL
show = 'volume_pulverized'
[]
[]
(assessment/LWR/validation/LOCA_ANL_cladding_burst_tests/analysis/OCL11/OCL11.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
displacements = 'disp_x disp_y'
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
[]
[Mesh]
coord_type = RZ
[smeared_pellet_mesh]
type = FuelPinMeshGenerator
pellet_quantity = 1
pellet_height = 0.270
pellet_outer_radius = 4.78e-3
clad_bot_gap_height = 0.001
clad_top_gap_height = 0.013
clad_thickness = 0.71e-3
clad_gap_width = 0.1e-3
pellet_mesh_density = coarse
clad_mesh_density = coarse
elem_type = QUAD8
[]
patch_size = 10
patch_update_strategy = auto
partitioner = centroid
centroid_partitioner_direction = y
[]
[Variables]
[temperature]
initial_condition = 300.0
[]
[]
[Functions]
[temperature_func]
type = PiecewiseLinear
x = '0 496.02 520.74 528.12 545.94 551.28 671.52 885.3 1195.74 1410.36 1657.86 1680 1690 1700 1710 1720 1730 1740 1750 1760 1770 1780 1790 1800 1810 1820 1830 1840 1848'
y = '300 300 405.465 482.048 583.351 632.287 634.297 632.825 630.378 631.059 632.59 633 683 733 783 833 883 933 983 1033 1083 1133 1183 1233 1283 1333 1383 1433 1477'
[]
[temperature_profile]
type = PiecewiseBilinear
data_file = 'temp_profile.csv'
axis = 1
[]
[cladding_temperature]
type = CompositeFunction
functions = 'temperature_func temperature_profile'
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[pellets]
block = pellet
add_variables = true
strain = FINITE
eigenstrain_names = 'fuel_thermal_strain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
generate_output = 'vonmises_stress hydrostatic_stress stress_xx stress_yy
stress_zz strain_xx strain_yy strain_zz hoop_stress'
extra_vector_tags = 'ref'
[]
[clad]
block = clad
add_variables = true
strain = FINITE
decomposition_method = EigenSolution
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz hoop_stress'
extra_vector_tags = 'ref'
[]
[]
[AuxVariables]
[creep_rate_aux]
order = CONSTANT
family = MONOMIAL
block = clad
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
block = clad
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
block = clad
[]
[scale_thickness]
order = CONSTANT
family = MONOMIAL
block = clad
[]
[oxywtfract_total]
order = CONSTANT
family = MONOMIAL
block = clad
[]
[oxywtfgain_total]
order = CONSTANT
family = MONOMIAL
block = clad
[]
[burst_stress]
order = CONSTANT
family = MONOMIAL
block = clad
[]
[burst]
order = CONSTANT
family = MONOMIAL
block = clad
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
extra_vector_tags = 'ref'
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
extra_vector_tags = 'ref'
[]
[]
[AuxKernels]
[creep_rate_aux]
type = MaterialRealAux
variable = creep_rate_aux
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
block = clad
[]
[scl_thickness]
type = MaterialRealAux
variable = scale_thickness
property = oxide_scale_thickness
boundary = clad_outside_right
[]
[ofract_total]
type = MaterialRealAux
variable = oxywtfract_total
property = current_oxygen_weight_frac_total
boundary = clad_outside_right
[]
[ofgain_total]
type = MaterialRealAux
boundary = clad_outside_right
variable = oxywtfgain_total
property = oxygen_weight_frac_gained_total
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = clad_outside_right
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = clad_outside_right
execute_on = timestep_end
[]
[]
[ThermalContact]
[thermal_contact]
type = GapHeatTransfer
primary = 5
secondary = 10
variable = temperature
gap_conductivity = 0.15 # k of He per Netzsch
[]
[]
[BCs]
[clad_surface_temperature]
type = FunctionDirichletBC
variable = temperature
boundary = '2'
function = cladding_temperature
[]
[no_x_all]
type = DirichletBC
variable = disp_x
boundary = 12
value = 0.0
[]
[no_y_clad_bottom]
type = DirichletBC
variable = disp_y
boundary = '1'
value = 0.0
[]
[no_y_fuel_bottom]
type = DirichletBC
variable = disp_y
boundary = '1020'
value = 0.0
[]
[Pressure]
[outer_pressure]
boundary = '1 2 3'
factor = 101325
[]
[inner_pressure]
boundary = '4 5 6'
factor = 8.28e6
[]
[]
[]
[PlenumTemperature]
[plenum_temp]
boundary = 5
inner_surfaces = '5'
outer_surfaces = '10'
temperature = temperature
[]
[]
[CoolantChannel]
[convective_clad_surface]
boundary = 2
variable = temperature
inlet_temperature = 473.0
inlet_pressure = 101325
inlet_massflux = 1.0 # kg/m^2-sec # almost stagnant steam
rod_diameter = 0.01118
rod_pitch = 1.26e-02 # default
oxide_thickness = scale_thickness
[]
[]
[Materials]
[fuel_thermal]
type = HeatConductionMaterial
block = pellet
thermal_conductivity = 3.5
specific_heat = 330.0
[]
[fuel_elasticity_tensor]
type = ComputeIsotropicElasticityTensor
block = pellet
youngs_modulus = 2.0e11
poissons_ratio = 0.345
[]
[fuel_elastic_stress]
type = ComputeFiniteStrainElasticStress
block = pellet
[]
[fuel_thermal_expansion]
type = ComputeThermalExpansionEigenstrain
block = pellet
thermal_expansion_coeff = 10.0e-6
temperature = temperature
stress_free_temperature = 300.0
eigenstrain_name = fuel_thermal_strain
[]
[fuel_density]
type = Density
block = pellet
density = 10980.0 #perfectly dense UO2
[]
[clad_thermal]
type = ZryThermal
block = clad
temperature = temperature
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = clad
matpro_youngs_modulus = false
matpro_poissons_ratio = false
[]
[clad_stress]
type = ComputeMultipleInelasticStress
inelastic_models = 'clad_zrycreep'
block = clad
tangent_operator = nonlinear
[]
[clad_zrycreep]
type = ZryCreepLOCAUpdate
block = clad
temperature = temperature
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
temperature_loca_creep_begin = 501
temperature_standard_thermal_creep_end = 500
[]
[thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = clad
temperature = temperature
stress_free_temperature = 300.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[clad_density]
type = Density
block = clad
density = 6550.0
[]
[phase]
type = ZrPhase
block = clad
temperature = temperature
numerical_method = 2
[]
[oxidation]
type = ZryOxidation
boundary = clad_outside_right
temperature = temperature
clad_inner_radius = 4.88e-3 #checked
clad_outer_radius = 5.59e-3 #checked
normal_operating_temperature_model = epri_kwu_ce
high_temperature_model = leistikow
use_coolant_channel = true
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = clad_outside_right
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate_aux
temperature = temperature
fraction_beta_phase = fract_beta_phase
fraction_oxygen_gain = oxywtfgain_total
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
verbose = true
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.0e-04
nl_abs_tol = 1.0e-08
start_time = 0
n_startup_steps = 1
end_time = 1800.0
dtmax = 100
dtmin = 0.0001
[TimeStepper]
type = IterationAdaptiveDT
timestep_limiting_postprocessor = material_timestep
dt = 10.0
time_dt = '100 10'
time_t = '10 400'
[]
[]
[Postprocessors]
[ave_clad_temp]
type = SideAverageValue
boundary = clad_outside_right
variable = temperature
[]
[gas_volume]
type = InternalVolume
boundary = 9
execute_on = 'initial linear'
[]
[max_clad_temp]
type = NodalExtremeValue
block = clad
value_type = max
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = clad
[]
[max_oxygen_fract]
type = ElementExtremeValue
block = clad
value_type = max
variable = oxywtfract_total
[]
[max_betaph_fract]
type = ElementExtremeValue
block = clad
value_type = max
variable = fract_beta_phase
[]
[max_hoop_stress]
type = ElementExtremeValue
block = clad
value_type = max
variable = hoop_stress
[]
[vonmises_stress_clad]
type = ElementAverageValue
block = clad
variable = vonmises_stress
[]
[min_burst_stress]
type = ElementExtremeValue
block = clad
value_type = min
variable = burst_stress
[]
[burst]
type = ElementExtremeValue
block = clad
value_type = max
variable = burst
[]
[oxide_thickness]
type = ElementAverageValue
block = clad
variable = scale_thickness
execute_on = TIMESTEP_END
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = clad
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
[]
[PerformanceMetricOutputs]
[]
[Outputs]
exodus = true
csv = true
color = false
perf_graph = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
show = 'max_clad_temp max_hoop_stress vonmises_stress_clad'
execute_on = 'FINAL'
[]
[]
[UserObjects]
[terminator1]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
[]
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-27/puzry-27.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-27.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 3000. '
y = '1.e+05 1.e+05 5.06e+06' # Linear increase at 0.0248 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 3000. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = EigenSolution
[]
[]
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = MaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = FunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = DirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = DirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1.e+11
poissons_ratio = 0.3
block = 1
[]
[creep_update]
type = ZryCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 1.e-04
temperature = temperature
temperature_standard_thermal_creep_end = 700
temperature_loca_creep_begin = 900.
[]
[creep]
type = ComputeMultipleInelasticStress
block = 1
tangent_operator = elastic
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = Density
block = 1
[]
[phase]
type = ZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
active = 'smp'
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0.
n_startup_steps = 1
end_time = 3000.
dtmax = 1.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-27_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/LOCA_Hardy_cladding_test/analysis/0pt3MPa/100C_sec/100C_sec_Hardy_Tube_Test_0pt3MPa.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
volumetric_locking_correction = false
displacements = 'disp_x disp_y'
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
group_variables = 'disp_x disp_y'
[]
[Mesh]
coord_type = RZ
patch_size = 10
patch_update_strategy = iteration
partitioner = centroid
centroid_partitioner_direction = y
[gen]
type = FuelPinMeshGenerator
include_fuel = false
include_clad = true
pellet_outer_radius = 0.0072527
clad_gap_width = 0.0
clad_top_gap_height = 0.0
clad_bot_gap_height = 0.0
clad_thickness = 0.38e-3
pellet_height = 0.5
pellet_quantity = 1
clad_mesh_density = customize
nx_c = 2
ny_c = 50
elem_type = QUAD8
[]
[]
[Variables]
[temperature]
initial_condition = 600.0
[]
[]
[AuxVariables]
[creep_rate_aux]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[total_hoop_strain]
order = CONSTANT
family = MONOMIAL
[]
[burst_stress]
order = CONSTANT
family = MONOMIAL
[]
[burst]
order = CONSTANT
family = MONOMIAL
[]
[]
[Functions]
[pressure_function]
type = PiecewiseLinear
x = '0 40'
y = '1 1'
[]
[temp_function]
type = PiecewiseLinear
y = '600 1600'
[]
[temperature_profile]
type = PiecewiseBilinear
y = '0 40'
x = '0 0.25224 0.50448'
z = '0.995 1.01 0.995 0.995 1.01 0.995'
axis = 1
[]
[inner_temperature]
type = CompositeFunction
functions = 'temp_function temperature_profile'
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[clad]
block = clad
add_variables = true
strain = FINITE
decomposition_method = EigenSolution
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz elastic_strain_xx elastic_strain_yy elastic_strain_zz
creep_strain_xx creep_strain_yy creep_strain_zz hoop_stress'
extra_vector_tags = 'ref'
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
extra_vector_tags = 'ref'
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
extra_vector_tags = 'ref'
[]
[]
[AuxKernels]
[creep_rate_aux]
type = MaterialRealAux
variable = creep_rate_aux
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[creep_rate]
type = MaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[total_hoop_strain]
type = RankTwoAux
rank_two_tensor = total_strain
variable = total_hoop_strain
index_i = 2
index_j = 2
execute_on = timestep_end
block = clad
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = clad_outside_right
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = clad_outside_right
execute_on = timestep_end
[]
[]
[BCs]
[Pressure]
[outer_surface]
boundary = 'clad_outside_bottom clad_outside_right clad_outside_top'
factor = 0.0
function = pressure_function
[]
[inner_surface]
boundary = 'clad_inside_right clad_inside_bottom clad_inside_top'
function = pressure_function
[]
[]
[u_bottom_fix]
type = DirichletBC
variable = disp_y
boundary = 1001
value = 0.0
[]
[x_fix]
type = DirichletBC
variable = disp_x
boundary = centerline
value = 0.0
[]
[temp_bc]
type = FunctionDirichletBC
function = inner_temperature
variable = temperature
boundary = 'clad_inside_bottom clad_inside_right clad_inside_top'
[]
[]
[Materials]
[clad_thermal]
type = ZryThermal
block = clad
zry_thermal_properties_model = MATPRO
temperature = temperature
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = clad
matpro_youngs_modulus = true
matpro_poissons_ratio = true
temperature = temperature
[]
[clad_stress]
type = ComputeMultipleInelasticStress
inelastic_models = 'clad_zrycreep'
block = clad
tangent_operator = nonlinear
[]
[clad_zrycreep]
type = ZryCreepLOCAUpdate
block = clad
temperature = temperature
model_irradiation_creep = false
model_primary_creep = true
model_thermal_creep = true
temperature_loca_creep_begin = 840 # values from the report
temperature_standard_thermal_creep_end = 975
[]
[thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = clad
temperature = temperature
stress_free_temperature = 600.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[clad_density]
type = Density
block = clad
density = 6550.0
[]
[phase]
type = ZrPhase
block = clad
temperature = temperature
numerical_method = 2
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = clad_outside_right
failure_criterion = combined_overstress_and_overstrain
hoop_stress = hoop_stress
hoop_creep_strain = creep_strain_zz
effective_strain_rate_creep = creep_rate_aux
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.0e-5
nl_abs_tol = 1.0e-8
start_time = 0
n_startup_steps = 1
end_time = 40
dtmax = 1
dtmin = 0.0000001
[TimeStepper]
type = IterationAdaptiveDT
timestep_limiting_postprocessor = material_timestep
dt = 1.0
[]
[]
[Postprocessors]
[ave_clad_temp]
type = SideAverageValue
boundary = clad_outside_right
variable = temperature
[]
[gas_volume]
type = InternalVolume
boundary = all_clad_interior
execute_on = 'initial linear'
[]
[max_clad_temp]
type = NodalExtremeValue
block = clad
value_type = max
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = clad
[]
[max_hoop_stress]
type = ElementExtremeValue
block = clad
value_type = max
variable = hoop_stress
[]
[vonmises_stress_clad]
type = ElementAverageValue
block = clad
variable = vonmises_stress
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = total_hoop_strain
[]
[max_disp_x]
type = NodalExtremeValue
block = clad
value_type = max
variable = disp_x
[]
[min_burst_stress]
type = ElementExtremeValue
block = clad
value_type = min
variable = burst_stress
[]
[burst]
type = ElementExtremeValue
block = clad
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = clad
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
[]
[PerformanceMetricOutputs]
[]
[Outputs]
color = false
perf_graph = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[csv]
type = CSV
[]
[chkfile]
type = CSV
show = 'max_disp_x max_hoop_stress vonmises_stress_clad'
execute_on = 'FINAL'
[]
[]
[UserObjects]
[terminator1]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '5'
include_fuel = false
[]
[]
(assessment/LWR/validation/RIA_CABRI_REP_Na4/analysis/REP_Na_4/REP_Na_4.i)
# REP Na 4 Rodlet Base Irradiation
[GlobalParams]
density = 10476.35 # assumed TD = 10970
order = SECOND
family = LAGRANGE
energy_per_fission = 3.2e-11 # J/fission
displacements = 'disp_x disp_y'
[]
[Problem]
type = AugmentedLagrangianContactProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
maximum_lagrangian_update_iterations = 200
acceptable_iterations = 30
acceptable_multiplier = 5
[]
[Mesh]
coord_type = RZ
patch_size = 40
#patch_update_strategy = auto
#partitioner = centroid
#centroid_partitioner_direction = y
[mesh]
type = FileMeshGenerator
file = REP_Na4.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temp]
initial_condition = 293.15
[]
[]
[UserObjects]
[pin_geometry]
type = FuelPinGeometry
clad_inner_wall = 5
clad_outer_wall = 2
clad_top = 3
clad_bottom = 1
pellet_exteriors = 8
[]
[]
[AuxVariables]
[fast_neutron_flux]
block = 'clad'
[]
[fast_neutron_fluence]
block = 'clad'
[]
[grain_radius]
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
initial_condition = 5.0e-6 # Assume Grain size 10 microns
[]
[gap_cond]
order = CONSTANT
family = MONOMIAL
[]
[fuel_cond]
order = CONSTANT
family = MONOMIAL
[]
[swelling_strain]
order = CONSTANT
family = MONOMIAL
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
[]
[hoop_creep_strain]
order = CONSTANT
family = MONOMIAL
[]
[hoop_plastic_strain]
order = CONSTANT
family = MONOMIAL
[]
[axial_creep_strain]
order = CONSTANT
family = MONOMIAL
[]
[hoop_elastic_strain]
order = CONSTANT
family = MONOMIAL
[]
[axial_plastic_strain]
order = CONSTANT
family = MONOMIAL
[]
[total_hoop_strain]
order = CONSTANT
family = MONOMIAL
[]
[total_axial_strain]
order = CONSTANT
family = MONOMIAL
[]
[axial_elastic_strain]
order = CONSTANT
family = MONOMIAL
[]
[clad_coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[coolant_temp]
order = CONSTANT
family = MONOMIAL
[]
[clad_coolant_flux]
order = CONSTANT
family = MONOMIAL
[]
[coolant_channel_hmode]
order = CONSTANT
family = MONOMIAL
[]
[coolant_channel_htype]
order = CONSTANT
family = MONOMIAL
[]
[critical_heat_flux]
order = CONSTANT
family = MONOMIAL
[]
[oxide_thickness]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[plastic_strain_mag]
order = CONSTANT
family = MONOMIAL
block = 'clad'
[]
[SED]
order = CONSTANT
family = MONOMIAL
block = 'clad'
[]
[oxywtfract_total]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfgain_total]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[]
[Functions]
[power_profile]
type = PiecewiseLinear # reads and interpolates an input file containing rod average linear power vs time
data_file = REPNa4_power_history_Full.csv
format = columns
scale_factor = 1
[]
[axial_peaking_factors] # reads and interpolates an input file containing the axial power profile vs time
type = PiecewiseBilinear
data_file = REPNa4_axial_peaking_Full.csv
scale_factor = 1
axis = 1
[]
[pressure_ramp] # inlet coolant pressure evolution
type = PiecewiseLinear
scale_factor = 1.0
xy_data = '0 101325
8640 15499970
124675200 15499970
124718400 101325
125193600 101325
125193610 101325
125193650 500008
125193700 500008
125193900 500008
125194000 101325
125194100 101325'
[]
[temp_ramp] # inlet coolant temp evolution
type = PiecewiseLinear
scale_factor = 0.985
xy_data = '0 293.15
8640 591
20476800 591
21859200 600
47692800 600
51840000 593
72144000 593
73440000 586
96940800 586
99360000 583
124675200 583
124761600 293.15
125193600 293.15
125193650 553.15
125193900.0 553.150
125194000.0 293.150
125194100.0 293.150'
[]
[burnup_GWd]
type = ParsedFunction
expression = bu*950
symbol_names = 'bu'
symbol_values = 'average_burnup'
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[pellets]
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
strain = FINITE
eigenstrain_names = 'fuel_thermal_strain fuel_relocation_strain
fuel_volumetric_strain'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz axial_stress'
extra_vector_tags = 'ref'
[]
[clad]
block = 'clad'
strain = FINITE
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
eigenstrain_names = 'clad_thermal_eigenstrain clad_irradiation_strain'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz plastic_strain_xx plastic_strain_yy plastic_strain_zz
creep_strain_xx creep_strain_yy creep_strain_zz elastic_strain_xx
elastic_strain_yy elastic_strain_zz hoop_stress axial_stress'
extra_vector_tags = 'ref'
[]
[]
[Kernels]
[heat] # gradient term in heat conduction equation
type = HeatConduction
variable = temp
extra_vector_tags = 'ref'
[]
[heat_ie] # time term in heat conduction equation
type = HeatConductionTimeDerivative
variable = temp
extra_vector_tags = 'ref'
[]
[heat_source_fuel] # source term in heat conduction equation
type = NeutronHeatSource
variable = temp
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
burnup_function = burnup
extra_vector_tags = 'ref'
[]
[]
[Burnup]
[burnup]
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
rod_ave_lin_pow = power_profile
axial_power_profile = axial_peaking_factors
num_radial = 80
num_axial = 11
a_upper = 0.5678974
a_lower = 0.0045
fuel_inner_radius = 0
fuel_outer_radius = 0.0040959
fuel_volume_ratio = 1
isotopes = 'U235 U238 Pu239 Pu240 Pu241 Pu242'
isotope_fractions = '0.0449 0.9551 0 0 0 0'
RPF = RPF
order = CONSTANT
family = MONOMIAL
[]
[]
[AuxKernels]
[fast_neutron_flux]
type = FastNeutronFluxAux
variable = fast_neutron_flux
axial_power_profile = axial_peaking_factors
rod_ave_lin_pow = power_profile
factor = 3e13 #n/m2-s
block = 'clad'
execute_on = timestep_begin
[]
[fast_neutron_fluence]
type = FastNeutronFluenceAux
variable = fast_neutron_fluence
fast_neutron_flux = fast_neutron_flux
block = 'clad'
execute_on = timestep_begin
[]
[grain_radius]
type = GrainRadiusAux
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
variable = grain_radius
temperature = temp
execute_on = linear
[]
[gap_conductance]
type = MaterialRealAux
property = gap_conductance
variable = gap_cond
boundary = 10
[]
[fuel_conductance]
type = MaterialRealAux
property = thermal_conductivity
variable = fuel_cond
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
[]
[swelling_strain]
type = MaterialRealAux
property = volumetric_swelling_strain
variable = swelling_strain
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
[]
[hoop_creep_strain]
type = RankTwoAux
rank_two_tensor = creep_strain
variable = hoop_creep_strain
index_i = 2
index_j = 2
execute_on = timestep_end
block = 'clad'
[]
[axial_creep_strain]
type = RankTwoAux
rank_two_tensor = creep_strain
variable = axial_creep_strain
index_i = 1
index_j = 1
execute_on = timestep_end
block = 'clad'
[]
[hoop_plastic_strain]
type = RankTwoAux
rank_two_tensor = plastic_strain
variable = hoop_plastic_strain
index_i = 2
index_j = 2
execute_on = timestep_end
block = 'clad'
[]
[axial_plastic_strain]
type = RankTwoAux
rank_two_tensor = plastic_strain
variable = axial_plastic_strain
index_i = 1
index_j = 1
execute_on = timestep_end
block = 'clad'
[]
[total_hoop_strain]
type = RankTwoAux
rank_two_tensor = total_strain
variable = total_hoop_strain
index_i = 2
index_j = 2
execute_on = timestep_end
block = 'clad'
[]
[total_axial_strain]
type = RankTwoAux
rank_two_tensor = total_strain
variable = total_axial_strain
index_i = 1
index_j = 1
execute_on = timestep_end
block = 'clad'
[]
[hoop_elastic_strain]
type = RankTwoAux
rank_two_tensor = elastic_strain
variable = hoop_elastic_strain
index_i = 2
index_j = 2
execute_on = timestep_end
block = 'clad'
[]
[axial_elastic_strain]
type = RankTwoAux
rank_two_tensor = elastic_strain
variable = axial_elastic_strain
index_i = 1
index_j = 1
execute_on = timestep_end
block = 'clad'
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
block = clad
execute_on = timestep_end
[]
[plastic_strain_mag]
type = MaterialRealAux
property = effective_plastic_strain
variable = plastic_strain_mag
block = clad
execute_on = timestep_end
[]
[clad_coolant_htc]
type = MaterialRealAux
property = coolant_channel_htc
variable = clad_coolant_htc
boundary = 2
[]
[coolant_temp]
type = MaterialRealAux
property = coolant_temperature
variable = coolant_temp
boundary = 2
[]
[clad_coolant_flux]
type = MaterialRealAux
property = output_heat_flux
variable = clad_coolant_flux
boundary = 2
[]
[coolant_channel_hmode]
type = MaterialRealAux
property = coolant_channel_hmode
variable = coolant_channel_hmode
boundary = 2
[]
[coolant_channel_htype]
type = MaterialRealAux
property = coolant_channel_htype
variable = coolant_channel_htype
boundary = 2
[]
[critical_heat_flux]
type = MaterialRealAux
property = critical_heat_flux
variable = critical_heat_flux
boundary = 2
[]
[oxide]
type = MaterialRealAux
property = oxide_scale_thickness
variable = oxide_thickness
boundary = 2
[]
[SED]
type = MaterialRealAux
variable = SED
property = strain_energy_density
execute_on = timestep_end
[]
[ofract_total]
type = MaterialRealAux
property = current_oxygen_weight_frac_total
variable = oxywtfract_total
execute_on = timestep_end
boundary = 2
[]
[ofgain_total]
type = MaterialRealAux
property = oxygen_weight_frac_gained_total
variable = oxywtfgain_total
execute_on = timestep_end
boundary = 2
[]
[fract_bphase]
type = MaterialRealAux
property = fract_beta_phase
variable = fract_beta_phase
block = 'clad'
[]
[]
# Define mechanical contact between the fuel (sideset=10) and the clad (sideset=5)
[Contact]
[pellet_clad_mechanical]
primary = 5
secondary = 210 #10
penalty = 1e9
model = coulomb
formulation = augmented_lagrange
friction_coefficient = 10.0
tangential_tolerance = 1e-3
normal_smoothing_distance = 0.1
al_penetration_tolerance = 1e-6
al_incremental_slip_tolerance = 1e-6
al_frictional_force_tolerance = 5e-2
[]
[pellet_clad_mechanical_2]
primary = 5
secondary = 410
penalty = 1e9
model = coulomb
formulation = augmented_lagrange
friction_coefficient = 0.0
tangential_tolerance = 1e-3
normal_smoothing_distance = 0.1
al_penetration_tolerance = 1e-6
al_incremental_slip_tolerance = 1e-6
al_frictional_force_tolerance = 5e-2
[]
[]
# Define thermal contact between the fuel (sideset=10) and the clad (sideset=5)
[ThermalContact]
[thermal_contact]
type = GasGapHeatTransfer
variable = temp
primary = 5
secondary = 10
initial_moles = initial_moles # coupling to a postprocessor which supplies the initial plenum/gap gas mass
gas_released = fission_gas_released # coupling to a postprocessor which supplies the fission gas addition
jump_distance_model = LANNING
plenum_pressure = plenum_pressure
contact_pressure = contact_pressure
roughness_primary = 2.0e-6
roughness_secondary = 0.5e-6
roughness_coef = 3.2
normal_smoothing_distance = 0.1
quadrature = true
emissivity_primary = 0.800 #Emissivity for fuel
emissivity_secondary = 0.325 #Emissivity for clad
refab_time = 125107200
refab_gas_types = He
refab_fractions = 1
contact_coef = 20 #10 default
[]
[]
[BCs]
# pin pellets and clad along axis of symmetry (y)
[no_x_all]
type = DirichletBC
variable = disp_x
boundary = 12
value = 0.0
[]
# pin clad bottom in the axial direction (y)
[no_y_clad_bottom]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[]
# pin fuel bottom in the axial direction (y)
[no_y_fuel_bottom]
type = DirichletBC
variable = disp_y
boundary = 20
value = 0.0
[]
[Pressure]
# apply coolant pressure on clad outer walls
[coolantPressure]
boundary = '1 2 3'
factor = 1
function = pressure_ramp # use the pressure_ramp function defined above
[]
[]
[PlenumPressure]
# apply plenum pressure on clad inner walls and pellet surfaces
[plenumPressure]
boundary = 9
initial_temperature = 293.15
initial_pressure = 2.60e6
startup_time = 0
R = 8.3143
output_initial_moles = initial_moles # coupling to post processor to get initial fill gas mass
temperature = ave_temp_interior #plenumTemp
volume = gas_volume # coupling to post processor to get gas volume
material_input = fission_gas_released # coupling to post processor to get fission gas added
output = plenum_pressure # coupling to post processor to output plenum/gap pressure
displacements = 'disp_x disp_y'
# extra_vector_tags = 'ref'
refab_time = 125107200
refab_pressure = 0.301e6
refab_temperature = 293.15
refab_volume = 2.0e-6
[]
[]
[]
[CoolantChannel]
[convective_clad_surface] # apply convective boundary to clad outer surface
boundary = '1 2 3'
variable = temp
inlet_temperature = temp_ramp # K
inlet_pressure = pressure_ramp # Pa
inlet_massflux = 3244.044104 # kg/m^2-sec
rod_diameter = 0.00951 # m
rod_pitch = 1.26e-2 # m
coolant_material = 'water'
compute_enthalpy = true
oxide_thickness = oxide_thickness # coupled oxide_thickness
number_axial_zone = 50
[]
#
# [convective_clad_surface_sodium] # apply convective boundary to clad outer surface
# boundary = '1 2 3'
# variable = temp
# inlet_temperature = temp_ramp # K
# inlet_pressure = pressure_ramp # Pa
# inlet_massflux = 3533 # kg/m^2-sec Based on flow rate provided and flow area and estimated density of 885.1 kg/m^3
# flow_area = 8.74855e-5 #m^2
# heated_diameter = 1.172526e-2 #m
# hydraulic_diameter = 4.7e-3 #m
# heated_perimeter = 2.984513e-2 #m
# coolant_material = 'sodium'
# compute_enthalpy = true
# heat_transfer_mode = 0
# oxide_thickness = oxide_thickness # coupled oxide_thickness
# number_axial_zone = 50
# rod_diameter = 0.0095 # m
# htc_correlation_type = 2
# []
[]
[Materials]
[fuel_density]
type = Density
#density = 10476.35
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
[]
[fuel_thermal]
type = UO2Thermal
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
temperature = temp
burnup_function = burnup
thermal_conductivity_model = NFIR
initial_porosity = 0.045
[]
[fuel_elasticity_tensor]
type = UO2ElasticityTensor
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
matpro_poissons_ratio = 1
matpro_youngs_modulus = 1
temperature = temp
[]
[fuel_elastic_stress]
type = ComputeFiniteStrainElasticStress
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
[]
[fuel_thermal_expansion]
type = UO2ThermalExpansionMATPROEigenstrain
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
temperature = temp
stress_free_temperature = 293.15
eigenstrain_name = fuel_thermal_strain
[]
[fuel_relocation]
type = UO2RelocationEigenstrain
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
burnup_function = burnup
rod_ave_lin_pow = power_profile
axial_power_profile = axial_peaking_factors
relocation_activation1 = 5000
burnup_relocation_stop = 0.0208
relocation_model = ESCORE_modified
eigenstrain_name = fuel_relocation_strain
fuel_pin_geometry = 'pin_geometry'
[]
[fuel_volumetric_swelling]
type = UO2VolumetricSwellingEigenstrain
gas_swelling_model_type = SIFGRS
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
temperature = temp
burnup_function = burnup
initial_fuel_density = 10476.35
total_densification = 0.00675
initial_porosity = 0.045
eigenstrain_name = fuel_volumetric_strain
[]
[fission_gas_release]
type = UO2Sifgrs
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
temperature = temp
fission_rate = fission_rate
initial_porosity = 0.045
grain_radius = grain_radius
gbs_model = true
transient_option = NO_TRANSIENT
[]
[clad_density]
type = Density
block = 'clad'
density = 6550
[]
[clad_thermal]
type = ZryThermal
block = 'clad'
temperature = temp
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
temperature = temp
matpro_poissons_ratio = true
matpro_youngs_modulus = true
cold_work_factor = 0.5
fast_neutron_fluence = fast_neutron_fluence
block = 'clad'
[]
[clad_stress]
type = ComputeMultipleInelasticStress
tangent_operator = elastic
inelastic_models = 'clad_zrycreep clad_zryplasticity'
block = 'clad'
[]
[clad_zrycreep]
type = ZryCreepLimbackHoppeUpdate
block = 'clad'
temperature = temp
fast_neutron_flux = fast_neutron_flux
fast_neutron_fluence = fast_neutron_fluence
creeprate_scale_factor = 1
model_irradiation_creep = 1
model_primary_creep = 1
model_thermal_creep = 1
max_inelastic_increment = 0.0002
[]
[clad_zryplasticity]
type = ZryPlasticityUpdate
block = 'clad'
temperature = temp
fast_neutron_flux = fast_neutron_flux
fast_neutron_fluence = fast_neutron_fluence
cold_work_factor = 0.5
plasticity_model_type = MATPRO
zircaloy_alloy_type = 4
max_inelastic_increment = 0.0002
[]
[clad_thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = 'clad'
temperature = temp
stress_free_temperature = 293.15
eigenstrain_name = clad_thermal_eigenstrain
[]
[clad_irradiation_swelling]
type = ZryIrradiationGrowthEigenstrain
block = 'clad'
fast_neutron_fluence = fast_neutron_fluence
zircaloy_material_type = stress_relief_annealed
eigenstrain_name = clad_irradiation_strain
[]
[clad_oxidation]
type = ZryOxidation
boundary = 2
clad_inner_radius = 0.00417789
clad_outer_radius = 0.00475615
use_coolant_channel = true
temperature = temp
fast_neutron_flux = fast_neutron_flux
oxygen_weight_fraction_initial = 0.0012
[]
[phase]
type = ZrPhase
block = 'clad'
numerical_method = 2
temperature = temp
[]
[StrainEnergyDensity]
type = StrainEnergyDensity
block = 'clad'
incremental = 1
[]
[]
[Dampers]
[BoundingValueNodalDamper]
type = BoundingValueNodalDamper
max_value = 3200 # The maximum permissible iterative value for the variable.
min_value = 200 # The minimum permissible iterative value for the variable.
variable = temp # The name of the variable that this damper operates on
[]
[contact_slip]
type = ContactSlipDamper
primary = 5
secondary = 10
min_damping_factor = 0.05
[]
[]
[Preconditioning]
[SMP]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'contact'
contact_line_search_allowed_lambda_cuts = 0
contact_line_search_ltol = 0.5
verbose = true
l_max_its = 100
l_tol = 1e-3
nl_max_its = 40
nl_rel_tol = 1e-4
nl_abs_tol = 1e-10
start_time = 0
end_time = 125193600 #125194100 is the end time for the RIA
dtmax = 1e6
dtmin = 1e-7
[TimeStepper]
type = IterationAdaptiveDT
dt = 1.0e3
optimal_iterations = 100
iteration_window = 2
linear_iteration_ratio = 100
timestep_limiting_function = power_profile
max_function_change = 1e6
force_step_every_function_point = true
timestep_limiting_postprocessor = material_timestep
time_t = '125193610 125193620 125193630 125193640 125193650 125193660 125193670 125193680'
time_dt = '10 10 10 10 10 10 10 10'
growth_factor = 5
[]
[Quadrature]
order = FIFTH #SEVENTH
side_order = SEVENTH #Comment out if order = SEVENTH
[]
[]
[Postprocessors]
[ave_temp_interior] # average temperature of the cladding interior and all pellet exteriors
type = SideAverageValue
boundary = 9 #For RIA the node number is ##***8479***##
variable = temp
execute_on = 'initial linear'
[]
[clad_inner_vol] # volume inside of cladding
type = InternalVolume
boundary = 7
execute_on = 'initial linear'
[]
[avg_clad_temp] # average temperature of cladding interior
type = SideAverageValue
boundary = 7
variable = temp
execute_on = 'initial timestep_end'
[]
[max_fuel_temp]
type = NodalExtremeValue
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
value_type = max
variable = temp
execute_on = 'initial timestep_end'
[]
[min_fuel_temp]
type = NodalExtremeValue
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
value_type = min
variable = temp
execute_on = 'initial timestep_end'
[]
[max_clad_temp]
type = NodalExtremeValue
block = 'clad'
value_type = max
variable = temp
execute_on = 'initial timestep_end'
[]
[min_clad_temp]
type = NodalExtremeValue
block = 'clad'
value_type = min
variable = temp
execute_on = 'initial timestep_end'
[]
[fis_gas_grain]
type = ElementIntegralFisGasGrainSifgrs
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
outputs = exodus
[]
[fis_gas_boundary]
type = ElementIntegralFisGasBoundarySifgrs
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
outputs = exodus
[]
[gas_volume] # gas volume
type = InternalVolume
boundary = 9
execute_on = 'initial linear'
[]
[flux_from_clad] # area integrated heat flux from the cladding
type = SideDiffusiveFluxIntegral
variable = temp
boundary = 5
diffusivity = thermal_conductivity
[]
[flux_from_fuel] # area integrated heat flux from the fuel
type = SideDiffusiveFluxIntegral
variable = temp
boundary = 10
diffusivity = thermal_conductivity
[]
[1_rod_input_power]
type = FunctionValuePostprocessor
function = power_profile
[]
[3_burnup_GWd]
type = FunctionValuePostprocessor
function = burnup_GWd
[]
[vonmises_stress_fuel]
type = ElementAverageValue
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
variable = vonmises_stress
[]
[vonmises_stress_clad]
type = ElementAverageValue
block = 'clad'
variable = vonmises_stress
[]
[z_average_RPF]
type = ElementAverageValue
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
variable = RPF
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = 'clad'
[]
## Nodal values
[FCT] #fuel centerline temperature
type = NodalVariableValue
variable = temp
nodeid = 3866 #(0, 0.303375, 0)
[]
[FST] #fuel surface temperature
type = NodalVariableValue
variable = temp
nodeid = 3823 #(0.0040959, 0.303375, 0)
[]
[CIST] #clad inner surface temperature
type = NodalVariableValue
variable = temp
nodeid = 9557 #(0.0041779, 0.305106, 0)
[]
[COST] #clad outer surface temperature
type = NodalVariableValue
variable = temp
nodeid = 9547 #(0.00475615, 0.305106, 0)
[]
[gap]
type = NodalVariableValue
variable = penetration
nodeid = 3823 #(0.0040959, 0.303375, 0)
use_displaced_mesh = true
[]
#######################################
[qpoint_penetration] #FOCE
type = ElementalVariableValue
variable = qpoint_penetration
elementid = 1200
use_displaced_mesh = 1
[]
[penetration] #FOCN
type = NodalVariableValue
variable = penetration
nodeid = 3823
use_displaced_mesh = 1
[]
[contact_pressure] #FOCN
type = NodalVariableValue
variable = contact_pressure
nodeid = 3823
use_displaced_mesh = 1
[]
[gap_cond] #FOCE
type = ElementalVariableValue
variable = gap_cond
elementid = 1200
use_displaced_mesh = 1
[]
[creep_hoop_strain] #COCE
type = ElementalVariableValue
variable = hoop_creep_strain
elementid = 2981
use_displaced_mesh = 1
[]
[elastic_hoop_strain] #COCE
type = ElementalVariableValue
variable = hoop_elastic_strain
elementid = 2981
use_displaced_mesh = 1
[]
[plastic_hoop_strain] #COCE
type = ElementalVariableValue
variable = hoop_plastic_strain
elementid = 2981
use_displaced_mesh = 1
[]
[total_hoop_strain] #COCE
type = ElementalVariableValue
variable = total_hoop_strain
elementid = 2981
use_displaced_mesh = 1
[]
[clad_hoop_stress] #COCE
type = ElementalVariableValue
variable = hoop_stress
elementid = 2981
use_displaced_mesh = 1
[]
[clad_axial_elongation] #COTN
type = NodalVariableValue
variable = disp_y
nodeid = 10755
use_displaced_mesh = 1
[]
[clad_oxide_thickness] #COCE
type = ElementalVariableValue
variable = oxide_thickness
elementid = 2981
use_displaced_mesh = 1
[]
[clad_coolant_htc] #COCE
type = ElementalVariableValue
variable = clad_coolant_htc
elementid = 2981
use_displaced_mesh = 1
[]
[coolant_temp] #COCE
type = ElementalVariableValue
variable = coolant_temp
elementid = 2981
use_displaced_mesh = 1
[]
[clad_coolant_flux] #COCE
type = ElementalVariableValue
variable = clad_coolant_flux
elementid = 2981
use_displaced_mesh = 1
[]
[coolant_channel_hmode] #COCE
type = ElementalVariableValue
variable = coolant_channel_hmode
elementid = 2981
use_displaced_mesh = 1
[]
[coolant_channel_htype] #COCE
type = ElementalVariableValue
variable = coolant_channel_htype
elementid = 2981
use_displaced_mesh = 1
[]
[critical_heat_flux] #COCE
type = ElementalVariableValue
variable = critical_heat_flux
elementid = 2981
use_displaced_mesh = 1
[]
[fuel_centerline_temp] #FICN
type = NodalVariableValue
variable = temp
nodeid = 3866
[]
[fuel_surface_temp] #FOCN
type = NodalVariableValue
variable = temp
nodeid = 3823
[]
[clad_inner_surface_temp] #CICN
type = NodalVariableValue
variable = temp
nodeid = 9557
[]
[clad_outer_surface_temp] #COCN
type = NodalVariableValue
variable = temp
nodeid = 9547
[]
[fuel_axial_elongation] #FOTN
type = NodalVariableValue
variable = disp_y
nodeid = 7739
[]
[clad_radial_elongation] #COCN
type = NodalVariableValue
variable = disp_x
nodeid = 9547
[]
[fuel_radial_elongation] #FOCN
type = NodalVariableValue
variable = disp_x
nodeid = 3823
[]
[SED_PPN_O] #COCE
type = ElementalVariableValue
variable = SED
elementid = 2981
use_displaced_mesh = 1
[]
[SED_PPN_I] #CICE
type = ElementalVariableValue
variable = SED
elementid = 2984
use_displaced_mesh = 1
[]
[zz_OFract_PPN_O] #COCE
type = ElementalVariableValue
variable = oxywtfract_total
elementid = 2981
use_displaced_mesh = 1
[]
[zz_OGain_PPN_O] #COCE
type = ElementalVariableValue
variable = oxywtfgain_total
elementid = 2981
use_displaced_mesh = 1
[]
#######################################
[max_clad_SED]
type = ElementExtremeValue
block = 'clad'
variable = SED
value_type = max
[]
#Post processor to calculate radial average enthalpy. This postprocessor isnt available yet in BISON
[z_RAE]
type = RadialAverageEnthalpy
vector_postprocessor = rad_temp
radial_direction = x
axial_direction = y
axial_position = 0.3
temperature_name = temp
[]
[peak_RAE]
type = TimeExtremeValue
postprocessor = z_RAE
[]
[]
[VectorPostprocessors]
[clad_dia]
type = NodalValueSampler
variable = disp_x
boundary = 2
sort_by = y
outputs = 'outfile_clad_diameter'
[]
[pellet_dia]
type = NodalValueSampler
variable = disp_x
boundary = 10
sort_by = y
outputs = 'outfile_pellet_diameter'
[]
#Location of peak power node at appoximately 0.3 m in mesh
[rad_temp]
type = NodalValueSampler
block = 3
sort_by = y
variable = temp
execute_on = timestep_end
outputs = 'outfile_radial_temp'
[]
[]
[StandardLWRFuelRodOutputs]
fuel_pellet_blocks = 'pellet_type_1 pellet_type_2 pellet_type_3'
temperature = temp
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
time_step_interval = 1
csv = true
#exodus = true
color = false
[outfile_clad_diameter]
type = CSV
sync_times = '125194100'
sync_only = true
[]
[outfile_pellet_diameter]
type = CSV
sync_times = '125194100'
sync_only = true
[]
[outfile_radial_temp]
type = CSV
end_time = -100000
[]
[console]
type = Console
output_linear = true
max_rows = 10
[]
[chkfile]
type = CSV
show = 'ave_temp_interior fission_gas_released FCT average_burnup peak_RAE'
execute_on = 'FINAL'
[]
[exodus]
type = Exodus
time_step_interval = 4
end_time = 125193700
[]
[exodus_RIA]
type = Exodus
time_step_interval = 3
start_time = 125193695
[]
[checkpoint_RIA]
type = Checkpoint
file_base = recover_files_RIA
sync_times = '124761600 125107200 125193600 125193650 125193700 125193700.06 125193700.07 125193700.08 125193700.09 125193700.10 125193700.20 125193700.30 125193700.40 125193700.50 125193700.60 125193700.70 125193700.80 125193700.90 125193701.00 125193701.25 125193701.50 125193701.75 125193702.00 125193702.25 125193702.50 125193702.75 125193703.00 125193704.00 125193705.00'
[]
[]
[Debug]
show_var_residual = 'disp_x disp_y temp'
show_var_residual_norms = true
show_material_props = true
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-19/puzry-19_aniso.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-19.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 2000. '
y = '1.e+05 1.e+05 2.53e+06' # Linear increase at 0.0243 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 2000. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
# Circumferential steady-state creep test and analysis of Zircaloy-4 fuel cladding
# Nuclear Engineering and Design, 53, 2312-2322 (2021)
[F]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.738 0.738 0.57'
[]
[G]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.174 0.174 0.45'
[]
[H]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.588 0.588 0.48'
[]
[L]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[M]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[N]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = TaylorExpansion
use_automatic_differentiation = true
[]
[]
[]
[]
[Kernels]
[heat]
type = ADHeatConduction
variable = temperature
[]
[heat_ie]
type = ADHeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = ADMaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = ADMaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = ADMaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = ADMaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = ADMaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = ADFunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = ADDirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = ADDirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ADZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1.e+11
poissons_ratio = 0.3
block = 1
[]
[hill_constants]
type = ADHillConstants
hill_constants = "0.738 0.174 0.588 1.0 1.0 1.0"
function_names = "F G H L M N"
temperature = temperature
[]
[creep_update]
type = ADZryAnisoCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 1.5e-05
temperature = temperature
temperature_standard_thermal_creep_end = 700
temperature_loca_creep_begin = 900.
fract_beta_phase_name = 'fract_beta_phase'
max_integration_error = 1000000.0
absolute_tolerance = 1e-13
relative_tolerance = 1e-11
[]
[creep]
type = ADComputeMultipleInelasticStress
block = 1
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ADZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = ADDensity
block = 1
[]
[phase]
type = ADZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ADZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = NEWTON
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0.
n_startup_steps = 1
end_time = 2500.
dtmax = 1.
dtmin = 1.0e-9
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-19_aniso_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-30/puzry-30_aniso.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-30.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 1300. '
y = '1.e+05 1.e+05 7.99e+06' # Linear increase at 0.2630 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 1300. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
# Circumferential steady-state creep test and analysis of Zircaloy-4 fuel cladding
# Nuclear Engineering and Design, 53, 2312-2322 (2021)
[F]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.738 0.738 0.57'
[]
[G]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.174 0.174 0.45'
[]
[H]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.588 0.588 0.48'
[]
[L]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[M]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[N]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = TaylorExpansion
use_automatic_differentiation = true
[]
[]
[]
[]
[Kernels]
[heat]
type = ADHeatConduction
variable = temperature
[]
[heat_ie]
type = ADHeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = ADMaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = ADMaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = ADMaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = ADMaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = ADMaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = ADFunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = ADDirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = ADDirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ADZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1.e+11
poissons_ratio = 0.3
block = 1
[]
[hill_constants]
type = ADHillConstants
hill_constants = "0.738 0.174 0.588 1.0 1.0 1.0"
function_names = "F G H L M N"
temperature = temperature
[]
[creep_update]
type = ADZryAnisoCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 1.5e-05
temperature = temperature
temperature_standard_thermal_creep_end = 700
temperature_loca_creep_begin = 900.
fract_beta_phase_name = 'fract_beta_phase'
max_integration_error = 1000000.0
absolute_tolerance = 1e-13
relative_tolerance = 1e-11
[]
[creep]
type = ADComputeMultipleInelasticStress
block = 1
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ADZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = ADDensity
block = 1
[]
[phase]
type = ADZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ADZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = NEWTON
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-07
start_time = 0.
n_startup_steps = 1
end_time = 2500.
dtmax = 1.
dtmin = 1.0e-9
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-30_aniso_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(test/tests/xfem/level_set_xfem_oxidation/ls_xfem_zry_oxidation_default.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
[mesh]
type = GeneratedMeshGenerator
dim = 2
nx = 8
ny = 4
xmin = 0.0
xmax = 575.0e-6 # A typical zircaloy cladding thickness
ymin = 0.0
ymax = 1200.0e-6 # A representative section of cladding length
elem_type = QUAD4
[]
[]
[XFEM]
qrule = moment_fitting
output_cut_plane = true
[]
[UserObjects]
[level_set_cut_uo]
type = LevelSetCutUserObject
level_set_var = phi
heal_always = true
[]
[]
[Constraints]
[xfem_u_constraint]
type = XFEMSingleVariableConstraint
variable = temp
geometric_cut_userobject = 'level_set_cut_uo'
use_penalty = true
alpha = 1e5
[]
[xfem_phi_constraint]
type = XFEMSingleVariableConstraint
variable = phi
geometric_cut_userobject = 'level_set_cut_uo'
use_penalty = true
alpha = 1e5
[]
[]
[Variables]
[temp]
[]
[phi]
[]
[]
[AuxVariables]
[fast_neutron_flux]
order = FIRST
family = LAGRANGE
initial_condition = 1.0e17
[]
[scale_thickness]
order = CONSTANT
family = MONOMIAL
[]
[ls_vel]
family = MONOMIAL_VEC
[]
[]
[Kernels]
[heat_diff]
type = HeatConduction
variable = temp
[]
[heat_time]
type = HeatConductionTimeDerivative
variable = temp
[]
[phi_advection]
type = LevelSetAdvection
variable = phi
velocity = ls_vel
[]
[phi_time]
type = TimeDerivative
variable = phi
[]
[]
[AuxKernels]
[fnflux]
type = FastNeutronFluxAux
variable = fast_neutron_flux
function = fnflux_func
execute_on = timestep_begin
[]
[scl_thickness]
type = MaterialRealAux
variable = scale_thickness
property = oxide_scale_thickness
[]
[coupled_phi_vel]
type = VectorMaterialRealVectorValueAux
variable = ls_vel
property = oxide_growth_rate_components
execute_on = timestep_end
[]
[]
[Functions]
[left_temp_func]
type = PiecewiseBilinear
axis = 1
x = '0.0 300.0e-6 600.0e-6 900.0e-6 1200.0e-6'
y = '0.0 100.0'
z = '620.0 619.8 619.5 619.05 618.35
620.0 619.8 619.5 619.05 618.35'
[]
[temp_ic_func]
type = PiecewiseLinear
x = '0.0 300.0e-6 600.0e-6 900.0e-6 1200.0e-6'
y = '620.0 619.8 619.5 619.05 618.35'
[]
[phi_ic_func]
type = ParsedFunction
expression = '(470e-6 - x)'
[]
[fnflux_func]
type = PiecewiseLinear
x = '0. 200.'
y = '1.e+17 1.e+17'
[]
[]
[Materials]
[density_Zry]
type = Density
density = 6550.0
base_name = Zry
[]
[thermal_Zry]
type = ZryThermal
temperature = temp
base_name = Zry
[]
[density_ZrO2]
type = Density
density = 5680.0
base_name = ZrO2
[]
[thermal_ZrO2]
type = ZrO2Thermal
temperature = temp
base_name = ZrO2
[]
[combined_density]
type = XFEMCutSwitchingMaterialReal
geometric_cut_userobject = level_set_cut_uo
cut_subdomain_ids = '0 1'
base_names = 'ZrO2 Zry'
prop_name = density
[]
[combined_thermal_conductivity]
type = XFEMCutSwitchingMaterialReal
geometric_cut_userobject = level_set_cut_uo
cut_subdomain_ids = '0 1'
base_names = 'ZrO2 Zry'
prop_name = thermal_conductivity
[]
[combined_thermal_conductivity_dT]
type = XFEMCutSwitchingMaterialReal
geometric_cut_userobject = level_set_cut_uo
cut_subdomain_ids = '0 1'
base_names = 'ZrO2 Zry'
prop_name = thermal_conductivity_dT
[]
[combined_specific_heat]
type = XFEMCutSwitchingMaterialReal
geometric_cut_userobject = level_set_cut_uo
cut_subdomain_ids = '0 1'
base_names = 'ZrO2 Zry'
prop_name = specific_heat
[]
[oxidation_growth_rate_components]
type = ZryOxidation
temperature = temp
ls_function = phi
fast_neutron_flux = fast_neutron_flux
normal_operating_temperature_model = epri_kwu_ce
high_temperature_model = leistikow
clad_inner_radius = 0
clad_outer_radius = 575.0e-6
[]
[]
[BCs]
[left_temp]
type = FunctionDirichletBC
variable = temp
function = left_temp_func
boundary = 'left'
[]
[right_temp]
type = DirichletBC
variable = temp
value = 580.0
boundary = 'right'
[]
[]
[ICs]
[temp_ic]
type = FunctionIC
variable = temp
function = temp_ic_func
[]
[phi_ic]
type = FunctionIC
variable = phi
function = phi_ic_func
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -bc_factor_mat_solver_package'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
l_tol = 1.0e-05
nl_abs_tol = 1.0e-06
nl_rel_tol = 1.0e-06
start_time = 0.0
end_time = 50.0
dt = 25.0
max_xfem_update = 2
[]
[Postprocessors]
[dt]
type = TimestepSize
[]
[temp]
type = NodalVariableValue
variable = temp
nodeid = 0
execute_on = 'initial timestep_end'
[]
[phi]
type = NodalVariableValue
variable = phi
nodeid = 1
execute_on = 'initial timestep_end'
[]
[]
[Outputs]
time_step_interval = 1
exodus = true
[console]
type = Console
output_linear = true
[]
[]
(assessment/LWR/validation/LOCA_ORNL_cladding_burst_tests/analysis/Zr4_1/ornl_zr4_1_ad_hill_aniso.i)
# Simulation ORNL burst tests Zr4_1
[GlobalParams]
density = 6550.
order = SECOND
family = LAGRANGE
displacements = 'disp_x disp_y'
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = zr4_ornl_burst_test_mesh.e
[]
[]
[Variables]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func] # only 10 inches of the rod are within the heated zone (cf. Terrani email)
type = PiecewiseBilinear
data_file = temperature_ornl_zr4_1.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
data_file = pressure_inner_ornl_zr4_1.csv
scale_factor = 1.e+06
format = columns
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 373.9'
y = '0.1 0.1 ' # atmospheric pressure
scale_factor = 1.e+06
[]
# Circumferential steady-state creep test and analysis of Zircaloy-4 fuel cladding
# Nuclear Engineering and Design, 53, 2312-2322 (2021)
[F]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.738 0.738 0.57'
[]
[G]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.174 0.174 0.45'
[]
[H]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.588 0.588 0.48'
[]
[L]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[M]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[N]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[clad]
block = cladding
add_variables = true
strain = FINITE
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
# decomposition_method = EigenSolution
eigenstrain_names = 'clad_thermal_eigenstrain'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz hoop_stress'
use_automatic_differentiation = true
decomposition_method = TaylorExpansion
[]
[]
[AuxVariables]
[creep_rate_aux]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[scale_thickness]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfract_total]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfgain_total]
order = CONSTANT
family = MONOMIAL
[]
[burst_stress]
order = CONSTANT
family = MONOMIAL
[]
[burst]
order = CONSTANT
family = MONOMIAL
[]
[]
[Kernels]
[heat]
type = ADHeatConduction
variable = temperature
[]
[heat_ie]
type = ADHeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate_aux]
type = ADMaterialRealAux
variable = creep_rate_aux
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = ADMaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[scl_thickness]
type = ADMaterialRealAux
variable = scale_thickness
property = oxide_scale_thickness
boundary = 2
[]
[ofract_total]
type = ADMaterialRealAux
variable = oxywtfract_total
property = current_oxygen_weight_frac_total
boundary = 2
[]
[ofgain_total]
type = ADMaterialRealAux
boundary = 2
variable = oxywtfgain_total
property = oxygen_weight_frac_gained_total
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = 2
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = 2
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = ADFunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 4'
preset = false
[]
[no_y_top]
type = ADDirichletBC
variable = disp_y
boundary = 3
value = 0.
preset = false
[]
[Pressure]
[outer_pressure] # apply steam pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[mid_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 98 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[converter]
type = MaterialADConverter
reg_props_in = 'fract_beta_phase'
ad_props_out = 'ad_fract_beta_phase'
[]
[thermal]
type = ADZryThermal
block = cladding
temperature = temperature
[]
[clad_elasticity_tensor]
type = ADZryElasticityTensor
block = cladding
matpro_youngs_modulus = false
matpro_poissons_ratio = false
[]
[clad_stress]
type = ADComputeMultipleInelasticStress
inelastic_models = 'clad_zrycreep'
block = cladding
[]
[hill_constants]
type = ADHillConstants
hill_constants = "0.738 0.174 0.588 1.0 1.0 1.0"
function_names = "F G H L M N"
temperature = temperature
[]
[clad_zrycreep]
type = ADZryAnisoCreepLOCAUpdate
block = cladding
temperature = temperature
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
temperature_loca_creep_begin = 301
temperature_standard_thermal_creep_end = 300
fract_beta_phase_name = 'ad_fract_beta_phase'
[]
[thermal_expansion]
type = ADZryThermalExpansionMATPROEigenstrain
block = cladding
temperature = temperature
stress_free_temperature = 300.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[density]
type = ADDensity
block = cladding
[]
[phase]
type = ZrPhase
block = cladding
temperature = temperature
numerical_method = 2
[]
[oxidation]
type = ADZryOxidation
boundary = 2
temperature = temperature
clad_inner_radius = 0.004175
clad_outer_radius = 0.004750
normal_operating_temperature_model = epri_kwu_ce
high_temperature_model = leistikow
#use_coolant_channel = true
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = 2
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate_aux
temperature = temperature
fraction_beta_phase = fract_beta_phase
fraction_oxygen_gain = oxywtfgain_total
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = PJFNK
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0
n_startup_steps = 1
end_time = 373.9
dtmax = 1.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[Postprocessors]
[pressure_inner]
type = FunctionValuePostprocessor
function = inner_pressure_func
execute_on = 'initial timestep_end'
[]
[pressure_outer]
type = FunctionValuePostprocessor
function = outer_pressure_func
execute_on = 'initial timestep_end'
[]
[ave_clad_temp]
type = SideAverageValue
boundary = 2
variable = temperature
execute_on = 'initial timestep_end'
[]
[max_clad_temp]
type = NodalExtremeValue
block = cladding
value_type = max
variable = temperature
execute_on = 'initial timestep_end'
[]
[min_clad_temp]
type = NodalExtremeValue
block = cladding
value_type = min
variable = temperature
execute_on = 'initial timestep_end'
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = cladding
[]
[max_oxygen_fract]
type = ElementExtremeValue
block = cladding
value_type = max
variable = oxywtfract_total
execute_on = 'initial timestep_end'
[]
[max_betaph_fract]
type = ElementExtremeValue
block = cladding
value_type = max
variable = fract_beta_phase
execute_on = 'initial timestep_end'
[]
[max_creep_rate]
type = ElementExtremeValue
block = cladding
value_type = max
variable = creep_rate_aux
execute_on = 'initial timestep_end'
[]
[max_creep_strain_mag]
type = ElementExtremeValue
block = cladding
value_type = max
variable = creep_strain_mag
execute_on = 'initial timestep_end'
[]
[max_hoop_strain]
type = ElementExtremeValue
block = cladding
value_type = max
variable = strain_zz
execute_on = 'initial timestep_end'
[]
[max_hoop_stress]
type = ElementExtremeValue
block = cladding
value_type = max
variable = hoop_stress
[]
[vonmises_stress_clad]
type = ElementAverageValue
block = cladding
variable = vonmises_stress
execute_on = 'initial timestep_end'
[]
[min_burst_stress]
type = ElementExtremeValue
block = cladding
value_type = min
variable = burst_stress
execute_on = 'initial timestep_end'
[]
[burst]
type = ElementExtremeValue
block = cladding
value_type = max
variable = burst
execute_on = 'initial timestep_end'
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = cladding
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[mid_disp_r_clad]
type = NodalVariableValue
variable = disp_x
nodeid = 22
[]
[stress_xx_midplane] # stress in the mid Element
type = ElementalVariableValue
variable = stress_xx
elementid = 19
[]
[stress_yy_midplane] # stress in the mid Element
type = ElementalVariableValue
variable = stress_yy
elementid = 19
[]
[stress_zz_midplane] # stress in the mid Element
type = ElementalVariableValue
variable = stress_zz
elementid = 19
[]
[strain_zz_midplane] # strain in the mid Element
type = ElementalVariableValue
variable = strain_zz
elementid = 19
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
plenum_boundary_name = 4
cladding_blocks = cladding
[]
[PerformanceMetricOutputs]
[]
[Outputs]
exodus = true
perf_graph = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 20
[]
[chkfile]
type = CSV
file_base = ornl_zr4_1_ad_hill_aniso_chkfile
show = 'pressure_inner max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(test/tests/phase_transition_zircaloy/test_zrphase.i)
# This test demonstrates the usage of the model for the high-temperature alpha <--> beta phase transition of Zircaloy. This is implemented in the class ZrPhase.
# Only Zircaloy-4 is considered at the moment.
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
temperature = temp
[]
[Mesh]
[mesh]
type = FileMeshGenerator
file = cube_111.e
[]
[]
[Functions]
[Temp_func]
type = PiecewiseLinear
x = '0. 10800. 50000. 50075. 50150. 50260.'
y = '300. 650. 650. 1400. 1400. 300. '
[]
[]
[Variables]
[temp]
order = FIRST
family = LAGRANGE
initial_condition = 300.
[]
[]
[AuxVariables]
[ratep_zrphase] # rate parameter
order = CONSTANT
family = MONOMIAL
[]
[fract_bp_equilibrium] # equilibrium beta/alpha phase fraction
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # actual beta/alpha phase fraction
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[solid]
block = 1
strain = FINITE
incremental = true
add_variables = true
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temp
[]
[]
[AuxKernels]
[rateparam]
type = MaterialRealAux
variable = ratep_zrphase
property = ratep_zrphase
block = 1
[]
[fractbp_eq]
type = MaterialRealAux
variable = fract_bp_equilibrium
property = fract_bp_equilibrium
block = 1
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
block = 1
[]
[]
[BCs]
[bottom_T]
type = FunctionDirichletBC
variable = temp
function = Temp_func
boundary = 1
[]
[x_disp]
type = DirichletBC
variable = disp_x
value = 0
boundary = 1
[]
[y_disp]
type = DirichletBC
variable = disp_y
value = 0
boundary = 2
[]
[z_disp]
type = DirichletBC
variable = disp_z
value = 0
boundary = 3
[]
[]
[Materials]
[felasticity_tensor]
type = ComputeIsotropicElasticityTensor
block = 1
youngs_modulus = 7.5e+10
poissons_ratio = 0.3
[]
[elastic_stress]
type = ComputeFiniteStrainElasticStress
block = 1
[]
[thermal]
type = ZryThermal
block = 1
temperature = temp
[]
[phase]
type = ZrPhase
block = 1
numerical_method = 2
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
l_tol = 1.e-08
nl_abs_tol = 1.e-08
nl_rel_tol = 1.e-08
start_time = 0.
num_steps = 5000
end_time = 50260
[TimeStepper]
type = IterationAdaptiveDT
dt = 1.e+02
optimal_iterations = 6
iteration_window = 2
linear_iteration_ratio = 100
time_t = '0. 10800. 50000. 50090. 50180. 50290.'
time_dt = '1.e+03 2.e+03 1. 1. 1. 1. '
growth_factor = 1.
[]
[]
[Postprocessors]
[_dt]
type = TimestepSize
[]
[temp]
type = NodalVariableValue
variable = temp
nodeid = 0
execute_on = 'initial timestep_end'
[]
[rate_parameter]
type = ElementalVariableValue
elementid = 0
variable = ratep_zrphase
[]
[beta_equilibrium]
type = ElementalVariableValue
elementid = 0
variable = fract_bp_equilibrium
[]
[beta_phase_fraction]
type = ElementalVariableValue
elementid = 0
variable = fract_beta_phase
[]
[]
[Outputs]
file_base = out_test_zrphase
[exodus]
type = Exodus
[]
[]
(assessment/LWR/validation/LOCA_REBEKA_cladding_burst_tests/analysis/rebeka_2d_10MPa/rebeka_singlerod_2d_10MPa_aniso.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
order = SECOND
family = LAGRANGE
displacements = 'disp_x disp_y'
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = rebeka_singlerod.e
[]
[]
[Variables]
[temperature]
initial_condition = 573.0
[]
[]
[Functions]
[temperature_func]
type = PiecewiseLinear
x = '0. 700. '
y = '573. 1273.' # From 300 to 1000 C at 1 K/s
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 700. '
y = '1.e+07 1.e+07' # 100 bar
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 700. '
y = '1.e+05 1.e+05' # atmospheric pressure
[]
# Circumferential steady-state creep test and analysis of Zircaloy-4 fuel cladding
# Nuclear Engineering and Design, 53, 2312-2322 (2021)
[F]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.738 0.738 0.57'
[]
[G]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.174 0.174 0.45'
[]
[H]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.588 0.588 0.48'
[]
[L]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[M]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[N]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[clad]
block = cladding
add_variables = true
strain = FINITE
decomposition_method = TaylorExpansion
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz hoop_stress'
use_automatic_differentiation = true
[]
[]
[AuxVariables]
[creep_rate_aux]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[scale_thickness]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfract_total]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfgain_total]
order = CONSTANT
family = MONOMIAL
[]
[burst_stress]
order = CONSTANT
family = MONOMIAL
[]
[burst]
order = CONSTANT
family = MONOMIAL
[]
[]
[Kernels]
[heat]
type = ADHeatConduction
variable = temperature
[]
[heat_ie]
type = ADHeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate_aux]
type = ADMaterialRealAux
variable = creep_rate_aux
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = ADMaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = ADMaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[scl_thickness]
type = ADMaterialRealAux
variable = scale_thickness
property = oxide_scale_thickness
boundary = 2
[]
[ofract_total]
type = ADMaterialRealAux
variable = oxywtfract_total
property = current_oxygen_weight_frac_total
boundary = 2
[]
[ofgain_total]
type = ADMaterialRealAux
boundary = 2
variable = oxywtfgain_total
property = oxygen_weight_frac_gained_total
[]
[sigmaburst]
type = ADMaterialRealAux
variable = burst_stress
property = burst_stress
boundary = 2
[]
[hasburst]
type = ADMaterialRealAux
variable = burst
property = failed
boundary = 2
execute_on = timestep_end
[]
[]
[BCs]
[inner_temperature]
type = REBEKADirichletBC
variable = temperature
function_tempm = temperature_func
minimum_temperature = 573.
translation = 0.1625
boundary = 4
[]
[no_y_midsection]
type = ADDirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply steam pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 101 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[CoolantChannel]
[convective_clad_surface]
boundary = 2
variable = temperature
inlet_temperature = 473.
inlet_pressure = 1.e+05
inlet_massflux = 1.0 # kg/m^2-sec # almost stagnant steam
rod_diameter = 10.75e-03
rod_pitch = 1.26e-02 # default
oxide_thickness = scale_thickness
use_ad = true
[]
[]
[Materials]
[thermal]
type = ADZryThermal
block = cladding
temperature = temperature
[]
[clad_elasticity_tensor]
type = ADZryElasticityTensor
block = cladding
matpro_youngs_modulus = false
matpro_poissons_ratio = false
[]
[clad_stress]
type = ADComputeMultipleInelasticStress
inelastic_models = 'clad_zrycreep'
block = cladding
[]
[hill_constants]
type = ADHillConstants
hill_constants = "0.738 0.174 0.588 1.0 1.0 1.0"
function_names = "F G H L M N"
temperature = temperature
[]
[clad_zrycreep]
type = ADZryAnisoCreepLOCAUpdate
block = cladding
temperature = temperature
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
temperature_loca_creep_begin = 501
temperature_standard_thermal_creep_end = 500
fract_beta_phase_name = 'fract_beta_phase'
[]
[thermal_expansion]
type = ADZryThermalExpansionMATPROEigenstrain
block = cladding
temperature = temperature
stress_free_temperature = 573.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[density]
type = ADDensity
block = cladding
[]
[phase]
type = ADZrPhase
block = cladding
temperature = temperature
numerical_method = 2
[]
[oxidation]
type = ADZryOxidation
boundary = 2
temperature = temperature
clad_inner_radius = 0.00465
clad_outer_radius = 0.005375
normal_operating_temperature_model = epri_kwu_ce
high_temperature_model = leistikow
use_coolant_channel = true
[]
[clad_failure_criterion]
type = ADZryCladdingFailure
boundary = 2
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate_aux
temperature = temperature
fraction_beta_phase = fract_beta_phase
fraction_oxygen_gain = oxywtfgain_total
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = NEWTON
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-06
nl_abs_tol = 1.e-08
start_time = 0
n_startup_steps = 1
end_time = 700.
dtmax = 1.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[Postprocessors]
[ave_clad_exterior_temp]
type = SideAverageValue
boundary = 2
variable = temperature
[]
[max_clad_temp]
type = NodalExtremeValue
block = cladding
value_type = max
variable = temperature
[]
[min_clad_temp]
type = NodalExtremeValue
block = cladding
value_type = min
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = cladding
[]
[max_oxygen_fract]
type = ElementExtremeValue
block = cladding
value_type = max
variable = oxywtfract_total
[]
[max_betaph_fract]
type = ElementExtremeValue
block = cladding
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
block = cladding
value_type = max
variable = creep_rate_aux
[]
[max_creep_strain_mag]
type = ElementExtremeValue
block = cladding
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
block = cladding
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
block = cladding
value_type = max
variable = hoop_stress
[]
[vonmises_stress_clad]
type = ElementAverageValue
block = cladding
variable = vonmises_stress
[]
[min_burst_stress]
type = ElementExtremeValue
block = cladding
value_type = min
variable = burst_stress
[]
[burst]
type = ElementExtremeValue
block = cladding
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = cladding
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[top_disp_r_clad] # this is mid height
type = NodalVariableValue
variable = disp_x
nodeid = 0 #coords (0.005375, 0.1625)
[]
[top_disp_r_clad_slice] # this is mid height matched to the 1.5d
type = NodalVariableValue
variable = disp_x
nodeid = 3 #coords (0.005375, 0.1625)
[]
[top_disp_z_clad]
type = NodalVariableValue
variable = disp_y
nodeid = 0 #coords (0.005375, 0.1625)
[]
[stress_xx] # stess in the top Element
type = ElementalVariableValue
variable = stress_xx
elementid = 0
[]
[stress_yy] # stess in the top Element
type = ElementalVariableValue
variable = stress_yy
elementid = 0
[]
[stress_zz] # stess in the top Element
type = ElementalVariableValue
variable = stress_zz
elementid = 0
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = cladding
plenum_boundary_name = 4
external_clad_boundary_name = 2
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = rebeka_2d_10MPa_aniso_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-06/puzry-06.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-06.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 3000. '
y = '1.e+05 1.e+05 1.06e+06' # Linear increase at 0.0759 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 3000. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = EigenSolution
[]
[]
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = MaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = FunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = DirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = DirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1.e+11
poissons_ratio = 0.3
block = 1
[]
[creep_update]
type = ZryCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 1.e-04
temperature = temperature
temperature_standard_thermal_creep_end = 700
temperature_loca_creep_begin = 900.
[]
[creep]
type = ComputeMultipleInelasticStress
block = 1
tangent_operator = elastic
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = Density
block = 1
[]
[phase]
type = ZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
active = 'smp'
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0.
n_startup_steps = 1
end_time = 3000.
dtmax = 1.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-06_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-29/puzry-29_aniso.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-29.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 2000. '
y = '1.e+05 1.e+05 7.3e+06' # Linear increase at 0.0720 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 2000. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
# Circumferential steady-state creep test and analysis of Zircaloy-4 fuel cladding
# Nuclear Engineering and Design, 53, 2312-2322 (2021)
[F]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.738 0.738 0.57'
[]
[G]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.174 0.174 0.45'
[]
[H]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.588 0.588 0.48'
[]
[L]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[M]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[N]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = TaylorExpansion
use_automatic_differentiation = true
[]
[]
[]
[]
[Kernels]
[heat]
type = ADHeatConduction
variable = temperature
[]
[heat_ie]
type = ADHeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = ADMaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = ADMaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = ADMaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = ADMaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = ADMaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = ADFunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = ADDirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = ADDirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ADZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1.e+11
poissons_ratio = 0.3
block = 1
[]
[hill_constants]
type = ADHillConstants
hill_constants = "0.738 0.174 0.588 1.0 1.0 1.0"
function_names = "F G H L M N"
temperature = temperature
[]
[creep_update]
type = ADZryAnisoCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 1.5e-05
temperature = temperature
temperature_standard_thermal_creep_end = 700
temperature_loca_creep_begin = 900.
fract_beta_phase_name = 'fract_beta_phase'
max_integration_error = 1000000.0
absolute_tolerance = 1e-13
relative_tolerance = 1e-11
[]
[creep]
type = ADComputeMultipleInelasticStress
block = 1
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ADZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = ADDensity
block = 1
[]
[phase]
type = ADZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ADZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = NEWTON
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-07
start_time = 0.
n_startup_steps = 1
end_time = 2500.
dtmax = 1.
dtmin = 1.0e-9
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-29_aniso_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-03/puzry-03_aniso.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-03.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 2000. '
y = '1.e+05 1.e+05 7.3e+05' # Linear increase at 0.063 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 2000. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
# Circumferential steady-state creep test and analysis of Zircaloy-4 fuel cladding
# Nuclear Engineering and Design, 53, 2312-2322 (2021)
[F]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.738 0.738 0.57'
[]
[G]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.174 0.174 0.45'
[]
[H]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.588 0.588 0.48'
[]
[L]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[M]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[N]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = TaylorExpansion
use_automatic_differentiation = true
[]
[]
[]
[]
[Kernels]
[heat]
type = ADHeatConduction
variable = temperature
[]
[heat_ie]
type = ADHeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = ADMaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = ADMaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = ADMaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = ADMaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = ADMaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = ADFunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = ADDirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = ADDirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ADZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1.e+11
poissons_ratio = 0.3
block = 1
[]
[hill_constants]
type = ADHillConstants
hill_constants = "0.738 0.174 0.588 1.0 1.0 1.0"
function_names = "F G H L M N"
temperature = temperature
[]
[creep_update]
type = ADZryAnisoCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 1.5e-05
temperature = temperature
temperature_standard_thermal_creep_end = 700
temperature_loca_creep_begin = 900.
fract_beta_phase_name = 'fract_beta_phase'
max_integration_error = 1000000.0
absolute_tolerance = 1e-07
relative_tolerance = 1e-07
[]
[creep]
type = ADComputeMultipleInelasticStress
block = 1
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ADZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = ADDensity
block = 1
[]
[phase]
type = ADZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ADZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = NEWTON
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0.
n_startup_steps = 1
end_time = 2500.
dtmax = 1.
dtmin = 1.0e-9
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-03_aniso_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/RIA_CABRI_REP_Na/analysis/REP_Na_10/REP_Na_10_RIA.i)
# REP Na 10 Rodlet RIA
[GlobalParams]
density = 10448.925 # assumed TD = 10970
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
energy_per_fission = 3.2e-11
temperature = temp
volumetric_locking_correction = false
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
acceptable_iterations = 30
acceptable_multiplier = 10
restart_file_base = 'recover_files_cp/LATEST'
[]
[Mesh]
coord_type = RZ
[smeared_pellet_mesh]
type = FuelPinMeshGenerator
clad_mesh_density = customize
pellet_mesh_density = customize
nx_p = 11
ny_p = 156
ny_cu = 3
ny_c = 160
ny_cl = 3
nx_c = 4
clad_thickness = 0.0005753
pellet_outer_radius = 0.004096055
pellet_quantity = 39
pellet_height = 0.01425001
clad_top_gap_height = 0.032027026
clad_bot_gap_height = 0.003
clad_gap_width = 82.0e-6
bottom_clad_height = 0.0015
top_clad_height = 0.0015
elem_type = QUAD8
[]
patch_size = 40
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temp]
[]
[]
[AuxVariables]
[fast_neutron_flux]
block = 1
[]
[fast_neutron_fluence]
block = 1
[]
[grain_radius]
block = 3
[]
[gap_cond]
order = CONSTANT
family = MONOMIAL
[]
[fuel_cond]
order = CONSTANT
family = MONOMIAL
[]
[swelling_strain]
order = CONSTANT
family = MONOMIAL
block = 3
[]
[total_hoop_strain]
order = CONSTANT
family = MONOMIAL
[]
[total_axial_strain]
order = CONSTANT
family = MONOMIAL
[]
[clad_coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[coolant_temp]
order = CONSTANT
family = MONOMIAL
[]
[clad_coolant_flux]
order = CONSTANT
family = MONOMIAL
[]
[coolant_channel_hmode]
order = CONSTANT
family = MONOMIAL
[]
[coolant_channel_htype]
order = CONSTANT
family = MONOMIAL
[]
[critical_heat_flux]
order = CONSTANT
family = MONOMIAL
[]
[oxide_thickness]
order = CONSTANT
family = MONOMIAL
[]
[SED]
order = CONSTANT
family = MONOMIAL
block = 1
[]
[oxywtfract_total]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfgain_total]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[]
[Functions]
[power_profile]
type = PiecewiseLinear
data_file = REPNa10_power_history_Full.csv
format = columns
[]
[axial_peaking_factors]
type = PiecewiseBilinear
data_file = REPNa10_axial_peaking_Full.csv
axis = 1
[]
[pressure_ramp]
type = PiecewiseLinear
xy_data = '0 101325
8640 15499970
125280000 15499970
125366400 101325
125798400 101325
125798410 101325
125798450 500008
125798500 500008
125798700 500008
125798800 101325
125798900 101325'
[]
[temp_ramp]
type = PiecewiseLinear
xy_data = '0 293.15
8640 588.706
125280000 588.706
125366400 293.15
125798400 293.15
125798410 293.15
125798450 553.15
125798500 553.15
125798700 553.15
125798800 293.15
125798900 293.15'
[]
[Fuel_CTE_function] #Fuel CTE as a function of temp from MATPRO data
type = PiecewiseLinear
xy_data = ' 0 1.000E-05
300 1.000E-05
350 1.000E-05
400 1.000E-05
450 1.000E-05
500 1.001E-05
550 1.002E-05
600 1.003E-05
650 1.005E-05
700 1.008E-05
750 1.011E-05
800 1.015E-05
850 1.020E-05
900 1.026E-05
950 1.032E-05
1000 1.039E-05
1050 1.046E-05
1100 1.053E-05
1150 1.061E-05
1200 1.069E-05
1250 1.077E-05
1300 1.085E-05
1350 1.094E-05
1400 1.102E-05
1450 1.111E-05
1500 1.119E-05
1550 1.127E-05
1600 1.135E-05
1650 1.143E-05
1700 1.151E-05
1750 1.158E-05
1800 1.166E-05
1850 1.173E-05
1900 1.180E-05
1950 1.187E-05
2000 1.193E-05
2050 1.199E-05
2100 1.205E-05
2150 1.211E-05
2200 1.217E-05
2250 1.222E-05
2300 1.227E-05
2350 1.232E-05
2400 1.237E-05
2450 1.242E-05
2500 1.246E-05
2550 1.250E-05
2600 1.254E-05
2650 1.258E-05
2700 1.262E-05
2750 1.265E-05
2800 1.268E-05
2850 1.271E-05
2900 1.274E-05
2950 1.277E-05
3000 1.280E-05
3050 1.282E-05
3100 1.285E-05'
[]
[burnup_GWd]
type = ParsedFunction
expression = bu*950
symbol_names = 'bu'
symbol_values = 'average_burnup_EAV'
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[fuel]
block = 3
strain = FINITE
incremental = true
eigenstrain_names = 'fuel_relocation_eigenstrain fuel_thermal_eigenstrain
fuel_volumetric_swelling_eigenstrain'
extra_vector_tags = 'ref'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz'
[]
[clad]
block = 1
strain = FINITE
incremental = true
eigenstrain_names = 'clad_irradiation_growth_eigenstrain
clad_thermal_eigenstrain'
extra_vector_tags = 'ref'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz plastic_strain_xx plastic_strain_yy plastic_strain_zz
creep_strain_xx creep_strain_yy creep_strain_zz elastic_strain_xx
elastic_strain_yy elastic_strain_zz hoop_stress'
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temp
extra_vector_tags = 'ref'
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temp
extra_vector_tags = 'ref'
[]
[heat_source_fuel]
type = NeutronHeatSource
variable = temp
block = 3
burnup_function = burnup
extra_vector_tags = 'ref'
[]
[]
[Burnup]
[burnup]
block = 3
rod_ave_lin_pow = power_profile
axial_power_profile = axial_peaking_factors
num_radial = 80
num_axial = 40
a_upper = 0.5602504
a_lower = 0.0045
fuel_inner_radius = 0
fuel_outer_radius = 0.004096055
fuel_volume_ratio = 1
isotopes = 'U235 U238 Pu239 Pu240 Pu241 Pu242'
isotope_fractions = '0.045 0.955 0 0 0 0'
RPF = RPF
order = CONSTANT
family = MONOMIAL
[]
[]
[AuxKernels]
[fast_neutron_flux]
type = FastNeutronFluxAux
variable = fast_neutron_flux
block = 1
axial_power_profile = axial_peaking_factors
rod_ave_lin_pow = power_profile
factor = 3e13 #n/m2-s
execute_on = timestep_begin
[]
[fast_neutron_fluence]
type = FastNeutronFluenceAux
variable = fast_neutron_fluence
fast_neutron_flux = fast_neutron_flux
block = 1
execute_on = timestep_begin
[]
[grain_radius]
type = GrainRadiusAux
block = 3
variable = grain_radius
temperature = temp
execute_on = linear
[]
[gap_conductance]
type = MaterialRealAux
property = gap_conductance
variable = gap_cond
boundary = 10
[]
[fuel_conductance]
type = MaterialRealAux
property = thermal_conductivity
variable = fuel_cond
block = 3
[]
[swelling_strain]
type = MaterialRealAux
property = volumetric_swelling_strain
variable = swelling_strain
block = 3
[]
[total_hoop_strain]
type = RankTwoScalarAux
rank_two_tensor = total_strain
variable = total_hoop_strain
scalar_type = HoopStress
execute_on = timestep_end
block = 1
[]
[total_axial_strain]
type = RankTwoScalarAux
rank_two_tensor = total_strain
variable = total_axial_strain
scalar_type = AxialStress
execute_on = timestep_end
block = 1
[]
[clad_coolant_htc]
type = MaterialRealAux
property = coolant_channel_htc
variable = clad_coolant_htc
boundary = 2
[]
[coolant_temp]
type = MaterialRealAux
property = coolant_temperature
variable = coolant_temp
boundary = 2
[]
[clad_coolant_flux]
type = MaterialRealAux
property = output_heat_flux
variable = clad_coolant_flux
boundary = 2
[]
[coolant_channel_hmode]
type = MaterialRealAux
property = coolant_channel_hmode
variable = coolant_channel_hmode
boundary = 2
[]
[coolant_channel_htype]
type = MaterialRealAux
property = coolant_channel_htype
variable = coolant_channel_htype
boundary = 2
[]
[critical_heat_flux]
type = MaterialRealAux
property = critical_heat_flux
variable = critical_heat_flux
boundary = 2
[]
[oxide]
type = MaterialRealAux
property = oxide_scale_thickness
variable = oxide_thickness
boundary = 2
[]
[SED]
type = MaterialRealAux
variable = SED
property = strain_energy_density
execute_on = timestep_end
[]
[ofract_total]
type = MaterialRealAux
variable = oxywtfract_total
property = current_oxygen_weight_frac_total
execute_on = timestep_end
boundary = 2
[]
[ofgain_total]
type = MaterialRealAux
variable = oxywtfgain_total
property = oxygen_weight_frac_gained_total
execute_on = timestep_end
boundary = 2
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
block = 1
[]
[]
[Contact]
[pellet_clad_mechanical]
primary = 5
secondary = 10
penalty = 1e10
formulation = penalty
normalize_penalty = false
model = frictionless
normal_smoothing_distance = 0.1
[]
[]
[ThermalContact]
[thermal_contact]
type = GasGapHeatTransfer
variable = temp
primary = 5
secondary = 10
initial_moles = initial_moles
gas_released = fission_gas_released
jump_distance_model = LANNING
plenum_pressure = plenum_pressure
contact_pressure = contact_pressure
roughness_primary = 0.1e-6 #2.0e-6
roughness_secondary = 0.1e-6 #0.5e-6
roughness_coef = 3.2
normal_smoothing_distance = 0.1
quadrature = true
emissivity_primary = 0.797698
emissivity_secondary = 0.325
refab_time = 125712000
refab_gas_types = He
refab_fractions = 1
[]
[]
[BCs]
[no_x_all]
type = DirichletBC
variable = disp_x
boundary = 12
value = 0.0
[]
[no_y_clad_bottom]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[]
[no_y_fuel_bottom]
type = DirichletBC
variable = disp_y
boundary = 20
value = 0.0
[]
[Pressure]
[coolantPressure]
boundary = '1 2 3'
function = pressure_ramp
[]
[]
[PlenumPressure]
[plenumPressure]
boundary = 9
initial_temperature = 293.15
initial_pressure = 2.60e6
startup_time = 0
R = 8.3143
output_initial_moles = initial_moles
temperature = plenum_temperature
volume = plenum_volume
material_input = fission_gas_released
output = plenum_pressure
refab_time = 125712000
refab_pressure = 0.301e6
refab_temperature = 293.15
refab_volume = 2.0e-6
[]
[]
[]
[CoolantChannel]
[convective_clad_surface]
boundary = '1 2 3'
variable = temp
inlet_temperature = temp_ramp # K
inlet_pressure = pressure_ramp # Pa
inlet_massflux = 3533 # kg/m^2-sec Based on flow rate provided and flow area and estimated density of 885.1 kg/m^3
flow_area = 8.74855e-5 #m^2
heated_diameter = 1.172526e-2 #m
hydraulic_diameter = 4.7e-3 #m
heated_perimeter = 2.984513e-2 #m
coolant_material = 'sodium'
compute_enthalpy = true
heat_transfer_mode = 0
#oxide_thickness = oxide_thickness # coupled oxide_thickness
number_axial_zone = 50
rod_pitch = 1.26e-2 # m
rod_diameter = 0.0095 # m
[]
[]
[Materials]
[swelling]
type = UO2VolumetricSwellingEigenstrain
block = 3
burnup_function = burnup
initial_fuel_density = 10448.925
include_solid_swelling = true
include_densification = true
total_densification = 0.00675
initial_porosity = 0.0475
eigenstrain_name = 'fuel_volumetric_swelling_eigenstrain'
[]
[fuel_thermal]
type = UO2Thermal
block = 3
thermal_conductivity_model = NFIR
temperature = temp
burnup_function = burnup
initial_porosity = 0.0475
[]
[fuel_elastic_stress]
type = ComputeFiniteStrainElasticStress
block = 3
[]
[fuel_elasticity_tensor]
type = UO2ElasticityTensor
block = 3
[]
[fuel_thermal_expansion]
type = ComputeInstantaneousThermalExpansionFunctionEigenstrain
block = 3
stress_free_temperature = 293.15
thermal_expansion_function = Fuel_CTE_function
eigenstrain_name = 'fuel_thermal_eigenstrain'
[]
[fuel_relocation]
type = UO2RelocationEigenstrain
block = 3
burnup_function = burnup
diameter = 0.00819211 #Fuel pellet diameter in m
rod_ave_lin_pow = power_profile
axial_power_profile = axial_peaking_factors
diametral_gap =164.0e-6
burnup_relocation_stop = 0.0
relocation_activation1 = 5000
eigenstrain_name = 'fuel_relocation_eigenstrain'
[]
[clad_thermal]
type = ZryThermal
block = 1
temperature = temp
[]
[clad_zrycreep]
type = ZryCreepLimbackHoppeUpdate
block = 1
fast_neutron_flux = fast_neutron_flux
fast_neutron_fluence = fast_neutron_fluence
zircaloy_material_type = stress_relief_annealed
max_inelastic_increment = 1.0e-4
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = 1
fast_neutron_fluence = fast_neutron_fluence
cold_work_factor = 0.5
oxygen_concentration = 0.02135
matpro_poissons_ratio = true
matpro_youngs_modulus = true
[]
[clad_inelastic_stress]
type = ComputeMultipleInelasticStress
block = 1
tangent_operator = elastic
inelastic_models = 'plasticity' #only use plasticity
[]
[clad_thermal_eigenstrain]
type = ZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 293.15
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[clad_irradiation_eigenstrain]
type = ZryIrradiationGrowthEigenstrain
block = 1
fast_neutron_fluence = fast_neutron_fluence
zircaloy_material_type = stress_relief_annealed
eigenstrain_name = 'clad_irradiation_growth_eigenstrain'
[]
[plasticity]
type = ZryPlasticityUpdate
block = 1
cold_work_factor = 0.5
fast_neutron_fluence = fast_neutron_fluence
fast_neutron_flux = fast_neutron_flux
plasticity_model_type = MATPRO
oxygen_concentration = 0.0
max_inelastic_increment = 1.0e-4
[]
[density_clad]
type = Density
block = 1
density = 6550
[]
[density_fuel]
type = Density
block = 3
[]
[fission_gas_release]
type = UO2Sifgrs
block = 3
temperature = temp
burnup_function = burnup
initial_porosity = 0.0475
grain_radius_const = 5.0e-6
gbs_model = false
transient_option = MICROCRACKING_BURNUP
[]
[ZryOxidation]
type = ZryOxidation
boundary = 2
clad_inner_radius = 0.00417806
clad_outer_radius = 0.00475336
use_coolant_channel = true
fast_neutron_flux = fast_neutron_flux
[]
[phase]
type = ZrPhase
block = 1
numerical_method = 2
[]
[strain_energy_density]
type = StrainEnergyDensity
incremental = true
[]
[]
[Dampers]
[BoundingValueNodalDamper]
type = BoundingValueNodalDamper
max_value = 3200
min_value = 200
variable = temp
[]
[contact_slip]
type = ContactSlipDamper
primary = 5
secondary = 10
min_damping_factor = 0.05
[]
[]
[Preconditioning]
[SMP]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-3
nl_max_its = 40
nl_rel_tol = 1e-4
nl_abs_tol = 1e-10
#start_time = 0
end_time = 125798900
dtmax = 10
dtmin = 1e-7
[TimeStepper]
type = IterationAdaptiveDT
dt = 10
optimal_iterations = 20
iteration_window = 4
linear_iteration_ratio = 100
timestep_limiting_function = power_profile
max_function_change = 1e5
force_step_every_function_point = true
timestep_limiting_postprocessor = material_timestep_control
time_t = '125798410 125798420 125798430 125798440 125798450 125798460 125798470 125798480 125798500 125798500.1 125798500.2 125798500.3 125798500.32 125798500.35'
time_dt = '1 1 1 1 1 1 1 1 0.001 0.001 0.001 0.001 0.001 0.001'
[]
[Quadrature]
order = FIFTH
side_order = SEVENTH
[]
[]
[Postprocessors]
[fis_gas_grain]
type = ElementIntegralFisGasGrainSifgrs
block = 3
outputs = exodus
[]
[fis_gas_boundary]
type = ElementIntegralFisGasBoundarySifgrs
block = 3
outputs = exodus
[]
[rod_input_power]
type = FunctionValuePostprocessor
function = power_profile
[]
[average_burnup_EAV]
type = ElementAverageValue
block = 3
variable = burnup
[]
[burnup_GWd]
type = FunctionValuePostprocessor
function = burnup_GWd
[]
#######################################
[penetration]
type = NodalVariableValue
variable = penetration
nodeid = 5535
use_displaced_mesh = 1
[]
[contact_pressure]
type = NodalVariableValue
variable = contact_pressure
nodeid = 5535
use_displaced_mesh = 1
[]
[gap_cond]
type = ElementalVariableValue
variable = gap_cond
elementid = 1664
use_displaced_mesh = 1
[]
[creep_hoop_strain]
type = ElementalVariableValue
variable = creep_strain_zz
elementid = 376
use_displaced_mesh = 1
[]
[elastic_hoop_strain]
type = ElementalVariableValue
variable = elastic_strain_zz
elementid = 376
use_displaced_mesh = 1
[]
[plastic_hoop_strain]
type = ElementalVariableValue
variable = plastic_strain_zz
elementid = 376
use_displaced_mesh = 1
[]
[total_hoop_strain]
type = ElementalVariableValue
variable = total_hoop_strain
elementid = 376
use_displaced_mesh = 1
[]
[clad_hoop_stress]
type = ElementalVariableValue
variable = hoop_stress
elementid = 376
use_displaced_mesh = 1
[]
[clad_axial_elongation]
type = NodalVariableValue
variable = disp_y
nodeid = 2451
use_displaced_mesh = 1
[]
[clad_oxide_thickness]
type = ElementalVariableValue
variable = oxide_thickness
elementid = 376
use_displaced_mesh = 1
[]
[clad_coolant_htc]
type = ElementalVariableValue
variable = clad_coolant_htc
elementid = 376
use_displaced_mesh = 1
[]
[coolant_temp]
type = ElementalVariableValue
variable = coolant_temp
elementid = 376
use_displaced_mesh = 1
[]
[fuel_centerline_temp]
type = NodalVariableValue
variable = temp
nodeid = 5504
[]
[fuel_surface_temp]
type = NodalVariableValue
variable = temp
nodeid = 5535
[]
[clad_inner_surface_temp]
type = NodalVariableValue
variable = temp
nodeid = 1307
[]
[clad_outer_surface_temp]
type = NodalVariableValue
variable = temp
nodeid = 1317
[]
[fuel_axial_elongation]
type = NodalVariableValue
variable = disp_y
nodeid = 8055
[]
[clad_radial_elongation]
type = NodalVariableValue
variable = disp_x
nodeid = 1317
[]
[fuel_radial_elongation]
type = NodalVariableValue
variable = disp_x
nodeid = 5535
[]
[SED_PPN_O]
type = ElementalVariableValue
variable = SED
elementid = 376
use_displaced_mesh = 1
[]
[SED_PPN_I]
type = ElementalVariableValue
variable = SED
elementid = 373
use_displaced_mesh = 1
[]
[OFract_PPN_O]
type = ElementalVariableValue
variable = oxywtfract_total
elementid = 376
use_displaced_mesh = 1
[]
[OGain_PPN_O]
type = ElementalVariableValue
variable = oxywtfgain_total
elementid = 376
use_displaced_mesh = 1
[]
#######################################
[max_fuel_temp]
type = NodalExtremeValue
block = 3
variable = temp
[]
[max_clad_temp]
type = NodalExtremeValue
block = 1
variable = temp
[]
[max_clad_SED]
type = ElementExtremeValue
block = 1
variable = SED
value_type = max
[]
[RAE]
type = RadialAverageEnthalpy
vector_postprocessor = rad_temp
radial_direction = x
axial_direction = y
axial_position = 0.3
temperature_name = temp
[]
[material_timestep_control]
type = MaterialTimeStepPostprocessor
block = 1
[]
[peak_RAE]
type = TimeExtremeValue
postprocessor = RAE
[]
[]
[VectorPostprocessors]
[ox_thick]
type = SideValueSampler
variable = oxide_thickness
boundary = 2
sort_by = y
outputs = 'outfile_oxide_thickness'
[]
[rad_temp]
type = NodalValueSampler
block = 3
sort_by = y
variable = temp
execute_on = timestep_end
outputs = 'outfile_radial_temp'
[]
[]
[StandardLWRFuelRodOutputs]
fuel_pellet_blocks = 3
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
csv = true
color = true
[outfile_oxide_thickness]
type = CSV
sync_times = '125798400 125798900'
sync_only = true
[]
[outfile_radial_temp]
type = CSV
enable = false
[]
[console]
type = Console
output_linear = true
max_rows = 10
[]
[chkfile]
type = CSV
show = 'plenum_temperature fission_gas_released_percentage
average_centerline_fuel_temperature average_burnup peak_RAE'
execute_on = 'FINAL'
[]
[exodus]
type = Exodus
time_step_interval = 4
end_time = 125798500
[]
[exodus_RIA]
type = Exodus
time_step_interval = 2
start_time = 125798495
[]
[]
(test/tests/zry_oxidation_cladding/zryoxidation.i)
# This test demonstrates the usage of the model for cladding oxidation from
# normal operating to high temperature (accident) conditions, through the
# epri_kwu_ce, Leistikow, and Prater relations.
#
# The purpose of this input is to be a control for the FuelPinGeometry version
# to compare against and confirm the error checking through cli-args.
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Mesh]
coord_type = RZ
[smeared_pellet_mesh]
type = FuelPinMeshGenerator
include_fuel = false
pellet_quantity = 1
pellet_height = 0.011143
pellet_outer_radius = 4.57e-3
clad_mesh_density = coarse
clad_gap_width = 70.0e-6
clad_thickness = 0.735e-3
clad_bot_gap_height = 1.0e-3
bottom_clad_height = 2.5e-3
top_clad_height = 2.5e-3
clad_top_gap_height = 5.0e-3
elem_type = QUAD4
[]
patch_size = 10
patch_update_strategy = iteration
partitioner = centroid
centroid_partitioner_direction = y
[]
[Functions]
[Temp_func]
type = PiecewiseLinear
x = '0.0 100000000.0 100000010.0 100000100.0 100000110.0 100000200.0 100000210.0 100000300.0'
y = '600.0 600.0 1100.0 1100.0 1850.0 1850.0 1950.0 1950.0 '
[]
[FNFlux_func]
type = PiecewiseLinear
x = '0.0 100000300.0'
y = '1.0e+17 1.0e+17 '
[]
[]
[Variables]
[temp]
order = FIRST
family = LAGRANGE
initial_condition = 600.0
[]
[disp_x]
order = FIRST
family = LAGRANGE
[]
[disp_y]
order = FIRST
family = LAGRANGE
[]
[]
[AuxVariables]
[fast_neutron_flux]
order = FIRST
family = LAGRANGE
initial_condition = 1.0e+17
[]
[scale_thickness] # ZrO2 scale thickness (m)
order = CONSTANT
family = MONOMIAL
[]
[oxyconc2_scale] # Oxygen concentration in ZrO2 scale (kg/m**2)
order = CONSTANT
family = MONOMIAL
[]
[oxyconc2_metal] # Oxygen concentration in metal (kg/m**2)
order = CONSTANT
family = MONOMIAL
[]
[oxyconc2_total] # Total oxygen concentration (oxide + metal) (kg/m**2)
order = CONSTANT
family = MONOMIAL
[]
[oxywtfract_metal] # Oxygen weight fraction in metal (/)
order = CONSTANT
family = MONOMIAL
[]
[oxywtfract_total] # Total oxygen weight fraction (oxide+metal) (/)
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[all]
strain = finite
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temp
[]
[]
[AuxKernels]
[fnflux]
type = FastNeutronFluxAux
variable = fast_neutron_flux
block = 1
function = FNFlux_func
execute_on = timestep_begin
[]
[scl_thickness]
type = MaterialRealAux
variable = scale_thickness
property = oxide_scale_thickness
boundary = 1
[]
[oconc_scale]
type = MaterialRealAux
variable = oxyconc2_scale
property = gained_oxygen_concentration_scale
boundary = 1
[]
[oconc_metal]
type = MaterialRealAux
variable = oxyconc2_metal
property = gained_oxygen_concentration_metal_wall
boundary = 1
[]
[oconc_total]
type = MaterialRealAux
variable = oxyconc2_total
property = gained_oxygen_concentration_total
boundary = 1
[]
[ofract_metal]
type = MaterialRealAux
variable = oxywtfract_metal
property = current_oxygen_weight_frac_metal_wall
boundary = 1
[]
[ofract_total]
type = MaterialRealAux
variable = oxywtfract_total
property = current_oxygen_weight_frac_total
boundary = 1
[]
[]
[BCs]
[bottom_T]
type = FunctionDirichletBC
variable = temp
function = Temp_func
boundary = 1
[]
[x_disp]
type = DirichletBC
variable = disp_x
value = 0
boundary = 1
[]
[y_disp]
type = DirichletBC
variable = disp_y
value = 0
boundary = 2
[]
[]
[Materials]
[elasticity_tensor]
type = ZryElasticityTensor
block = 1
[]
[stress]
type = ComputeFiniteStrainElasticStress
block = 1
[]
[thermal]
type = ZryThermal
block = 1
temperature = temp
[]
[oxidation_zry]
type = ZryOxidation
boundary = 1
normal_operating_temperature_model = epri_kwu_ce
high_temperature_model = leistikow
temperature = temp
fast_neutron_flux = fast_neutron_flux
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = 'lu superlu_dist'
l_tol = 1.0e-08
nl_abs_tol = 1.0e-08
nl_rel_tol = 1.0e-08
start_time = 0.0
num_steps = 5000
end_time = 100000300
[TimeStepper]
type = IterationAdaptiveDT
dt = 1.0e+06
optimal_iterations = 6
iteration_window = 2
linear_iteration_ratio = 100
time_t = '0.0 100000000.'
time_dt = '1.0e+06 10.0 '
growth_factor = 1.0
[]
[]
[Postprocessors]
[_dt]
type = TimestepSize
[]
[temp]
type = NodalVariableValue
variable = temp
nodeid = 0
execute_on = 'initial timestep_end'
[]
[scale_thickness]
type = ElementalVariableValue
elementid = 0
variable = scale_thickness
[]
[oxyconc2_scale]
type = ElementalVariableValue
elementid = 0
variable = oxyconc2_scale
[]
[oxyconc2_metal]
type = ElementalVariableValue
elementid = 0
variable = oxyconc2_metal
[]
[oxyconc2_total]
type = ElementalVariableValue
elementid = 0
variable = oxyconc2_total
[]
[oxywtfract_metal]
type = ElementalVariableValue
elementid = 0
variable = oxywtfract_metal
[]
[oxywtfract_total]
type = ElementalVariableValue
elementid = 0
variable = oxywtfract_total
[]
[]
[Outputs]
exodus = true
[]
(assessment/LWR/validation/LOCA_Hardy_cladding_test/analysis/5pt5MPa/25C_sec/25C_sec_Hardy_Tube_Test_5pt5MPa.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
volumetric_locking_correction = false
displacements = 'disp_x disp_y'
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
group_variables = 'disp_x disp_y'
[]
[Mesh]
coord_type = RZ
patch_size = 10
patch_update_strategy = iteration
partitioner = centroid
centroid_partitioner_direction = y
[gen]
type = FuelPinMeshGenerator
include_fuel = false
include_clad = true
pellet_outer_radius = 0.0072527
clad_gap_width = 0.0
clad_top_gap_height = 0.0
clad_bot_gap_height = 0.0
clad_thickness = 0.38e-3
pellet_height = 0.5
pellet_quantity = 1
clad_mesh_density = customize
nx_c = 2
ny_c = 50
elem_type = QUAD8
[]
[]
[Variables]
[temperature]
initial_condition = 600.0
[]
[]
[AuxVariables]
[creep_rate_aux]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[total_hoop_strain]
order = CONSTANT
family = MONOMIAL
[]
[burst_stress]
order = CONSTANT
family = MONOMIAL
[]
[burst]
order = CONSTANT
family = MONOMIAL
[]
[]
[Functions]
[pressure_function]
type = PiecewiseLinear
x = '0 40'
y = '1 1'
[]
[temp_function]
type = PiecewiseLinear
y = '600 1600'
[]
[temperature_profile]
type = PiecewiseBilinear
y = '0 40'
x = '0 0.25224 0.50448'
z = '0.995 1.01 0.995 0.995 1.01 0.995'
axis = 1
[]
[inner_temperature]
type = CompositeFunction
functions = 'temp_function temperature_profile'
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[clad]
block = clad
add_variables = true
strain = FINITE
decomposition_method = EigenSolution
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz elastic_strain_xx elastic_strain_yy elastic_strain_zz
creep_strain_xx creep_strain_yy creep_strain_zz hoop_stress'
extra_vector_tags = 'ref'
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
extra_vector_tags = 'ref'
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
extra_vector_tags = 'ref'
[]
[]
[AuxKernels]
[creep_rate_aux]
type = MaterialRealAux
variable = creep_rate_aux
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[creep_rate]
type = MaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[total_hoop_strain]
type = RankTwoAux
rank_two_tensor = total_strain
variable = total_hoop_strain
index_i = 2
index_j = 2
execute_on = timestep_end
block = clad
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = clad_outside_right
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = clad_outside_right
execute_on = timestep_end
[]
[]
[BCs]
[Pressure]
[outer_surface]
boundary = 'clad_outside_bottom clad_outside_right clad_outside_top'
factor = 0.0
function = pressure_function
[]
[inner_surface]
boundary = 'clad_inside_right clad_inside_bottom clad_inside_top'
function = pressure_function
[]
[]
[u_bottom_fix]
type = DirichletBC
variable = disp_y
boundary = 1001
value = 0.0
[]
[x_fix]
type = DirichletBC
variable = disp_x
boundary = centerline
value = 0.0
[]
[temp_bc]
type = FunctionDirichletBC
function = inner_temperature
variable = temperature
boundary = 'clad_inside_bottom clad_inside_right clad_inside_top'
[]
[]
[Materials]
[clad_thermal]
type = ZryThermal
block = clad
zry_thermal_properties_model = MATPRO
temperature = temperature
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = clad
matpro_youngs_modulus = true
matpro_poissons_ratio = true
temperature = temperature
[]
[clad_stress]
type = ComputeMultipleInelasticStress
inelastic_models = 'clad_zrycreep'
block = clad
tangent_operator = nonlinear
[]
[clad_zrycreep]
type = ZryCreepLOCAUpdate
block = clad
temperature = temperature
model_irradiation_creep = false
model_primary_creep = true
model_thermal_creep = true
temperature_loca_creep_begin = 840 # values from the report
temperature_standard_thermal_creep_end = 975
[]
[thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = clad
temperature = temperature
stress_free_temperature = 600.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[clad_density]
type = Density
block = clad
density = 6550.0
[]
[phase]
type = ZrPhase
block = clad
temperature = temperature
numerical_method = 2
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = clad_outside_right
failure_criterion = combined_overstress_and_overstrain
hoop_stress = hoop_stress
hoop_creep_strain = creep_strain_zz
effective_strain_rate_creep = creep_rate_aux
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.0e-5
nl_abs_tol = 1.0e-8
start_time = 0
n_startup_steps = 1
end_time = 40
dtmax = 1
dtmin = 0.0000001
[TimeStepper]
type = IterationAdaptiveDT
timestep_limiting_postprocessor = material_timestep
dt = 1.0
[]
[]
[Postprocessors]
[ave_clad_temp]
type = SideAverageValue
boundary = clad_outside_right
variable = temperature
[]
[gas_volume]
type = InternalVolume
boundary = all_clad_interior
execute_on = 'initial linear'
[]
[max_clad_temp]
type = NodalExtremeValue
block = clad
value_type = max
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = clad
[]
[max_hoop_stress]
type = ElementExtremeValue
block = clad
value_type = max
variable = hoop_stress
[]
[vonmises_stress_clad]
type = ElementAverageValue
block = clad
variable = vonmises_stress
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = total_hoop_strain
[]
[max_disp_x]
type = NodalExtremeValue
block = clad
value_type = max
variable = disp_x
[]
[min_burst_stress]
type = ElementExtremeValue
block = clad
value_type = min
variable = burst_stress
[]
[burst]
type = ElementExtremeValue
block = clad
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = clad
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
[]
[PerformanceMetricOutputs]
[]
[Outputs]
color = false
perf_graph = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[csv]
type = CSV
[]
[chkfile]
type = CSV
show = 'max_disp_x max_hoop_stress vonmises_stress_clad'
execute_on = 'FINAL'
[]
[]
[UserObjects]
[terminator1]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '5'
include_fuel = false
[]
[]
(test/tests/standard_lwr_outputs_action/clad_only.i)
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = clad_only.e
[]
[]
[Variables]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
x = '0.0 0.025'
y = '0.0 300.0 300.0'
z = '1000.0 1400.0 1400.0 2000.0 1400.0 1400.0'
axis = 1 # (0,1,2) => (x,y,z)
[]
[power_history]
type = PiecewiseLinear
x = '0.000000 10800'
y = '0.000000 16404.200000' #LHR5
scale_factor = 1
[]
[axial_peaking_factors]
type = PiecewiseBilinear
x = '0.00324 3.77797'
y = '0.000000 10800'
z = '1.0 1.0 1.0 1.0'
axis = 1
scale_factor = 1
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 2000. '
y = '1.e+05 1.e+05 7.4e+05'
[]
[pressure_ramp]
type = PiecewiseLinear
scale_factor = 1
x = '0 10800.0'
y = '0.00651 1.0'
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[clad]
block = clad
add_variables = true
strain = finite
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
[]
[]
[BCs]
[no_x_all]
type = DirichletBC
variable = disp_x
boundary = 12
value = 0.0
[]
[no_y_clad_bottom]
type = DirichletBC
variable = disp_y
boundary = '1'
value = 0.0
[]
[Pressure]
[coolantPressure]
boundary = '1 2 3'
factor = 15.5e6
function = pressure_ramp
[]
[]
[Pressure]
[inner_pressure]
boundary = 7
function = inner_pressure_func
[]
[]
[]
[CoolantChannel]
[convective_clad_surface]
boundary = '1 2 3'
variable = temperature
inlet_temperature = 580
inlet_pressure = 15.5e6
inlet_massflux = 3800
rod_diameter = 0.948e-2
rod_pitch = 1.26e-2
linear_heat_rate = power_history
axial_power_profile = axial_peaking_factors
[]
[]
[Materials]
[thermal]
block = 1
type = ZryThermal
temperature = temperature
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = clad
[]
[clad_stress]
type = ComputeFiniteStrainElasticStress
block = clad
[]
[density]
type = Density
block = clad
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -sub_pc_type'
petsc_options_value = 'asm lu'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0.
end_time = 20.
dtmax = 10.0
dtmin = 10
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
[]
[Outputs]
perf_graph = true
exodus = false
csv = true
[console]
type = Console
output_linear = true
max_rows = 2
[]
[chkfile]
type = CSV
file_base = clad_only_chkfile
show = 'average_interior_clad_temperature'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-15/puzry-15.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-15.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 2000. '
y = '1.e+05 1.e+05 1.183e+07' # Linear increase at 0.1173 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 2000. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = EigenSolution
[]
[]
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = MaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = FunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = DirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = DirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1.e+11
poissons_ratio = 0.3
block = 1
[]
[creep_update]
type = ZryCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 1.e-04
temperature = temperature
temperature_standard_thermal_creep_end = 700
temperature_loca_creep_begin = 900.
[]
[creep]
type = ComputeMultipleInelasticStress
block = 1
tangent_operator = elastic
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = Density
block = 1
[]
[phase]
type = ZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
active = 'smp'
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0.
n_startup_steps = 1
end_time = 2000.
dtmax = 1.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-15_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/RIA_NSRR_FK/analysis/FK5/FK05.i)
# This file was created using BIF with the following inputs:
# FK05/FK05.var - md5sum: 789d603cfbdaaeb2625ea98056214f6f
# pulse.tpl - md5sum: 37e5a6b8a0c63ad020906dada3472585
[GlobalParams]
density = 10310.8809782
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
energy_per_fission = 3.2e-11
a_lower = 0.01822
a_upper = 0.12422
temperature = temp
volumetric_locking_correction = false
[]
[Mesh]
coord_type = RZ
[smeared_pellet_mesh]
type = FuelPinMeshGenerator
clad_mesh_density = customize
pellet_mesh_density = customize
elem_type = QUAD8
ny_p = 100
nx_c = 4
ny_c = 100
nx_p = 12
ny_cu = 3
ny_cl = 3
bx_p = 0.75
clad_bot_gap_height = 0.00152
bottom_clad_height = 0.0167
top_clad_height = 0.0167
clad_thickness = 0.00086
pellet_outer_radius = 0.00527
clad_top_gap_height = 0.05265
pellet_height = 0.106
clad_gap_width = 1e-05
pellet_quantity = 1
[]
patch_size = 5
patch_update_strategy = auto
partitioner = centroid
centroid_partitioner_direction = y
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
converge_on = 'disp_x disp_y temp'
[]
[Variables]
[temp]
initial_condition = 293
block = '1 3'
[]
[]
[AuxVariables]
[BuTC]
[]
[gap]
order = CONSTANT
family = MONOMIAL
[]
[fast_neutron_flux]
block = 1
[]
[fast_neutron_fluence]
block = 1
[]
[buavg]
order = CONSTANT
family = MONOMIAL
[]
[fission_rate]
initial_condition = 0
[]
[grain_radius]
block = 3
initial_condition = 5.96e-6
[]
[integral_burnup]
order = CONSTANT
family = MONOMIAL
[]
[pellet_id]
order = CONSTANT
family = MONOMIAL
block = 3
[]
[porosity]
order = CONSTANT
family = MONOMIAL
initial_condition = 0.0592261881186
[]
[SED]
order = CONSTANT
family = MONOMIAL
[]
[]
[Functions]
[linear_heat_rate_profile]
type = PiecewiseLinear
data_file = pulse.csv
format = columns
[]
[flux]
type = ConstantFunction
value = 0.0
[]
[axial_peaking_factors]
type = ConstantFunction
value = 1
[]
[coolant_pressure_ramp]
type = ConstantFunction
value = 101325
[]
[linear_heat_generation_rate]
type = CompositeFunction
functions = 'linear_heat_rate_profile axial_peaking_factors'
[]
[axial_flux]
type = CompositeFunction
functions = 'flux axial_peaking_factors'
[]
[burnup_thermal_conductivity]
type = ConstantFunction
value = 1 # should be burnup / 950
[]
[radial_power_profile]
type = PiecewiseLinear
data_file = RadialPowerProfile.csv
format = columns
axis = X
[]
[radial_burnup_profile]
type = PiecewiseLinear
data_file = RadialBurnupProfile.csv
format = columns
axis = X
[]
[initial_burnup]
type = CompositeFunction
functions = 'burnup_thermal_conductivity radial_burnup_profile'
[]
[]
[Burnup]
[burnup]
block = 3
rod_ave_lin_pow = linear_heat_rate_profile
axial_power_profile = axial_peaking_factors
rpf_input = radial_power_profile
num_radial = 80
num_axial = 49
fuel_inner_radius = 0.0
fuel_outer_radius = 0.00527
fuel_volume_ratio = 1.0
isotopes = 'U235 U238 Pu239 Pu240 Pu241 Pu242'
isotope_fractions = '0.045 0.955 0.0 0.0 0.0 0.0'
[]
[]
[Physics/SolidMechanics/QuasiStatic]
add_variables = true
[fuel]
block = 3
strain = FINITE
incremental = true
eigenstrain_names = 'fuel_thermal_eigenstrain
fuel_volumetric_swelling_eigenstrain'
extra_vector_tags = 'ref'
generate_output = 'vonmises_stress hydrostatic_stress elastic_strain_xx
elastic_strain_yy elastic_strain_zz stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz'
decomposition_method = EigenSolution
[]
[clad]
block = 1
strain = FINITE
incremental = true
eigenstrain_names = 'clad_thermal_eigenstrain'
extra_vector_tags = 'ref'
generate_output = 'vonmises_stress elastic_strain_xx
elastic_strain_yy elastic_strain_zz stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz creep_strain_xx creep_strain_yy creep_strain_zz'
decomposition_method = EigenSolution
[]
[]
[Kernels]
[gravity]
type = Gravity
variable = disp_y
value = -9.81
block = '1 3'
extra_vector_tags = 'ref'
[]
[heat]
type = HeatConduction
variable = temp
block = '1 3'
extra_vector_tags = 'ref'
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temp
block = '1 3'
extra_vector_tags = 'ref'
[]
[heat_source]
type = NeutronHeatSource
fission_rate = fission_rate
variable = temp
block = 3
extra_vector_tags = 'ref'
[]
[]
[AuxKernels]
[BuTC]
type = FunctionAux
block = 3
variable = BuTC
function = initial_burnup
[]
[pelletid]
type = PelletIdAux
block = 3
variable = pellet_id
number_pellets = 1
execute_on = initial
[]
[gap]
type = SpatialUserObjectAux
block = 3
variable = gap
execute_on = timestep_end
user_object = avg_gap
[]
[buavg]
type = SpatialUserObjectAux
block = 3
variable = buavg
execute_on = timestep_end
user_object = integral_burnup
[]
[fast_neutron_flux]
type = FastNeutronFluxAux
variable = fast_neutron_flux
function = axial_flux
block = 1
execute_on = timestep_begin
[]
[fast_neutron_fluence]
type = FastNeutronFluenceAux
variable = fast_neutron_fluence
block = 1
fast_neutron_flux = fast_neutron_flux
execute_on = timestep_begin
[]
[fuel_porosity]
type = PorosityAuxUO2
block = 3
variable = porosity
execute_on = timestep_begin
[]
[grain_radius]
type = GrainRadiusAux
block = 3
variable = grain_radius
temperature = temp
execute_on = timestep_begin
[]
[SED]
type = MaterialRealAux
variable = SED
property = strain_energy_density
execute_on = timestep_end
block = 1
[]
[]
[Contact]
[mechanical]
model = coulomb
formulation = mortar
primary = 5
secondary = 10
friction_coefficient = 0.4
c_normal = 1e+12
c_tangential = 1e+24
tangential_lm_scaling = 1.0e-16
normal_lm_scaling = 1.0e-10
[]
[]
[ThermalContactMortar]
[thermal_contact]
secondary_variable = temp
primary_boundary = '5'
secondary_boundary = '10'
layer_thickness = layer_thickness_action
roughness_coef = 3.2
roughness_primary = 1.5e-6
roughness_secondary = 1.75e-6
jump_distance_model = LANNING
plenum_pressure = plenum_pressure
initial_moles = initial_moles
gas_released = fission_gas_released
contact_pressure = mechanical_normal_lm
thermal_lm_scaling = 1.0e-2
[]
[]
[BCs]
[no_x_all]
type = DirichletBC
variable = disp_x
boundary = 12
value = 0.0
[]
[no_y_fuel_bottom]
type = DirichletBC
variable = disp_y
boundary = 20
value = 0.0
[]
[no_y_clad_bottom]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[]
[coolant_temp]
type = DirichletBC
boundary = '1 2 3'
variable = temp
value = 293
[]
[Pressure]
[coolantPressure]
boundary = '1 2 3'
factor = 1
function = coolant_pressure_ramp
[]
[]
[PlenumPressure]
[plenumPressure]
boundary = '10 5'
initial_pressure = 0.5e6
startup_time = 0
R = 8.314462
output_initial_moles = initial_moles
temperature = plenum_temperature
volume = plenum_volume
material_input = fission_gas_released
output = plenum_pressure
initial_temperature = 293
[]
[]
[]
[Materials]
[fuel_swelling]
type = UO2VolumetricSwellingEigenstrain
block = 3
burnup = burnup
initial_fuel_density = 10310.8809782
total_densification = 0.006
gas_swelling_model_type = SIFGRS
eigenstrain_name = 'fuel_volumetric_swelling_eigenstrain'
[]
[fuel_thermal]
type = UO2Thermal
thermal_conductivity_model = NFIR
block = 3
temperature = temp
burnup = BuTC
initial_porosity = 0.0592261881186
[]
[fuel_elasticity_tensor]
type = UO2ElasticityTensor
block = 3
[]
[fuel_thermal_expansion]
type = UO2ThermalExpansionMartinEigenstrain
block = 3
stress_free_temperature = 293
eigenstrain_name = 'fuel_thermal_eigenstrain'
[]
[fuel_elastic_stress]
type = ComputeFiniteStrainElasticStress
block = '3'
[]
[clad_thermal]
type = ZryThermal
block = 1
temperature = temp
[]
[clad_inelastic_stress]
type = ComputeMultipleInelasticStress
block = 1
tangent_operator = elastic
inelastic_models ='plasticity'
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = 1
fast_neutron_fluence = fast_neutron_fluence
initial_fast_fluence = 1.20e26
cold_work_factor = 0.01
matpro_youngs_modulus = true
matpro_poissons_ratio = true
[]
## TODO: Creep is not active, but is transfered from the SM version.
## Adding creep causes the Peak Hoop strain to best match the FALCON
## results given by R. Montgomery and D. Sunderland. Only retaining
## plasticity matches the results from Wenfeng Liu, John Alvis, Robert Montgomery, and Ken Yueh
[clad_creep_stress]
type = ZryCreepLimbackHoppeUpdate
block = 1
fast_neutron_flux = fast_neutron_flux
fast_neutron_fluence = fast_neutron_fluence
initial_fast_fluence = 1.20e26
[]
[clad_thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 293.0
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[plasticity]
type = ZryPlasticityUpdate
block = 1
initial_fast_fluence = 1.20e26
fast_neutron_flux = fast_neutron_flux
fast_neutron_fluence = fast_neutron_fluence
cold_work_factor = .01
plasticity_model_type = MATPRO
output_properties = yield_stress
outputs = all
zircaloy_alloy_type = 4
[]
[fission_gas_release]
type = UO2Sifgrs
block = 3
temperature = temp
fission_rate = fission_rate
grain_radius = grain_radius
gbs_model = true
burnup = BuTC
transient_option = MICROCRACKING
[]
[clad_density]
type = Density
block = 1
density = 6551
[]
[fuel_density]
type = Density
block = 3
[]
[strain_energy_density]
type = StrainEnergyDensity
block = '1 3'
incremental = true
[]
[]
[UserObjects]
[avg_gap]
type = LayeredAverage
block = 3
variable = penetration
direction = y
num_layers = 48
[]
[pbz]
type = PelletBrittleZone
block = 3
pellet_id = pellet_id
temperature = temp
pellet_radius = 0.00527
number_pellets = 1
execute_on = timestep_begin
[]
[integral_burnup]
type = LayeredAverage
block = 3
variable = burnup
direction = y
num_layers = 1
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_converged_reason -ksp_converged_reason -snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package -mat_mffd_err -pc_factor_shift_type '
'-pc_factor_shift_amount'
petsc_options_value = 'lu superlu_dist 1e-5 NONZERO 1e-12'
line_search = 'none'
l_max_its = 40
l_tol = 8e-3
nl_max_its = 40
nl_rel_tol = 1e-3
nl_abs_tol = 1e-10
dtmin = 0.00001
dtmax = 1.0
start_time = 0
end_time = 100
[TimeStepper]
type = IterationAdaptiveDT
dt = 0.0001
optimal_iterations = 200
linear_iteration_ratio = 100
timestep_limiting_function = linear_heat_rate_profile
max_function_change = 500000
force_step_every_function_point = true
[]
[]
[Dampers]
[limitT]
type = MaxIncrement
max_increment = 200.0
variable = temp
[]
[limitX]
type = MaxIncrement
max_increment = 1e-4
variable = disp_x
[]
[]
[Postprocessors]
[max_hoop_strain]
type = ElementExtremeValue
variable = strain_zz
block = 1
[]
[max_SED]
type = ElementExtremeValue
variable = SED
block = 1
[]
[average_grain_radius]
type = ElementAverageValue
block = 3
outputs = 'exodus'
variable = grain_radius
[]
[clad_inner_vol]
type = InternalVolume
boundary = 7
outputs = 'exodus'
execute_on = 'timestep_begin initial'
[]
[flux_from_clad]
type = SideDiffusiveFluxIntegral
variable = temp
boundary = 5
diffusivity = thermal_conductivity
outputs = 'exodus'
[]
[flux_from_fuel]
type = SideDiffusiveFluxIntegral
variable = temp
boundary = 10
diffusivity = thermal_conductivity
outputs = 'exodus'
[]
[rod_total_power]
type = ElementIntegralPower
variable = temp
fission_rate = fission_rate
block = 3
[]
[rod_input_power]
type = FunctionValuePostprocessor
function = linear_heat_rate_profile
scale_factor = 0.106
[]
[average_fission_rate]
type = ElementAverageValue
variable = fission_rate
block = '3'
[]
[RAE]
type = RadialAverageEnthalpy
vector_postprocessor = rad_temp
radial_direction = x
axial_direction = y
axial_position = 0.0503
temperature_name = temp
[]
[peak_RAE]
type = TimeExtremeValue
postprocessor = RAE
[]
[]
[VectorPostprocessors]
[rad_temp]
type = NodalValueSampler
block = 3
sort_by = y
variable = temp
execute_on = timestep_end
outputs = dummy
[]
[]
[StandardLWRFuelRodOutputs]
fuel_pellet_blocks = 3
cladding_blocks = 1
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[chkfile]
type = CSV
show = 'average_centerline_fuel_temperature average_fission_rate fission_gas_released_percentage peak_RAE rod_total_power'
execute_on = 'FINAL'
[]
[console]
type = Console
max_rows = 25
output_linear = true
[]
[dummy]
type = CSV
enable = false
[]
[]
(assessment/LWR/validation/LOCA_ANL_cladding_burst_tests/analysis/OCL11/OCL11_ad.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
displacements = 'disp_x disp_y'
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
[]
[Mesh]
coord_type = RZ
[smeared_pellet_mesh]
type = FuelPinMeshGenerator
pellet_quantity = 1
pellet_height = 0.270
pellet_outer_radius = 4.78e-3
clad_bot_gap_height = 0.001
clad_top_gap_height = 0.013
clad_thickness = 0.71e-3
clad_gap_width = 0.1e-3
pellet_mesh_density = coarse
clad_mesh_density = coarse
elem_type = QUAD8
[]
patch_size = 10
patch_update_strategy = auto
partitioner = centroid
centroid_partitioner_direction = y
[]
[Variables]
[temperature]
initial_condition = 300.0
[]
[]
[Functions]
[temperature_func]
type = PiecewiseLinear
x = '0 496.02 520.74 528.12 545.94 551.28 671.52 885.3 1195.74 1410.36 1657.86 1680 1690 1700 1710 1720 1730 1740 1750 1760 1770 1780 1790 1800 1810 1820 1830 1840 1848'
y = '300 300 405.465 482.048 583.351 632.287 634.297 632.825 630.378 631.059 632.59 633 683 733 783 833 883 933 983 1033 1083 1133 1183 1233 1283 1333 1383 1433 1477'
[]
[temperature_profile]
type = PiecewiseBilinear
data_file = 'temp_profile.csv'
axis = 1
[]
[cladding_temperature]
type = CompositeFunction
functions = 'temperature_func temperature_profile'
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[pellets]
block = pellet
use_automatic_differentiation = true
add_variables = true
strain = FINITE
decomposition_method = TaylorExpansion
eigenstrain_names = 'fuel_thermal_strain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
generate_output = 'vonmises_stress hydrostatic_stress stress_xx stress_yy
stress_zz strain_xx strain_yy strain_zz hoop_stress'
extra_vector_tags = 'ref'
[]
[clad]
block = clad
use_automatic_differentiation = true
add_variables = true
strain = FINITE
decomposition_method = TaylorExpansion
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz hoop_stress'
extra_vector_tags = 'ref'
[]
[]
[AuxVariables]
[creep_rate_aux]
order = CONSTANT
family = MONOMIAL
block = clad
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
block = clad
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
block = clad
[]
[scale_thickness]
order = CONSTANT
family = MONOMIAL
block = clad
[]
[oxywtfract_total]
order = CONSTANT
family = MONOMIAL
block = clad
[]
[oxywtfgain_total]
order = CONSTANT
family = MONOMIAL
block = clad
[]
[burst_stress]
order = CONSTANT
family = MONOMIAL
block = clad
[]
[burst]
order = CONSTANT
family = MONOMIAL
block = clad
[]
[]
[Kernels]
[heat]
type = ADHeatConduction
variable = temperature
extra_vector_tags = 'ref'
[]
[heat_ie]
type = ADHeatConductionTimeDerivative
variable = temperature
extra_vector_tags = 'ref'
[]
[]
[AuxKernels]
[creep_rate_aux]
type = ADMaterialRealAux
variable = creep_rate_aux
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = ADMaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
block = clad
[]
[scl_thickness]
type = ADMaterialRealAux
variable = scale_thickness
property = oxide_scale_thickness
boundary = clad_outside_right
[]
[ofract_total]
type = ADMaterialRealAux
variable = oxywtfract_total
property = current_oxygen_weight_frac_total
boundary = clad_outside_right
[]
[ofgain_total]
type = ADMaterialRealAux
boundary = clad_outside_right
variable = oxywtfgain_total
property = oxygen_weight_frac_gained_total
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = clad_outside_right
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = clad_outside_right
execute_on = timestep_end
[]
[]
[ThermalContact]
[thermal_contact]
type = GapHeatTransfer
primary = 5
secondary = 10
variable = temperature
gap_conductivity = 0.15 # k of He per Netzsch
[]
[]
[BCs]
[clad_surface_temperature]
type = ADFunctionDirichletBC
variable = temperature
boundary = '2'
function = cladding_temperature
[]
[no_x_all]
type = ADDirichletBC
variable = disp_x
boundary = 12
value = 0.0
[]
[no_y_clad_bottom]
type = ADDirichletBC
variable = disp_y
boundary = '1'
value = 0.0
[]
[no_y_fuel_bottom]
type = ADDirichletBC
variable = disp_y
boundary = '1020'
value = 0.0
[]
[Pressure]
[outer_pressure]
boundary = '1 2 3'
factor = 101325
[]
[inner_pressure]
boundary = '4 5 6'
factor = 8.28e6
[]
[]
[]
[PlenumTemperature]
[plenum_temp]
boundary = 5
inner_surfaces = '5'
outer_surfaces = '10'
temperature = temperature
[]
[]
[CoolantChannel]
[convective_clad_surface]
boundary = 2
variable = temperature
inlet_temperature = 473.0
inlet_pressure = 101325
inlet_massflux = 1.0 # kg/m^2-sec # almost stagnant steam
rod_diameter = 0.01118
rod_pitch = 1.26e-02 # default
oxide_thickness = scale_thickness
thermal_conductivity = reg_thermal_conductivity
[]
[]
[Materials]
[fuel_thermal]
type = ADHeatConductionMaterial
block = pellet
thermal_conductivity = 3.5
specific_heat = 330.0
[]
[fuel_converter]
type = MaterialADConverter
block = pellet
ad_props_in = 'thermal_conductivity'
reg_props_out = 'reg_thermal_conductivity'
[]
[fuel_elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
block = pellet
youngs_modulus = 2.0e11
poissons_ratio = 0.345
[]
[fuel_elastic_stress]
type = ADComputeFiniteStrainElasticStress
block = pellet
[]
[fuel_thermal_expansion]
type = ADComputeThermalExpansionEigenstrain
block = pellet
thermal_expansion_coeff = 10.0e-6
temperature = temperature
stress_free_temperature = 300.0
eigenstrain_name = fuel_thermal_strain
[]
[fuel_density]
type = ADDensity
block = pellet
density = 10980.0 #perfectly dense UO2
[]
[clad_thermal]
type = ADZryThermal
block = clad
temperature = temperature
[]
[clad_converter]
type = MaterialADConverter
block = clad
ad_props_in = 'thermal_conductivity'
reg_props_out = 'reg_thermal_conductivity'
[]
[clad_elasticity_tensor]
type = ADZryElasticityTensor
block = clad
matpro_youngs_modulus = false
matpro_poissons_ratio = false
[]
[clad_stress]
type = ADComputeMultipleInelasticStress
inelastic_models = 'clad_zrycreep'
block = clad
[]
[hill_constants]
type = ADHillConstants
hill_constants = "0.5 0.5 0.5 1.0 1.0 1.0"
#hill_constants = "0.738 0.174 0.588 1.0 1.0 1.0"
#function_names = "F G H L M N"
[]
[clad_zrycreep]
type = ADZryAnisoCreepLOCAUpdate
block = clad
temperature = temperature
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
temperature_loca_creep_begin = 501
temperature_standard_thermal_creep_end = 500
fract_beta_phase_name = 'ad_fract_beta_phase'
[]
[thermal_expansion]
type = ADZryThermalExpansionMATPROEigenstrain
block = clad
temperature = temperature
stress_free_temperature = 300.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[clad_density]
type = ADDensity
block = clad
density = 6550.0
[]
[phase]
type = ZrPhase
block = clad
temperature = temperature
numerical_method = 2
[]
[phase_converter]
type = MaterialADConverter
block = clad
reg_props_in = 'fract_beta_phase'
ad_props_out = 'ad_fract_beta_phase'
[]
[oxidation]
type = ADZryOxidation
boundary = clad_outside_right
temperature = temperature
clad_inner_radius = 4.88e-3 #checked
clad_outer_radius = 5.59e-3 #checked
normal_operating_temperature_model = epri_kwu_ce
high_temperature_model = leistikow
use_coolant_channel = true
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = clad_outside_right
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate_aux
temperature = temperature
fraction_beta_phase = fract_beta_phase
fraction_oxygen_gain = oxywtfgain_total
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
verbose = true
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.0e-04
nl_abs_tol = 1.0e-08
start_time = 0
n_startup_steps = 1
end_time = 1800.0
dtmax = 100
dtmin = 0.0001
[TimeStepper]
type = IterationAdaptiveDT
timestep_limiting_postprocessor = material_timestep
dt = 10.0
time_dt = '100 10'
time_t = '10 400'
[]
[]
[Postprocessors]
[ave_clad_temp]
type = SideAverageValue
boundary = clad_outside_right
variable = temperature
[]
[gas_volume]
type = InternalVolume
boundary = 9
execute_on = 'initial linear'
[]
[max_clad_temp]
type = NodalExtremeValue
block = clad
value_type = max
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = clad
[]
[max_oxygen_fract]
type = ElementExtremeValue
block = clad
value_type = max
variable = oxywtfract_total
[]
[max_betaph_fract]
type = ElementExtremeValue
block = clad
value_type = max
variable = fract_beta_phase
[]
[max_hoop_stress]
type = ElementExtremeValue
block = clad
value_type = max
variable = hoop_stress
[]
[vonmises_stress_clad]
type = ElementAverageValue
block = clad
variable = vonmises_stress
[]
[min_burst_stress]
type = ElementExtremeValue
block = clad
value_type = min
variable = burst_stress
[]
[burst]
type = ElementExtremeValue
block = clad
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = clad
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[oxide_thickness]
type = ElementAverageValue
block = clad
variable = scale_thickness
execute_on = TIMESTEP_END
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
[]
[PerformanceMetricOutputs]
[]
[Outputs]
exodus = true
csv = true
color = false
perf_graph = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
show = 'max_clad_temp max_hoop_stress vonmises_stress_clad'
execute_on = 'FINAL'
[]
[]
[UserObjects]
[terminator1]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
[]
[]
(assessment/LWR/validation/LOCA_REBEKA_cladding_burst_tests/analysis/rebeka_2d_12MPa/rebeka_singlerod_2d_12MPa_aniso.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
order = SECOND
family = LAGRANGE
displacements = 'disp_x disp_y'
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = rebeka_singlerod.e
[]
[]
[Variables]
[temperature]
initial_condition = 573.0
[]
[]
[Functions]
[temperature_func]
type = PiecewiseLinear
x = '0. 700. '
y = '573. 1273.' # From 300 to 1000 C at 1 K/s
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 700. '
y = '12.e+06 12.e+06' # 120 bar
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 700. '
y = '1.e+05 1.e+05' # atmospheric pressure
[]
# Circumferential steady-state creep test and analysis of Zircaloy-4 fuel cladding
# Nuclear Engineering and Design, 53, 2312-2322 (2021)
[F]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.738 0.738 0.57'
[]
[G]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.174 0.174 0.45'
[]
[H]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.588 0.588 0.48'
[]
[L]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[M]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[N]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[clad]
block = cladding
add_variables = true
strain = FINITE
decomposition_method = TaylorExpansion
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz hoop_stress'
use_automatic_differentiation = true
[]
[]
[AuxVariables]
[creep_rate_aux]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[scale_thickness]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfract_total]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfgain_total]
order = CONSTANT
family = MONOMIAL
[]
[burst_stress]
order = CONSTANT
family = MONOMIAL
[]
[burst]
order = CONSTANT
family = MONOMIAL
[]
[]
[Kernels]
[heat]
type = ADHeatConduction
variable = temperature
[]
[heat_ie]
type = ADHeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate_aux]
type = ADMaterialRealAux
variable = creep_rate_aux
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = ADMaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[scl_thickness]
type = ADMaterialRealAux
variable = scale_thickness
property = oxide_scale_thickness
boundary = 2
[]
[ofract_total]
type = ADMaterialRealAux
variable = oxywtfract_total
property = current_oxygen_weight_frac_total
boundary = 2
[]
[ofgain_total]
type = ADMaterialRealAux
boundary = 2
variable = oxywtfgain_total
property = oxygen_weight_frac_gained_total
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = 2
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = 2
execute_on = timestep_end
[]
[]
[BCs]
[inner_temperature]
type = REBEKADirichletBC
variable = temperature
function_tempm = temperature_func
minimum_temperature = 573.
translation = 0.1625
boundary = 4
[]
[no_y_midsection]
type = ADDirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply steam pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 101 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[CoolantChannel]
[convective_clad_surface]
boundary = 2
variable = temperature
inlet_temperature = 473.
inlet_pressure = 1.e+05
inlet_massflux = 1.0 # kg/m^2-sec # almost stagnant steam
rod_diameter = 10.75e-03
rod_pitch = 1.26e-02 # default
oxide_thickness = scale_thickness
number_axial_zone = 15
use_ad = true
[]
[]
[Materials]
[converter]
type = MaterialADConverter
reg_props_in = 'fract_beta_phase'
ad_props_out = 'ad_fract_beta_phase'
[]
[thermal]
type = ADZryThermal
block = cladding
temperature = temperature
[]
[clad_elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
block = cladding
youngs_modulus = 1.0e11
poissons_ratio = 0.3
[]
[clad_stress]
type = ADComputeMultipleInelasticStress
inelastic_models = 'clad_zrycreep'
block = cladding
[]
[hill_constants]
type = ADHillConstants
hill_constants = "0.738 0.174 0.588 1.0 1.0 1.0"
function_names = "F G H L M N"
temperature = temperature
[]
[clad_zrycreep]
type = ADZryAnisoCreepLOCAUpdate
block = cladding
temperature = temperature
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
temperature_loca_creep_begin = 501
temperature_standard_thermal_creep_end = 500
fract_beta_phase_name = 'ad_fract_beta_phase'
[]
[thermal_expansion]
type = ADZryThermalExpansionMATPROEigenstrain
block = cladding
temperature = temperature
stress_free_temperature = 573.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[density]
type = ADDensity
block = cladding
[]
[phase]
type = ZrPhase
block = cladding
temperature = temperature
numerical_method = 2
[]
[oxidation]
type = ADZryOxidation
boundary = 2
temperature = temperature
clad_inner_radius = 0.00465
clad_outer_radius = 0.005375
normal_operating_temperature_model = epri_kwu_ce
high_temperature_model = leistikow
use_coolant_channel = true
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = 2
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate_aux
temperature = temperature
fraction_beta_phase = fract_beta_phase
fraction_oxygen_gain = oxywtfgain_total
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-06
nl_abs_tol = 1.e-08
start_time = 0
n_startup_steps = 1
end_time = 700.
dtmax = 1.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[Postprocessors]
[ave_clad_exterior_temp]
type = SideAverageValue
boundary = 2
variable = temperature
[]
[max_clad_temp]
type = NodalExtremeValue
block = cladding
value_type = max
variable = temperature
[]
[min_clad_temp]
type = NodalExtremeValue
block = cladding
value_type = min
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = cladding
[]
[max_oxygen_fract]
type = ElementExtremeValue
block = cladding
value_type = max
variable = oxywtfract_total
[]
[max_betaph_fract]
type = ElementExtremeValue
block = cladding
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
block = cladding
value_type = max
variable = creep_rate_aux
[]
[max_creep_strain_mag]
type = ElementExtremeValue
block = cladding
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
block = cladding
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
block = cladding
value_type = max
variable = hoop_stress
[]
[vonmises_stress_clad]
type = ElementAverageValue
block = cladding
variable = vonmises_stress
[]
[min_burst_stress]
type = ElementExtremeValue
block = cladding
value_type = min
variable = burst_stress
[]
[burst]
type = ElementExtremeValue
block = cladding
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = cladding
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[top_disp_r_clad] # this is mid height
type = NodalVariableValue
variable = disp_x
nodeid = 0 #coords (0.005375, 0.1625)
[]
[top_disp_r_clad_slice] # this is mid height matched to the 1.5d
type = NodalVariableValue
variable = disp_x
nodeid = 3 #coords (0.005375, 0.1625)
[]
[top_disp_z_clad]
type = NodalVariableValue
variable = disp_y
nodeid = 0 #coords (0.005375, 0.1625)
[]
[stress_xx] # stess in the top Element
type = ElementalVariableValue
variable = stress_xx
elementid = 0
[]
[stress_yy] # stess in the top Element
type = ElementalVariableValue
variable = stress_yy
elementid = 0
[]
[stress_zz] # stess in the top Element
type = ElementalVariableValue
variable = stress_zz
elementid = 0
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = cladding
plenum_boundary_name = 4
external_clad_boundary_name = 2
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = rebeka_2d_12MPa_aniso_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
(assessment/LWR/validation/LOCA_REBEKA_cladding_burst_tests/analysis/rebeka_2d_10MPa/rebeka_singlerod_2d_10MPa_1pt5_aniso.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
order = SECOND
family = LAGRANGE
volumetric_locking_correction = false
displacements = 'disp_x'
[]
[Mesh]
coord_type = RZ
[layered1D_mesh]
type = Layered1DMeshGenerator
clad_mesh_density = customize
include_fuel = false
include_clad = true
include_plenum = false
pellet_outer_radius = 0.00465
clad_gap_width = 0
clad_thickness = 0.000725
fuel_height = 0.1625
slices_per_block = 10
pellet_bottom_coor = 0.0
nx_c = 1
[]
patch_update_strategy = auto
partitioner = centroid
centroid_partitioner_direction = y
[]
[UserObjects]
[pin_geometry]
type = Layered1DFuelPinGeometry
include_fuel = false
mesh_generator = layered1D_mesh
[]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[]
[Variables]
[temperature]
initial_condition = 573.0
[]
[]
[Functions]
[temperature_func]
type = PiecewiseLinear
x = '0. 700. '
y = '573. 1273.' # From 300 to 1000 C at 1 K/s
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 700. '
y = '1.e+07 1.e+07' # 100 bar
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 700. '
y = '1.e+05 1.e+05' # atmospheric pressure
[]
[clad_axial_pressure]
type = CladdingAxialPressureFunction
plenum_pressure = inner_pressure_func
coolant_pressure = outer_pressure_func
coolant_pressure_scaling_factor = 1
fuel_pin_geometry = pin_geometry
[]
# Circumferential steady-state creep test and analysis of Zircaloy-4 fuelcladding
# Nuclear Engineering and Design, 53, 2312-2322 (2021)
[F]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.738 0.57 0.57'
[]
[G]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.174 0.45 0.45'
[]
[H]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.588 0.48 0.48'
[]
[L]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[M]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[N]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[]
[Physics/SolidMechanics/Layered1D]
[clad]
block = clad
add_variables = true
strain = FINITE
add_scalar_variables = true
out_of_plane_strain_name = strain_yy
fuel_pin_geometry = pin_geometry
out_of_plane_pressure_function = clad_axial_pressure
decomposition_method = TaylorExpansion
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
eigenstrain_names = 'clad_thermal_eigenstrain'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz
creep_strain_xx creep_strain_yy creep_strain_xy creep_strain_zz strain_xx
strain_yy strain_zz hoop_stress'
group_scalar_vars_in_reference_residual = false
mesh_generator = layered1D_mesh
use_automatic_differentiation = true
[]
[]
[AuxVariables]
[disp_y] ## Required for easier visualization in Paraview
[]
[disp_z] ## Required for easier visualization in Paraview
[]
[creep_rate_aux]
order = CONSTANT
family = MONOMIAL
[]
[effective_creep_strain]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[scale_thickness]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfract_total]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfgain_total]
order = CONSTANT
family = MONOMIAL
[]
[burst_stress]
order = CONSTANT
family = MONOMIAL
[]
[burst]
order = CONSTANT
family = MONOMIAL
[]
[]
[Kernels]
[heat]
type = ADHeatConduction
variable = temperature
[]
[heat_ie]
type = ADHeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate_aux]
type = ADMaterialRealAux
variable = creep_rate_aux
property = creep_rate
execute_on = timestep_end
[]
[effective_creep_strain]
type = ADMaterialRealAux
property = effective_creep_strain
variable = effective_creep_strain
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[scl_thickness]
type = ADMaterialRealAux
variable = scale_thickness
property = oxide_scale_thickness
boundary = 2
[]
[ofract_total]
type = ADMaterialRealAux
variable = oxywtfract_total
property = current_oxygen_weight_frac_total
boundary = 2
[]
[ofgain_total]
type = ADMaterialRealAux
boundary = 2
variable = oxywtfgain_total
property = oxygen_weight_frac_gained_total
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = 2
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = 2
execute_on = timestep_end
[]
[]
[BCs]
# [inner_temperature]
# type = REBEKADirichletBC
# variable = temperature
# function_tempm = temperature_func
# minimum_temperature = 573.0
# translation = 0.1625
# boundary = 5
# []
[Pressure]
[outer_pressure] # apply steam pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 5
function = inner_pressure_func
[]
[]
[]
# [CoolantChannel]
# [convective_clad_surface]
# boundary = 2
# variable = temperature
# inlet_temperature = 473.
# inlet_pressure = 1.e+05
# inlet_massflux = 1. # kg/m^2-sec # almost stagnant steam
# rod_diameter = 10.75e-03
# rod_pitch = 1.26e-02 # default
# oxide_thickness = scale_thickness
# []
# []
[Materials]
[converter]
type = MaterialADConverter
reg_props_in = 'fract_beta_phase'
ad_props_out = 'ad_fract_beta_phase'
[]
[thermal]
type = ADZryThermal
block = clad
temperature = temperature
[]
[clad_elasticity_tensor]
type = ADZryElasticityTensor
block = clad
matpro_youngs_modulus = false
matpro_poissons_ratio = false
[]
[clad_stress]
type = ADComputeMultipleInelasticStress
inelastic_models = 'clad_zrycreep'
block = clad
[]
[hill_constants]
type = ADHillConstants
hill_constants = "0.738 0.174 0.588 1.0 1.0 1.0"
function_names = "F G H L M N"
temperature = temperature
[]
[clad_zrycreep]
type = ADZryAnisoCreepLOCAUpdate
block = clad
temperature = temperature
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
temperature_loca_creep_begin = 501
temperature_standard_thermal_creep_end = 500
fract_beta_phase_name = 'ad_fract_beta_phase'
[]
[thermal_expansion]
type = ADZryThermalExpansionMATPROEigenstrain
block = clad
temperature = temperature
stress_free_temperature = 573.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[density]
type = ADDensity
block = clad
[]
[phase]
type = ZrPhase
block = clad
temperature = temperature
numerical_method = 2
[]
[oxidation]
type = ADZryOxidation
boundary = 2
temperature = temperature
clad_inner_radius = 0.00465
clad_outer_radius = 0.005375
normal_operating_temperature_model = epri_kwu_ce
high_temperature_model = leistikow
# use_coolant_channel = true
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = 2
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate_aux
temperature = temperature
fraction_beta_phase = 'ad_fract_beta_phase'
fraction_oxygen_gain = oxywtfgain_total
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-06
nl_abs_tol = 1.e-08
start_time = 0
n_startup_steps = 1
end_time = 700.
dtmax = 1.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[Postprocessors]
[ave_clad_exterior_temp]
type = LayeredSideAverageValuePostprocessor
boundary = 2
variable = temperature
fuel_pin_geometry = pin_geometry
[]
[max_clad_temp]
type = NodalExtremeValue
block = clad
value_type = max
variable = temperature
[]
[min_clad_temp]
type = NodalExtremeValue
block = clad
value_type = min
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = clad
[]
[max_oxygen_fract]
type = ElementExtremeValue
block = clad
value_type = max
variable = oxywtfract_total
[]
[max_betaph_fract]
type = ElementExtremeValue
block = clad
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
block = clad
value_type = max
variable = creep_rate_aux
[]
[max_eff_creep_strain]
type = ElementExtremeValue
block = clad
value_type = max
variable = effective_creep_strain
[]
[max_hoop_strain]
type = ElementExtremeValue
block = clad
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
block = clad
value_type = max
variable = hoop_stress
[]
[vonmises_stress_clad]
type = ElementAverageValue
block = clad
variable = vonmises_stress
[]
[min_burst_stress]
type = ElementExtremeValue
block = clad
value_type = min
variable = burst_stress
[]
[burst]
type = ElementExtremeValue
block = clad
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = clad
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = pin_geometry
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[top_disp_r_clad_slice] # this is mid height
type = NodalVariableValue
variable = disp_x
nodeid = 28 # 1 line element
[]
[inner_pressure_func]
type = FunctionValuePostprocessor
function = inner_pressure_func
execute_on = 'initial linear'
[]
[stress_xx] # stess in the top Element
type = ElementalVariableValue
variable = stress_xx
elementid = 9 #single line element
[]
[stress_yy] # stess in the top Element
type = ElementalVariableValue
variable = stress_yy
elementid = 9 #single line element
[]
[stress_zz] # stess in the top Element
type = ElementalVariableValue
variable = stress_zz
elementid = 9 #single line element
[]
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = rebeka_2d_10MPa_1pt5_out_chkfile
show = 'ave_clad_exterior_temp max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/LOCA_IFA_650/analysis/IFA_650_4/IFA_650_4_part2.i)
[GlobalParams]
density = 10452.96
initial_porosity = 0.048
order = SECOND
family = LAGRANGE
displacements = disp_x
temperature = temperature
energy_per_fission = 3.2e-11 #J/fission
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
acceptable_multiplier = 10
restart_file_base = 'IFA_650_4_part1_checkpoint_cp/LATEST'
[]
[Mesh]
coord_type = RZ
[layered1D_mesh]
type = Layered1DMeshGenerator
slices_per_block = 30
pellet_outer_radius = 4.565e-3
clad_gap_width = 0.085e-3
clad_thickness = 0.725e-3
fuel_height = 0.480
plenum_height = 0.291185
pellet_mesh_density = customize
clad_mesh_density = customize
nx_p = 11
nx_c = 5
[]
patch_update_strategy = auto
partitioner = centroid
centroid_partitioner_direction = y
[]
[Variables]
[disp_x]
[]
[temperature]
[]
[]
[Functions]
[power_history]
type = PiecewiseLinear
data_file = power_history.csv
scale_factor = 1.0
format = columns
[]
[axial_peaking_factors]
type = PiecewiseBilinear
data_file = axial_peaking_factors.csv
axis = 1
scale_factor = 1
[]
[pressure_ramp]
type = PiecewiseLinear
data_file = coolant_pressure.csv
scale_factor = 1
format = columns
[]
[average_htc]
type = PiecewiseLinear
data_file = average_coolant_htc.csv
format = columns
scale_factor = 1
[]
[forced_times]
type = PiecewiseLinear
data_file = timestep_limiting.csv
scale_factor = 1
format = columns
[]
[heat_sink_temperature]
type = PiecewiseBilinear
data_file = heater_temp.csv
scale_factor = 1
axis = 1
[]
[clad_outer_temperature]
type = PiecewiseBilinear
data_file = clad_surface_temp.csv
scale_factor = 1
axis = 1
[]
[heat_transfer_mode]
type = PiecewiseConstant
x = '-200 172489073 172489661'
y = '9 9 8 '
direction = 'right'
[]
[clad_axial_pressure]
type = CladdingAxialPressureFunction
plenum_pressure = plenum_pressure
coolant_pressure = pressure_ramp
coolant_pressure_scaling_factor = 1.0
fuel_pin_geometry = fuel_pin_geometry
[]
[fuel_axial_pressure]
type = ParsedFunction
expression = plenum_pressure
symbol_names = plenum_pressure
symbol_values = plenum_pressure
[]
[]
[AuxVariables]
[disp_y]
[]
[disp_z]
[]
[fast_neutron_flux]
block = clad
[]
[fast_neutron_fluence]
block = clad
[]
[grain_radius]
block = fuel
[]
[hoop_stress]
order = CONSTANT
family = MONOMIAL
[]
[effective_creep_strain]
block = clad
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[oxide_thickness]
order = CONSTANT
family = MONOMIAL
[]
[burst]
order = CONSTANT
family = MONOMIAL
[]
[gap_conductance]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[layered_maximum_clad_radius]
order = CONSTANT
family = MONOMIAL
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
extra_vector_tags = 'ref'
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
extra_vector_tags = 'ref'
[]
[heat_source]
type = NeutronHeatSource
variable = temperature
block = fuel
burnup_function = burnup
axial_relocation_object = axial_relocation
extra_vector_tags = 'ref'
[]
[]
[Physics]
[SolidMechanics]
[Layered1D]
[fuel]
add_scalar_variables = true
out_of_plane_strain_name = strain_yy
fuel_pin_geometry = fuel_pin_geometry
out_of_plane_pressure_function = fuel_axial_pressure
strain = finite
block = fuel
eigenstrain_names = 'fuel_thermal_strain fuel_swelling_strain fuel_relocation_strain axial_relocation_eigenstrain'
decomposition_method = EigenSolution
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress'
extra_vector_tags = 'ref'
group_scalar_vars_in_reference_residual = true
mesh_generator = layered1D_mesh
[]
[clad]
add_scalar_variables = true
out_of_plane_strain_name = strain_yy
fuel_pin_geometry = fuel_pin_geometry
strain = finite
out_of_plane_pressure_function = clad_axial_pressure
block = clad
eigenstrain_names = 'clad_thermal_strain clad_irradiation_strain'
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress strain_zz creep_strain_zz'
decomposition_method = EigenSolution
extra_vector_tags = 'ref'
group_scalar_vars_in_reference_residual = true
mesh_generator = layered1D_mesh
[]
[]
[]
[]
[Burnup]
[burnup]
block = fuel
rod_ave_lin_pow = power_history
axial_power_profile = axial_peaking_factors
num_radial = 80
num_axial = 11
fuel_pin_geometry = fuel_pin_geometry
fuel_volume_ratio = 1.0
order = CONSTANT
family = MONOMIAL
RPF = RPF
isotopes = 'U235 U238 Pu239 Pu240 Pu241 Pu242'
isotope_fractions = '0.035 0.965 0 0 0 0'
[]
[]
[AuxKernels]
[fast_neutron_flux]
type = FastNeutronFluxAux
block = clad
variable = fast_neutron_flux
rod_ave_lin_pow = power_history
axial_power_profile = axial_peaking_factors
factor = 3e13
execute_on = timestep_begin
[]
[fast_neutron_fluence]
type = FastNeutronFluenceAux
block = clad
variable = fast_neutron_fluence
fast_neutron_flux = fast_neutron_flux
execute_on = timestep_begin
[]
[grain_radius]
type = GrainRadiusAux
block = fuel
variable = grain_radius
temperature = temperature
execute_on = linear
[]
[hoop_stress]
type = RankTwoScalarAux
rank_two_tensor = stress
variable = hoop_stress
scalar_type = HoopStress
execute_on = timestep_end
[]
[effective_creep_strain]
type = MaterialRealAux
block = clad
variable = effective_creep_strain
property = effective_creep_strain
execute_on = 'timestep_end'
[]
[fract_bphase]
type = MaterialRealAux
block = clad
variable = fract_beta_phase
property = fract_beta_phase
execute_on = 'initial linear'
[]
[oxide_thickness]
type = MaterialRealAux
boundary = 2
variable = oxide_thickness
property = oxide_scale_thickness
execute_on = 'initial linear'
[]
[hasburst]
type = MaterialRealAux
boundary = 2
variable = burst
property = failed
execute_on = timestep_end
[]
[conductance]
type = MaterialRealAux
boundary = 10
property = gap_conductance
variable = gap_conductance
execute_on = 'initial linear'
[]
[coolant_htc]
type = MaterialRealAux
property = coolant_channel_htc
variable = coolant_htc
boundary = 2
execute_on = 'initial linear'
[]
[creep_rate]
type = MaterialRealAux
block = clad
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[]
[AxialRelocation]
[fuel_relo]
mesh_generator = layered1D_mesh
rod_ave_lin_pow = power_history
axial_direction = y
fuel_blocks = fuel
clad_blocks = clad
contact_pressure_variable = contact_pressure
out_of_plane_strain_variable = strain_yy
penetration_variable = penetration
clad_inner_volume_addition = 3.17755E-06 # Addition of the volume to bring the starting total volume to 21.5cm^3 to begin the transient experiment
burnup_variable = burnup
temperature = temperature
axial_relocation_output_options = MASS_FRACTION
[]
[]
[CoolantChannel]
[convective_clad_surface] # apply convective boundary to clad outer surface
boundary = 2
variable = temperature
heat_transfer_mode = heat_transfer_mode
heat_transfer_coefficient = average_htc # Calculated from an initial simulation of the base irradiation using the inlet_pressure, inlet_massflux, and inlet_temperature commented out below.
inlet_temperature = heat_sink_temperature # K
effective_emissivity = 0.75
# inlet_temperature = 580
# inlet_pressure = 15.3e6 # Pa
# inlet_massflux = 3800 # kg/m^2-sec
rod_diameter = 0.01075 # m
rod_pitch = 1.26e-2 # m
compute_enthalpy = false
linear_heat_rate = power_history
axial_power_profile = axial_peaking_factors
output_properties = 'coolant_channel_htype coolant_channel_hmode'
[]
[]
[Contact]
[pellet_clad_mechanical]
primary = 5
secondary = 10
penalty = 1e7
formulation = kinematic
model = frictionless
[]
[]
[ThermalContact]
[thermal_contact]
type = GasGapHeatTransfer
variable = temperature
primary = 5
secondary = 10
initial_gas_types = 'He Ar'
initial_fractions = '0.05 0.95'
initial_moles = initial_moles
gas_released = fis_gas_released
plenum_pressure = plenum_pressure
contact_pressure = contact_pressure
jump_distance_model = LANNING
roughness_coef = 3.2
refab_gas_types = 'He Ar'
refab_fractions = '0.05 0.95'
refab_time = 172387800
refab_type = 0
[]
[]
[BCs]
[no_x_all]
type = DirichletBC
variable = disp_x
boundary = 12
value = 0.0
[]
[Pressure]
[coolantPressure]
boundary = 2
function = pressure_ramp
factor = 1.0
[]
[]
[clad_outer_temp]
type = FunctionDirichletBC
boundary = 2
variable = temperature
function = clad_outer_temperature
[]
[PlenumPressure]
[plenumPressure]
boundary = 9
initial_pressure = 2.0e6
startup_time = 0
R = 8.3143
output_initial_moles = initial_moles
temperature = plenum_temp
volume = 'clad_volume pellet_volume'
material_input = fis_gas_released
output = plenum_pressure
refab_time = 172387800
refab_pressure = 4.0e6
refab_temperature = 295.0
refab_volume = 2.15e-05
[]
[]
[]
[LayeredPlenumTemperature]
[plenum_temp]
boundary = 5
fuel_pin_geometry = fuel_pin_geometry
out_of_plane_strain = strain_yy
inner_surfaces = '5'
outer_surfaces = '10'
temperature = temperature
[]
[]
[Controls]
[period1]
type = TimePeriod
disable_objects = 'BCs/clad_outer_temp'
start_time = 172489043
end_time = 172489661
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
execute_on = timestep_end
[]
[]
[Materials]
[fuel_thermal]
type = UO2Thermal
block = fuel
thermal_conductivity_model = STAICU
hbs_porosity_correction = KAMPF
model_hbs_formation = true
temperature = temperature
burnup_function = burnup
axial_relocation_object = axial_relocation
gap_thermal_conductivity = layered_average_gap_conductivity
[]
[relocation]
type = UO2RelocationEigenstrain
block = fuel
burnup_function = burnup
rod_ave_lin_pow = power_history
axial_power_profile = axial_peaking_factors
fuel_pin_geometry = fuel_pin_geometry
burnup_relocation_stop = 0.024
relocation_activation1 = 5000.0
relocation_model = ESCORE_modified
eigenstrain_name = fuel_relocation_strain
[]
[fuel_thermal_strain]
type = ComputeThermalExpansionEigenstrain
block = fuel
thermal_expansion_coeff = 10.0e-6
stress_free_temperature = 295.0
eigenstrain_name = fuel_thermal_strain
[]
[fuel_swelling]
type = UO2VolumetricSwellingEigenstrain
gas_swelling_model_type = SIFGRS
block = fuel
burnup_function = burnup
initial_fuel_density = 10452.96
eigenstrain_name = fuel_swelling_strain
[]
[fission_gas_release]
type = UO2Sifgrs
block = fuel
temperature = temperature
burnup_function = burnup
grain_radius = grain_radius
transient_option = MICROCRACKING_BURNUP
diff_coeff_option = TURNBULL_D1_D2
gbs_model = true
[]
[fuel_elasticity_tensor]
type = UO2IsotropicDamageElasticityTensor
block = fuel
fragmentation_model = BARANI
temperature = temperature
rod_ave_lin_pow = power_history
# axial_relocation_object = axial_relocation
crumbling_scale_factor = 0.0001
[]
[fuel_stress]
type = ComputeMultipleInelasticStress
tangent_operator = elastic
inelastic_models = 'fuel_creep'
block = fuel
[]
[fuel_creep]
type = UO2CreepUpdate
block = fuel
temperature = temperature
burnup_function = burnup
initial_grain_radius = 5.0e-6
[]
[HBS]
type = HighBurnupStructureFormation
block = fuel
burnup_function = burnup
temperature = temperature
output_properties = 'hbs_volume_fraction'
outputs = 'exodus'
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = clad
[]
[stress]
type = ComputeMultipleInelasticStress
tangent_operator = elastic
inelastic_models = 'zrycreep'
block = clad
[]
[zrycreep]
type = ZryCreepLOCAUpdate
fast_neutron_flux = fast_neutron_flux
fast_neutron_fluence = fast_neutron_fluence
model_irradiation_creep = true
model_primary_creep = true
model_thermal_creep = true
max_inelastic_increment = 5e-4
zircaloy_material_type = stress_relief_annealed
block = clad
[]
[thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = clad
stress_free_temperature = 295.0
eigenstrain_name = clad_thermal_strain
[]
[irradiation_swelling]
type = ZryIrradiationGrowthEigenstrain
block = clad
fast_neutron_fluence = fast_neutron_fluence
zircaloy_material_type = stress_relief_annealed
eigenstrain_name = clad_irradiation_strain
[]
[clad_phase]
type = ZrPhase
block = clad
temperature = temperature
numerical_method = 2
[]
[clad_oxidation]
type = ZryOxidation
boundary = 2
temperature = temperature
clad_inner_radius = 4.65e-03
clad_outer_radius = 5.375e-03
normal_operating_temperature_model = epri_kwu_ce
high_temperature_model = cathcart
use_coolant_channel = true
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = 2
failure_criterion = plastic_instability
hoop_stress = hoop_stress
# hoop_creep_strain = creep_strain_zz
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[clad_thermal]
type = ZryThermal
block = clad
temperature = temperature
[]
[fuel_density]
type = Density
block = fuel
[]
[clad_density]
type = Density
block = clad
density = 6551.0
[]
[]
[Postprocessors]
[ave_temp_interior]
type = LayeredSideAverageValuePostprocessor
boundary = 9
variable = temperature
execute_on = 'initial linear'
fuel_pin_geometry = fuel_pin_geometry
[]
[pellet_volume_2]
type = LayeredInternalVolumePostprocessor
boundary = 8
component = 0
fuel_pin_geometry = fuel_pin_geometry
out_of_plane_strain = strain_yy
execute_on = 'initial linear'
[]
[avg_clad_temp]
type = LayeredSideAverageValuePostprocessor
boundary = 7
variable = temperature
fuel_pin_geometry = fuel_pin_geometry
execute_on = 'initial linear'
[]
[fis_gas_produced]
type = LayeredElementIntegralFisGasGeneratedSifgrsPostprocessor
block = fuel
fuel_pin_geometry = fuel_pin_geometry
[]
[fis_gas_released]
type = LayeredElementIntegralFisGasReleasedSifgrsPostprocessor
block = fuel
fuel_pin_geometry = fuel_pin_geometry
[]
[fis_gas_grain]
type = LayeredElementIntegralFisGasGrainSifgrsPostprocessor
block = fuel
outputs = exodus
fuel_pin_geometry = fuel_pin_geometry
[]
[fis_gas_boundary]
type = LayeredElementIntegralFisGasBoundarySifgrsPostprocessor
block = fuel
outputs = exodus
fuel_pin_geometry = fuel_pin_geometry
[]
[fission_gas_release]
type = FGRPercent
fission_gas_released = fis_gas_released
fission_gas_generated = fis_gas_produced
[]
[average_coolant_htc]
type = LayeredSideAverageValuePostprocessor
boundary = 2
variable = coolant_htc
execute_on = 'initial linear'
fuel_pin_geometry = fuel_pin_geometry
[]
[average_burnup]
type = RodAverageBurnup
burnup_function = burnup
[]
[temp_clad_max]
type = NodalExtremeValue
block = clad
value_type = max
variable = temperature
execute_on = 'initial timestep_end'
[]
[betaph_fract_max]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
block = clad
execute_on = 'initial timestep_end'
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
block = clad
execute_on = 'initial timestep_end'
[]
[timestep_material]
type = MaterialTimeStepPostprocessor
block = clad
execute_on = 'initial timestep_end'
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = clad
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geometry
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[Dampers]
[limitT]
type = BoundingValueNodalDamper
variable = temperature
max_value = 3200.0
min_value = 0.0
[]
[limitX]
type = MaxIncrement
max_increment = 1e-5
variable = disp_x
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package -ksp_gmres_restart'
petsc_options_value = 'lu superlu_dist 51'
line_search = 'none'
l_max_its = 50
l_tol = 1e-3
nl_max_its = 100
nl_rel_tol = 1e-4
nl_abs_tol = 1e-8
dtmax = 5e5
dtmin = 1e-5
# end_time = 172387800 # End base irradiation
# end_time = 172489043 # Begin Blowdown
end_time = 172489661 # End
[TimeStepper]
type = IterationAdaptiveDT
dt = 200
timestep_limiting_postprocessor = timestep_material
optimal_iterations = 20
iteration_window = 4
linear_iteration_ratio = 100
timestep_limiting_function = forced_times
force_step_every_function_point = true
max_function_change = 2000
time_t = '172387800 172388043 172488043 172489043 172489073 172489661'
time_dt = '1.0e04 1.0e04 10.0 5.0 3.0 5.0'
[]
[]
[VectorPostprocessors]
[clad_radial_disp]
type = NodalValueSampler
variable = disp_x
boundary = 2
sort_by = y
outputs = 'outfile_2'
[]
[clad_out_temp]
type = NodalValueSampler
variable = temperature
boundary = 2
sort_by = y
outputs = 'outfile_temp_2'
[]
[mass_fraction]
type = LineValueSampler
start_point = '0 0.01124 0'
end_point = '0 0.47524 0'
num_points = 30
sort_by = y
variable = layered_mass_fraction
outputs = 'outfile_mass_2'
[]
[]
[PerformanceMetricOutputs]
[]
[Outputs]
csv = true
color = false
exodus = true
execute_on = 'initial timestep_end'
perf_graph = true
[outfile_2]
type = CSV
execute_on = 'FINAL'
create_final_symlink = true
[]
[outfile_temp_2]
type = CSV
execute_on = 'FINAL'
create_final_symlink = true
[]
[outfile_mass_2]
type = CSV
execute_on = 'FINAL'
create_final_symlink = true
[]
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-26/puzry-26.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-26.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 2000. '
y = '1.e+05 1.e+05 1.203e+07' # Linear increase at 0.1193 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 2000. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = EigenSolution
[]
[]
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = MaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = FunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = DirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = DirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1.e+11
poissons_ratio = 0.3
block = 1
[]
[creep_update]
type = ZryCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 1.e-04
temperature = temperature
temperature_standard_thermal_creep_end = 700
temperature_loca_creep_begin = 900.
[]
[creep]
type = ComputeMultipleInelasticStress
block = 1
tangent_operator = elastic
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = Density
block = 1
[]
[phase]
type = ZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
active = 'smp'
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0.
n_startup_steps = 1
end_time = 2000.
dtmax = 1.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-26_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/RIA_CABRI_REP_Na/analysis/REP_Na_2/REP_Na_2_1pt5.i)
# REP Na 2 Base Irradiation
[GlobalParams]
displacements = disp_x
temperature = temp
order = SECOND
family = LAGRANGE
energy_per_fission = 3.2e-11 # J/fission
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
acceptable_iterations = 30
acceptable_multiplier = 10
[]
[Mesh]
coord_type = RZ
[layered1D_mesh]
type = Layered1DMeshGenerator
clad_thickness = 0.000637
pellet_outer_radius = 0.0040248
fuel_height = 1.00706
plenum_height = 0.044077
clad_gap_width = 93.0e-6
pellet_bottom_coor = 0.0045
slices_per_block = 10
[]
patch_update_strategy = auto
partitioner = centroid
centroid_partitioner_direction = y
[]
[UserObjects]
[pin_geometry]
type = Layered1DFuelPinGeometry
mesh_generator = layered1D_mesh
[]
[]
[Variables]
[temp]
initial_condition = 293.15
[]
[]
[AuxVariables]
[fast_neutron_flux]
block = clad
[]
[fast_neutron_fluence]
block = clad
[]
[grain_radius]
block = fuel
initial_condition = 5.0e-6
[]
[gap_cond]
order = CONSTANT
family = MONOMIAL
[]
[fuel_cond]
order = CONSTANT
family = MONOMIAL
[]
[swelling_strain]
order = CONSTANT
family = MONOMIAL
block = fuel
[]
[hoop_creep_strain]
order = CONSTANT
family = MONOMIAL
[]
[axial_creep_strain]
order = CONSTANT
family = MONOMIAL
[]
[hoop_plastic_strain]
order = CONSTANT
family = MONOMIAL
[]
[axial_plastic_strain]
order = CONSTANT
family = MONOMIAL
[]
[total_hoop_strain]
order = CONSTANT
family = MONOMIAL
[]
[total_axial_strain]
order = CONSTANT
family = MONOMIAL
[]
[hoop_elastic_strain]
order = CONSTANT
family = MONOMIAL
[]
[axial_elastic_strain]
order = CONSTANT
family = MONOMIAL
[]
[clad_coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[coolant_temp]
order = CONSTANT
family = MONOMIAL
[]
[clad_coolant_flux]
order = CONSTANT
family = MONOMIAL
[]
[coolant_channel_hmode]
order = CONSTANT
family = MONOMIAL
[]
[coolant_channel_htype]
order = CONSTANT
family = MONOMIAL
[]
[critical_heat_flux]
order = CONSTANT
family = MONOMIAL
[]
[oxide_thickness]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfract_total]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfgain_total]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[]
[Functions]
[power_profile]
type = PiecewiseLinear # reads and interpolates an input file containing rod average linear power vs time
data_file = REPNa2_power_history_Full.csv
format = columns
[]
[axial_peaking_factors] # reads and interpolates an input file containing the axial power profile vs time
type = PiecewiseBilinear
data_file = REPNa2_axial_peaking_Full.csv
axis = 1
[]
[pressure_ramp] # inlet coolant pressure evolution
type = PiecewiseLinear
xy_data = '0 101325
8640 13999808
57067200 13999808
57110400 101325
57542410 101325
57542450 500008
57542700 500008
57542800 101325
57542900 101325'
[]
[temp_ramp] # inlet coolant temp evolution
type = PiecewiseLinear
xy_data = '0 293.15
8640 543.15
57067200 543.15
57110400 293.15
57542410 293.15
57542450 553.15
57542700 553.15
57542800 293.15
57542900 293.15'
[]
[Fuel_CTE_function] #Fuel CTE as a function of temp from MATPRO data
type = PiecewiseLinear
xy_data = ' 0 1.000E-05
300 1.000E-05
350 1.000E-05
400 1.000E-05
450 1.000E-05
500 1.001E-05
550 1.002E-05
600 1.003E-05
650 1.005E-05
700 1.008E-05
750 1.011E-05
800 1.015E-05
850 1.020E-05
900 1.026E-05
950 1.032E-05
1000 1.039E-05
1050 1.046E-05
1100 1.053E-05
1150 1.061E-05
1200 1.069E-05
1250 1.077E-05
1300 1.085E-05
1350 1.094E-05
1400 1.102E-05
1450 1.111E-05
1500 1.119E-05
1550 1.127E-05
1600 1.135E-05
1650 1.143E-05
1700 1.151E-05
1750 1.158E-05
1800 1.166E-05
1850 1.173E-05
1900 1.180E-05
1950 1.187E-05
2000 1.193E-05
2050 1.199E-05
2100 1.205E-05
2150 1.211E-05
2200 1.217E-05
2250 1.222E-05
2300 1.227E-05
2350 1.232E-05
2400 1.237E-05
2450 1.242E-05
2500 1.246E-05
2550 1.250E-05
2600 1.254E-05
2650 1.258E-05
2700 1.262E-05
2750 1.265E-05
2800 1.268E-05
2850 1.271E-05
2900 1.274E-05
2950 1.277E-05
3000 1.280E-05
3050 1.282E-05
3100 1.285E-05'
[]
[burnup_GWd]
type = ParsedFunction
expression = bu*950
symbol_names = 'bu'
symbol_values = 'average_burnup'
[]
[clad_axial_pressure]
type = CladdingAxialPressureFunction
plenum_pressure = plenum_pressure
coolant_pressure = pressure_ramp
fuel_pin_geometry = pin_geometry
[]
[fuel_axial_pressure]
type = ParsedFunction
expression = plenum_pressure
symbol_names = plenum_pressure
symbol_values = plenum_pressure
[]
[]
[Physics/SolidMechanics/Layered1D]
[pellets]
block = fuel
add_variables = true
add_scalar_variables = true
out_of_plane_strain_name = strain_yy
fuel_pin_geometry = pin_geometry
out_of_plane_pressure_function = fuel_axial_pressure
strain = FINITE
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
eigenstrain_names = 'fuel_relocation_strain fuel_thermal_strain
fuel_volumetric_strain'
generate_output = 'hoop_stress axial_stress vonmises_stress'
mesh_generator = layered1D_mesh
extra_vector_tags = 'ref'
group_scalar_vars_in_reference_residual = true
[]
[clad]
block = clad
add_variables = true
add_scalar_variables = true
out_of_plane_strain_name = strain_yy
fuel_pin_geometry = pin_geometry
out_of_plane_pressure_function = clad_axial_pressure
strain = FINITE
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
eigenstrain_names = 'clad_thermal_eigenstrain clad_irradiation_strain'
generate_output = 'hoop_stress axial_stress vonmises_stress'
mesh_generator = layered1D_mesh
extra_vector_tags = 'ref'
group_scalar_vars_in_reference_residual = true
[]
[]
[Kernels]
[heat] # gradient term in heat conduction equation
type = HeatConduction
variable = temp
extra_vector_tags = 'ref'
[]
[heat_ie] # time term in heat conduction equation
type = HeatConductionTimeDerivative
variable = temp
extra_vector_tags = 'ref'
[]
[heat_source_fuel] # source term in heat conduction equation
type = NeutronHeatSource
variable = temp
block = fuel
burnup_function = burnup
extra_vector_tags = 'ref'
[]
[]
[Burnup]
[burnup]
block = fuel
density = 10344.71
rod_ave_lin_pow = power_profile
axial_power_profile = axial_peaking_factors
num_radial = 80
num_axial = 85
a_upper = 1.0115592
a_lower = 0.0045
fuel_inner_radius = 0
fuel_outer_radius = 0.0040248
fuel_volume_ratio = 1
isotopes = 'U235 U238 Pu239 Pu240 Pu241 Pu242'
isotope_fractions = '0.0685 0.9315 0 0 0 0'
RPF = RPF
order = CONSTANT
family = MONOMIAL
[]
[]
[AuxKernels]
[fast_neutron_flux]
type = FastNeutronFluxAux
variable = fast_neutron_flux
axial_power_profile = axial_peaking_factors
rod_ave_lin_pow = power_profile
factor = 3e13 #n/m2-s
block = clad
execute_on = timestep_begin
[]
[fast_neutron_fluence]
type = FastNeutronFluenceAux
variable = fast_neutron_fluence
fast_neutron_flux = fast_neutron_flux
block = clad
execute_on = timestep_begin
[]
[grain_radius]
type = GrainRadiusAux
block = fuel
variable = grain_radius
temperature = temp
execute_on = linear
[]
[gap_conductance]
type = MaterialRealAux
property = gap_conductance
variable = gap_cond
boundary = 10
[]
[fuel_conductance]
type = MaterialRealAux
property = thermal_conductivity
variable = fuel_cond
block = fuel
[]
[swelling_strain]
type = MaterialRealAux
property = volumetric_swelling_strain
variable = swelling_strain
block = fuel
[]
[hoop_creep_strain]
type = RankTwoAux
rank_two_tensor = creep_strain
variable = hoop_creep_strain
index_i = 2
index_j = 2
execute_on = timestep_end
block = clad
[]
[axial_creep_strain]
type = RankTwoAux
rank_two_tensor = creep_strain
variable = axial_creep_strain
index_i = 1
index_j = 1
execute_on = timestep_end
block = clad
[]
[hoop_plastic_strain]
type = RankTwoAux
rank_two_tensor = plastic_strain
variable = hoop_plastic_strain
index_i = 2
index_j = 2
execute_on = timestep_end
block = clad
[]
[axial_plastic_strain]
type = RankTwoAux
rank_two_tensor = plastic_strain
variable = axial_plastic_strain
index_i = 1
index_j = 1
execute_on = timestep_end
block = clad
[]
[total_hoop_strain]
type = RankTwoAux
rank_two_tensor = total_strain
variable = total_hoop_strain
index_i = 2
index_j = 2
execute_on = timestep_end
block = clad
[]
[total_axial_strain]
type = RankTwoAux
rank_two_tensor = total_strain
variable = total_axial_strain
index_i = 1
index_j = 1
execute_on = timestep_end
block = clad
[]
[hoop_elastic_strain]
type = RankTwoAux
rank_two_tensor = elastic_strain
variable = hoop_elastic_strain
index_i = 2
index_j = 2
execute_on = timestep_end
block = clad
[]
[axial_elastic_strain]
type = RankTwoAux
rank_two_tensor = elastic_strain
variable = axial_elastic_strain
index_i = 1
index_j = 1
execute_on = timestep_end
block = clad
[]
[clad_coolant_htc]
type = MaterialRealAux
property = coolant_channel_htc
variable = clad_coolant_htc
boundary = 2
[]
[coolant_temp]
type = MaterialRealAux
property = coolant_temperature
variable = coolant_temp
boundary = 2
[]
[clad_coolant_flux]
type = MaterialRealAux
property = output_heat_flux
variable = clad_coolant_flux
boundary = 2
[]
[coolant_channel_hmode]
type = MaterialRealAux
property = coolant_channel_hmode
variable = coolant_channel_hmode
boundary = 2
[]
[coolant_channel_htype]
type = MaterialRealAux
property = coolant_channel_htype
variable = coolant_channel_htype
boundary = 2
[]
[critical_heat_flux]
type = MaterialRealAux
property = critical_heat_flux
variable = critical_heat_flux
boundary = 2
[]
[oxide]
type = MaterialRealAux
property = oxide_scale_thickness
variable = oxide_thickness
boundary = 2
[]
[ofract_total]
type = MaterialRealAux
property = current_oxygen_weight_frac_total
variable = oxywtfract_total
execute_on = timestep_end
boundary = 2
[]
[ofgain_total]
type = MaterialRealAux
property = oxygen_weight_frac_gained_total
variable = oxywtfgain_total
execute_on = timestep_end
boundary = 2
[]
[fract_bphase]
type = MaterialRealAux
property = fract_beta_phase
variable = fract_beta_phase
block = clad
[]
[]
[Contact]
[pellet_clad_mechanical]
primary = 5
secondary = 10
penalty = 1e14
formulation = penalty
normalize_penalty = true
model = frictionless
[]
[]
[ThermalContact]
[thermal_contact]
type = GasGapHeatTransfer
variable = temp
primary = 5
secondary = 10
initial_moles = initial_moles # coupling to a postprocessor which supplies the initial plenum/gap gas mass
gas_released = fis_gas_released # coupling to a postprocessor which supplies the fission gas addition
jump_distance_model = LANNING
plenum_pressure = plenum_pressure
contact_pressure = contact_pressure
roughness_primary = 2.0e-6
roughness_secondary = 0.5e-6
roughness_coef = 3.2
quadrature = true
emissivity_primary = 0.797698 #Emissivity for fuel
emissivity_secondary = 0.325 #Emissivity for clad
refab_time = 57456000
refab_gas_types = He
refab_fractions = 1
[]
[]
[BCs]
[no_x_all]
type = DirichletBC
variable = disp_x
boundary = 12
value = 0.0
[]
[Pressure]
[coolantPressure]
boundary = 2
function = pressure_ramp # use the pressure_ramp function defined above
[]
[]
[PlenumPressure]
[plenumPressure]
boundary = 9
initial_temperature = 293.15
initial_pressure = 1.70e6
startup_time = 0
R = 8.3143
output_initial_moles = initial_moles # coupling to post processor to get initial fill gas mass
temperature = ave_temp_interior #plenumTemp
volume = gas_volume # coupling to post processor to get gas volume
material_input = fis_gas_released # coupling to post processor to get fission gas added
output = plenum_pressure # coupling to post processor to output plenum/gap pressure
refab_time = 57456000
refab_pressure = 0.1e6
refab_temperature = 293.15
refab_volume = 2.3e-6
[]
[]
[]
[CoolantChannel]
[convective_clad_surface_water] # apply convective boundary to clad outer surface
boundary = 2
variable = temp
inlet_temperature = temp_ramp # K
inlet_pressure = pressure_ramp # Pa
inlet_massflux = 1779 # kg/m^2-sec
rod_diameter = 0.0095096 # m
rod_pitch = 1.265e-2 # m
#linear_heat_rate = power_profile
#axial_power_profile = axial_peaking_factors
coolant_material = 'water'
compute_enthalpy = true
oxide_thickness = oxide_thickness # coupled oxide_thickness
[]
[]
[Materials]
[fuel_density]
type = Density
density = 10344.71
block = fuel
[]
[fuel_thermal]
type = UO2Thermal
block = fuel
temperature = temp
burnup_function = burnup
thermal_conductivity_model = NFIR
initial_porosity = 0.057
[]
[fuel_elasticity_tensor]
type = ComputeIsotropicElasticityTensor
block = fuel
youngs_modulus = 2.0e11
poissons_ratio = 0.345
[]
[fuel_elastic_stress]
type = ComputeFiniteStrainElasticStress
block = fuel
[]
[fuel_thermal_expansion]
type = ComputeInstantaneousThermalExpansionFunctionEigenstrain
block = fuel
thermal_expansion_function = Fuel_CTE_function
stress_free_temperature = 293.15
eigenstrain_name = fuel_thermal_strain
[]
[fuel_relocation]
type = UO2RelocationEigenstrain
block = fuel
burnup_function = burnup
diameter = 0.0080496 #Fuel pellet diameter in m
rod_ave_lin_pow = power_profile
axial_power_profile = axial_peaking_factors
diametral_gap =186.0e-6
relocation_activation1 = 5000
burnup_relocation_stop = 0.024
eigenstrain_name = fuel_relocation_strain
[]
[fuel_volumetric_swelling]
type = UO2VolumetricSwellingEigenstrain
block = fuel
temperature = temp
burnup_function = burnup
initial_fuel_density = 10344.71
total_densification = 0.00676
initial_porosity = 0.057
eigenstrain_name = fuel_volumetric_strain
[]
[fission_gas_release]
type = UO2Sifgrs
block = fuel
temperature = temp
burnup_function = burnup
initial_porosity = 0.057
grain_radius = grain_radius
gbs_model = true
[]
[clad_density]
type = Density
block = clad
density = 6550
[]
[clad_thermal]
type = ZryThermal
block = clad
temperature = temp
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
fast_neutron_fluence = fast_neutron_fluence
block = clad
[]
[clad_stress]
type = ComputeMultipleInelasticStress
tangent_operator = elastic
inelastic_models = 'clad_zrycreep clad_zryplasticity'
block = clad
[]
[clad_zrycreep]
type = ZryCreepLimbackHoppeUpdate
block = clad
max_inelastic_increment = 1.0e-4
fast_neutron_flux = fast_neutron_flux
fast_neutron_fluence = fast_neutron_fluence
[]
[clad_zryplasticity]
type = ZryPlasticityUpdate
block = clad
cold_work_factor = 0.5
max_inelastic_increment = 1.0e-4
fast_neutron_fluence = fast_neutron_fluence
fast_neutron_flux = fast_neutron_flux
plasticity_model_type = MATPRO
[]
[clad_thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = clad
stress_free_temperature = 293.15
eigenstrain_name = clad_thermal_eigenstrain
[]
[clad_irradiation_swelling]
type = ZryIrradiationGrowthEigenstrain
block = clad
fast_neutron_fluence = fast_neutron_fluence
zircaloy_material_type = stress_relief_annealed
eigenstrain_name = clad_irradiation_strain
[]
[clad_oxidation]
type = ZryOxidation
boundary = 2
clad_inner_radius = 0.0041178
clad_outer_radius = 0.0047549
use_coolant_channel = true
fast_neutron_flux = fast_neutron_flux
[]
[clad_phase]
type = ZrPhase
block = clad
numerical_method = 2
[]
[]
[Dampers]
[limitT]
type = MaxIncrement
max_increment = 10.0
variable = temp
[]
[contact_slip]
type = ContactSlipDamper
primary = 5
secondary = 10
min_damping_factor = 0.05
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-3
nl_max_its = 40
nl_rel_tol = 1e-4
nl_abs_tol = 1e-8
start_time = 0
end_time = 57542400
dtmax = 1e6
dtmin = 1e-7
[TimeStepper]
type = IterationAdaptiveDT
dt = 1.0e3
optimal_iterations = 10
iteration_window = 4
linear_iteration_ratio = 100
timestep_limiting_function = power_profile
max_function_change = 1e5
force_step_every_function_point = true
timestep_limiting_postprocessor = material_timestep_control
time_t = '57542410 57542420 57542430 57542440 57542450 57542460 57542470 57542480'
time_dt = '10 10 10 10 10 10 10 10'
[]
[Quadrature]
order = FIFTH
side_order = SEVENTH
[]
[]
[Postprocessors]
[ave_temp_interior] # average temperature of the cladding interior and all pellet exteriors
type = LayeredSideAverageValuePostprocessor
boundary = 9
variable = temp
execute_on = 'initial linear'
fuel_pin_geometry = pin_geometry
[]
[avg_clad_temp] # average temperature of cladding interior
type = LayeredSideAverageValuePostprocessor
boundary = 7
variable = temp
fuel_pin_geometry = pin_geometry
execute_on = 'initial timestep_end'
[]
[max_fuel_temp]
type = NodalExtremeValue
block = fuel
value_type = max
variable = temp
execute_on = 'initial timestep_end'
[]
[min_fuel_temp]
type = NodalExtremeValue
block = fuel
value_type = min
variable = temp
execute_on = 'initial timestep_end'
[]
[max_clad_temp]
type = NodalExtremeValue
block = clad
value_type = max
variable = temp
execute_on = 'initial timestep_end'
[]
[min_clad_temp]
type = NodalExtremeValue
block = clad
value_type = min
variable = temp
execute_on = 'initial timestep_end'
[]
[fis_gas_generated]
type = LayeredElementIntegralFisGasGeneratedSifgrsPostprocessor
block = fuel
fuel_pin_geometry = pin_geometry
[]
[fis_gas_released]
type = LayeredElementIntegralFisGasReleasedSifgrsPostprocessor
block = fuel
fuel_pin_geometry = pin_geometry
[]
[fis_gas_grain]
type = LayeredElementIntegralFisGasGrainSifgrsPostprocessor
block = fuel
outputs = exodus
fuel_pin_geometry = pin_geometry
[]
[fis_gas_boundary]
type = LayeredElementIntegralFisGasBoundarySifgrsPostprocessor
block = fuel
outputs = exodus
fuel_pin_geometry = pin_geometry
[]
[clad_inner_vol]
type = LayeredInternalVolumePostprocessor
boundary = 7
component = 0
fuel_pin_geometry = pin_geometry
out_of_plane_strain = strain_yy
execute_on = 'initial linear'
[]
[pellet_volume]
type = LayeredInternalVolumePostprocessor
boundary = 8
component = 0
fuel_pin_geometry = pin_geometry
out_of_plane_strain = strain_yy
execute_on = 'initial linear'
[]
[gas_volume] # gas volume
type = LayeredInternalVolumePostprocessor
boundary = 9
execute_on = 'initial linear'
component = 0
fuel_pin_geometry = pin_geometry
out_of_plane_strain = strain_yy
[]
[flux_from_clad]
type = LayeredSideFluxIntegralPostprocessor
variable = temp
boundary = 5
diffusivity = thermal_conductivity
fuel_pin_geometry = pin_geometry
[]
[flux_from_fuel]
type = LayeredSideFluxIntegralPostprocessor
variable = temp
boundary = 10
diffusivity = thermal_conductivity
fuel_pin_geometry = pin_geometry
[]
[rod_input_power]
type = FunctionValuePostprocessor
function = power_profile
scale_factor = 1.05114 # rod height
[]
[average_burnup]
type = RodAverageBurnup
burnup_function = burnup
[]
[burnup_GWd]
type = FunctionValuePostprocessor
function = burnup_GWd
[]
[fis_gas_percent]
type = FGRPercent
fission_gas_released = fis_gas_released
fission_gas_generated = fis_gas_generated
[]
[vonmises_stress_fuel]
type = ElementAverageValue
block = fuel
variable = vonmises_stress
[]
[vonmises_stress_clad]
type = ElementAverageValue
block = clad
variable = vonmises_stress
[]
[material_timestep_control]
type = MaterialTimeStepPostprocessor
block = clad
[]
## Nodal values
[FCT] #fuel centerline temperature
type = NodalVariableValue
variable = temp
nodeid = 264 #(0, 0.558383, 0)
[]
[FST] #fuel surface temperature
type = NodalVariableValue
variable = temp
nodeid = 295 #(0.0040248, 0.558383, 0)
[]
[CIST] #clad inner surface temperature
type = NodalVariableValue
variable = temp
nodeid = 45 #(0.0041178, 0.558383, 0)
[]
[COST] #clad outer surface temperature
type = NodalVariableValue
variable = temp
nodeid = 52 #(0.0047548, 0.558383, 0)
[]
[gap]
type = NodalVariableValue
variable = penetration
nodeid = 295 #(0.0040248, 0.558383, 0)
use_displaced_mesh = true
[]
[contact_pressure]
type = NodalVariableValue
variable = contact_pressure
nodeid = 295 #(0.0040248, 0.558383, 0)
use_displaced_mesh = true
[]
[]
[VectorPostprocessors]
[clad_dia]
type = NodalValueSampler
variable = disp_x
boundary = 2
sort_by = y
outputs = 'outfile_clad_diameter'
[]
[pellet_dia]
type = NodalValueSampler
variable = disp_x
boundary = 10
sort_by = y
outputs = 'outfile_pellet_diameter'
[]
[ox_thick]
type = SideValueSampler
variable = oxide_thickness
boundary = 2
sort_by = y
outputs = 'outfile_oxide_thickness'
[]
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
time_step_interval = 1
csv = true
#exodus = true
color = false
[outfile_clad_diameter]
type = CSV
#execute_on = 'FINAL'
sync_times = '57542400 57542900'
sync_only = true
[]
[outfile_pellet_diameter]
type = CSV
#execute_on = 'FINAL'
sync_times = '57542400 57542900'
sync_only = true
[]
[outfile_oxide_thickness]
type = CSV
#execute_on = 'FINAL'
sync_times = '57542400 57542900'
sync_only = true
[]
[console]
type = Console
output_linear = true
max_rows = 10
[]
[chkfile]
type = CSV
show = 'ave_temp_interior fis_gas_released FCT average_burnup'
execute_on = 'FINAL'
[]
[exodus]
type = Exodus
time_step_interval = 4
[]
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-02/puzry-02_aniso.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-02.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 2000. '
y = '1.e+05 1.e+05 7.5e+05' # Linear increase at 0.064 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 2000. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
# Circumferential steady-state creep test and analysis of Zircaloy-4 fuel cladding
# Nuclear Engineering and Design, 53, 2312-2322 (2021)
[F]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.738 0.738 0.57'
[]
[G]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.174 0.174 0.45'
[]
[H]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.588 0.588 0.48'
[]
[L]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[M]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[N]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = TaylorExpansion
use_automatic_differentiation = true
[]
[]
[]
[]
[Kernels]
[heat]
type = ADHeatConduction
variable = temperature
[]
[heat_ie]
type = ADHeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = ADMaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = ADMaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = ADMaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = ADMaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = ADMaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = ADFunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = ADDirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = ADDirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ADZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1.e+11
poissons_ratio = 0.3
block = 1
[]
[hill_constants]
type = ADHillConstants
hill_constants = "0.738 0.174 0.588 1.0 1.0 1.0"
function_names = "F G H L M N"
temperature = temperature
[]
[creep_update]
type = ADZryAnisoCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 2.5e-05
temperature = temperature
temperature_standard_thermal_creep_end = 700
temperature_loca_creep_begin = 900.
fract_beta_phase_name = 'fract_beta_phase'
max_integration_error = 1000000.0
absolute_tolerance = 1e-07
relative_tolerance = 1e-07
[]
[creep]
type = ADComputeMultipleInelasticStress
block = 1
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ADZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = ADDensity
block = 1
[]
[phase]
type = ADZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ADZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = NEWTON
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0.
n_startup_steps = 1
end_time = 2500.
dtmax = 1.
dtmin = 1.0e-9
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-02_aniso_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-16/puzry-16_aniso.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-16.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 2000. '
y = '1.e+05 1.e+05 1.234e+07' # Linear increase at 0.1224 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 2000. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
# Circumferential steady-state creep test and analysis of Zircaloy-4 fuel cladding
# Nuclear Engineering and Design, 53, 2312-2322 (2021)
[F]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.738 0.738 0.57'
[]
[G]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.174 0.174 0.45'
[]
[H]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.588 0.588 0.48'
[]
[L]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[M]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[N]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = TaylorExpansion
use_automatic_differentiation = true
[]
[]
[]
[]
[Kernels]
[heat]
type = ADHeatConduction
variable = temperature
[]
[heat_ie]
type = ADHeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = ADMaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = ADMaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = ADMaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = ADMaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = ADMaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = ADFunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = ADDirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = ADDirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ADZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1.e+11
poissons_ratio = 0.3
block = 1
[]
[hill_constants]
type = ADHillConstants
hill_constants = "0.738 0.174 0.588 1.0 1.0 1.0"
function_names = "F G H L M N"
temperature = temperature
[]
[creep_update]
type = ADZryAnisoCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 1.5e-05
temperature = temperature
temperature_standard_thermal_creep_end = 700
temperature_loca_creep_begin = 900.
fract_beta_phase_name = 'fract_beta_phase'
max_integration_error = 1000000.0
absolute_tolerance = 1e-13
relative_tolerance = 1e-11
[]
[creep]
type = ADComputeMultipleInelasticStress
block = 1
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ADZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = ADDensity
block = 1
[]
[phase]
type = ADZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ADZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = NEWTON
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-07
start_time = 0.
n_startup_steps = 1
end_time = 2500.
dtmax = 1.
dtmin = 1.0e-9
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-16_aniso_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(test/tests/thermalZry/thermal_zry_negative_temperature_exception.i)
# This test ensures that the moose exception to cut the timestep when a
# negative temperature is detected in ZryThermal is properly executed.
[Mesh]
[line]
type = GeneratedMeshGenerator
dim = 1
[]
[]
[Functions]
[temperature_func]
type = PiecewiseLinear
x = '0 2'
y = '300 -100.0'
[]
[]
[Variables]
[temp]
initial_condition = 300
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temp
[]
[]
[BCs]
[fixed_temp]
type = FunctionDirichletBC
variable = temp
boundary = 'left right'
function = temperature_func
[]
[]
[Materials]
[thermal_clad]
type = ZryThermal
temperature = temp
[]
[]
[Executioner]
type = Transient
num_steps = 2
dt = 2
[]
[Postprocessors]
[dt]
type = TimestepSize
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'dt = 1'
execute_on = timestep_end
[]
[]
[Outputs]
csv = true
[]
(assessment/LWR/validation/LOCA_REBEKA_cladding_burst_tests/analysis/rebeka_2d_10MPa/rebeka_singlerod_2d_10MPa_aniso_hunt.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
order = SECOND
family = LAGRANGE
displacements = 'disp_x disp_y'
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = rebeka_singlerod.e
[]
[]
[Variables]
[temperature]
initial_condition = 573.0
[]
[]
[Functions]
[temperature_func]
type = PiecewiseLinear
x = '0. 700. '
y = '573. 1273.' # From 300 to 1000 C at 1 K/s
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 700. '
y = '1.e+07 1.e+07' # 100 bar
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 700. '
y = '1.e+05 1.e+05' # atmospheric pressure
[]
# Circumferential steady-state creep test and analysis of Zircaloy-4 fuelcladding
# Nuclear Engineering and Design, 53, 2312-2322 (2021)
[F]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.738 0.57 0.57'
[]
[G]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.174 0.45 0.45'
[]
[H]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.588 0.48 0.48'
[]
[L]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[M]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[N]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[clad]
block = cladding
add_variables = true
strain = FINITE
decomposition_method = TaylorExpansion
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz hoop_stress'
use_automatic_differentiation = true
[]
[]
[AuxVariables]
[creep_rate_aux]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[scale_thickness]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfract_total]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfgain_total]
order = CONSTANT
family = MONOMIAL
[]
[burst_stress]
order = CONSTANT
family = MONOMIAL
[]
[burst]
order = CONSTANT
family = MONOMIAL
[]
[]
[Kernels]
[heat]
type = ADHeatConduction
variable = temperature
[]
[heat_ie]
type = ADHeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate_aux]
type = ADMaterialRealAux
variable = creep_rate_aux
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = ADMaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = ADMaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[scl_thickness]
type = ADMaterialRealAux
variable = scale_thickness
property = oxide_scale_thickness
boundary = 2
[]
[ofract_total]
type = ADMaterialRealAux
variable = oxywtfract_total
property = current_oxygen_weight_frac_total
boundary = 2
[]
[ofgain_total]
type = ADMaterialRealAux
boundary = 2
variable = oxywtfgain_total
property = oxygen_weight_frac_gained_total
[]
[sigmaburst]
type = ADMaterialRealAux
variable = burst_stress
property = burst_stress
boundary = 2
[]
[hasburst]
type = ADMaterialRealAux
variable = burst
property = failed
boundary = 2
execute_on = timestep_end
[]
[]
[BCs]
[inner_temperature]
type = REBEKADirichletBC
variable = temperature
function_tempm = temperature_func
minimum_temperature = 573.
translation = 0.1625
boundary = 4
[]
[no_y_midsection]
type = ADDirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply steam pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 101 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[CoolantChannel]
[convective_clad_surface]
boundary = 2
variable = temperature
inlet_temperature = 473.
inlet_pressure = 1.e+05
inlet_massflux = 1.0 # kg/m^2-sec # almost stagnant steam
rod_diameter = 10.75e-03
rod_pitch = 1.26e-02 # default
oxide_thickness = scale_thickness
use_ad = true
[]
[]
[Materials]
[thermal]
type = ADZryThermal
block = cladding
temperature = temperature
[]
[clad_elasticity_tensor]
type = ADZryElasticityTensor
block = cladding
matpro_youngs_modulus = false
matpro_poissons_ratio = false
[]
[clad_stress]
type = ADComputeMultipleInelasticStress
inelastic_models = 'clad_zrycreep'
block = cladding
[]
[hill_constants]
type = ADHillConstants
hill_constants = "0.956 0.240 0.304 1.0 1.0 1.0"
# function_names = "F G H L M N"
# temperature = temperature
[]
[clad_zrycreep]
type = ADZryAnisoCreepLOCAUpdate
block = cladding
temperature = temperature
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
temperature_loca_creep_begin = 501
temperature_standard_thermal_creep_end = 500
fract_beta_phase_name = 'fract_beta_phase'
[]
[thermal_expansion]
type = ADZryThermalExpansionMATPROEigenstrain
block = cladding
temperature = temperature
stress_free_temperature = 573.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[density]
type = ADDensity
block = cladding
[]
[phase]
type = ADZrPhase
block = cladding
temperature = temperature
numerical_method = 2
[]
[oxidation]
type = ADZryOxidation
boundary = 2
temperature = temperature
clad_inner_radius = 0.00465
clad_outer_radius = 0.005375
normal_operating_temperature_model = epri_kwu_ce
high_temperature_model = leistikow
use_coolant_channel = true
[]
[clad_failure_criterion]
type = ADZryCladdingFailure
boundary = 2
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate_aux
temperature = temperature
fraction_beta_phase = fract_beta_phase
fraction_oxygen_gain = oxywtfgain_total
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = NEWTON
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-06
nl_abs_tol = 1.e-08
start_time = 0
n_startup_steps = 1
end_time = 700.
dtmax = 1.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[Postprocessors]
[ave_clad_exterior_temp]
type = SideAverageValue
boundary = 2
variable = temperature
[]
[max_clad_temp]
type = NodalExtremeValue
block = cladding
value_type = max
variable = temperature
[]
[min_clad_temp]
type = NodalExtremeValue
block = cladding
value_type = min
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = cladding
[]
[max_oxygen_fract]
type = ElementExtremeValue
block = cladding
value_type = max
variable = oxywtfract_total
[]
[max_betaph_fract]
type = ElementExtremeValue
block = cladding
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
block = cladding
value_type = max
variable = creep_rate_aux
[]
[max_creep_strain_mag]
type = ElementExtremeValue
block = cladding
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
block = cladding
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
block = cladding
value_type = max
variable = hoop_stress
[]
[vonmises_stress_clad]
type = ElementAverageValue
block = cladding
variable = vonmises_stress
[]
[min_burst_stress]
type = ElementExtremeValue
block = cladding
value_type = min
variable = burst_stress
[]
[burst]
type = ElementExtremeValue
block = cladding
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = cladding
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[top_disp_r_clad] # this is mid height
type = NodalVariableValue
variable = disp_x
nodeid = 0 #coords (0.005375, 0.1625)
[]
[top_disp_r_clad_slice] # this is mid height matched to the 1.5d
type = NodalVariableValue
variable = disp_x
nodeid = 3 #coords (0.005375, 0.1625)
[]
[top_disp_z_clad]
type = NodalVariableValue
variable = disp_y
nodeid = 0 #coords (0.005375, 0.1625)
[]
[stress_xx] # stess in the top Element
type = ElementalVariableValue
variable = stress_xx
elementid = 0
[]
[stress_yy] # stess in the top Element
type = ElementalVariableValue
variable = stress_yy
elementid = 0
[]
[stress_zz] # stess in the top Element
type = ElementalVariableValue
variable = stress_zz
elementid = 0
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = cladding
plenum_boundary_name = 4
external_clad_boundary_name = 2
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = rebeka_2d_10MPa_aniso_hunt_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-13/puzry-13_aniso.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-13.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 5000. '
y = '1.e+05 1.e+05 1.266e+07' # Linear increase at 0.0314 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 5000. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
# Circumferential steady-state creep test and analysis of Zircaloy-4 fuel cladding
# Nuclear Engineering and Design, 53, 2312-2322 (2021)
[F]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.738 0.738 0.57'
[]
[G]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.174 0.174 0.45'
[]
[H]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.588 0.588 0.48'
[]
[L]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[M]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[N]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = TaylorExpansion
use_automatic_differentiation = true
[]
[]
[]
[]
[Kernels]
[heat]
type = ADHeatConduction
variable = temperature
[]
[heat_ie]
type = ADHeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = ADMaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = ADMaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = ADMaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = ADMaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = ADMaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = ADFunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = ADDirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = ADDirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ADZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1.e+11
poissons_ratio = 0.3
block = 1
[]
[hill_constants]
type = ADHillConstants
hill_constants = "0.738 0.174 0.588 1.0 1.0 1.0"
function_names = "F G H L M N"
temperature = temperature
[]
[creep_update]
type = ADZryAnisoCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 5e-05
temperature = temperature
temperature_standard_thermal_creep_end = 700
temperature_loca_creep_begin = 900.
fract_beta_phase_name = 'fract_beta_phase'
max_integration_error = 1000000.0
absolute_tolerance = 1e-13
relative_tolerance = 1e-11
[]
[creep]
type = ADComputeMultipleInelasticStress
block = 1
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ADZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = ADDensity
block = 1
[]
[phase]
type = ADZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ADZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = NEWTON
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-07
start_time = 0.
n_startup_steps = 1
end_time = 2500.
dtmax = 1.
dtmin = 1.0e-9
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-13_aniso_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/LOCA_REBEKA_cladding_burst_tests/analysis/rebeka_2d_06MPa/rebeka_singlerod_2d_06MPa.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.0
order = SECOND
family = LAGRANGE
displacements = 'disp_x disp_y'
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = rebeka_singlerod.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 573.0
[]
[]
[Functions]
[temperature_func]
type = PiecewiseLinear
x = '0. 700. '
y = '573. 1273.' # From 300 to 1000 C at 1 K/s
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 700. '
y = '6.e+06 6.e+06' # 60 bar
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 700. '
y = '1.e+05 1.e+05' # atmospheric pressure
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[clad]
block = cladding
add_variables = false
strain = FINITE
decomposition_method = EigenSolution
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz hoop_stress'
[]
[]
[AuxVariables]
[creep_rate_aux]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[scale_thickness]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfract_total]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfgain_total]
order = CONSTANT
family = MONOMIAL
[]
[burst_stress]
order = CONSTANT
family = MONOMIAL
[]
[burst]
order = CONSTANT
family = MONOMIAL
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate_aux]
type = MaterialRealAux
variable = creep_rate_aux
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[scl_thickness]
type = MaterialRealAux
variable = scale_thickness
property = oxide_scale_thickness
boundary = 2
[]
[ofract_total]
type = MaterialRealAux
variable = oxywtfract_total
property = current_oxygen_weight_frac_total
boundary = 2
[]
[ofgain_total]
type = MaterialRealAux
boundary = 2
variable = oxywtfgain_total
property = oxygen_weight_frac_gained_total
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = 2
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = 2
execute_on = timestep_end
[]
[]
[BCs]
[inner_temperature]
type = REBEKADirichletBC
variable = temperature
function_tempm = temperature_func
minimum_temperature = 573.
translation = 0.1625
boundary = 4
[]
[no_y_midsection]
type = DirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply steam pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 101 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[CoolantChannel]
[convective_clad_surface]
boundary = 2
variable = temperature
inlet_temperature = 473.
inlet_pressure = 1.e+05
inlet_massflux = 1.0 # kg/m^2-sec # almost stagnant steam
rod_diameter = 10.75e-03
rod_pitch = 1.26e-02 # default
number_axial_zone = 15
oxide_thickness = scale_thickness
[]
[]
[Materials]
[thermal]
type = ZryThermal
block = cladding
temperature = temperature
[]
[clad_elasticity_tensor]
type = ComputeIsotropicElasticityTensor
block = cladding
youngs_modulus = 1.0e11
poissons_ratio = 0.3
[]
[clad_stress]
type = ComputeMultipleInelasticStress
tangent_operator = elastic
inelastic_models = 'clad_zrycreep'
block = cladding
[]
[clad_zrycreep]
type = ZryCreepLOCAUpdate
block = cladding
temperature = temperature
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
temperature_loca_creep_begin = 501 # see Erbacher et al., 1982
temperature_standard_thermal_creep_end = 500
[]
[thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = cladding
temperature = temperature
stress_free_temperature = 573.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[density]
type = Density
block = cladding
[]
[phase]
type = ZrPhase
block = cladding
temperature = temperature
numerical_method = 2
[]
[oxidation]
type = ZryOxidation
boundary = 2
temperature = temperature
clad_inner_radius = 0.00465
clad_outer_radius = 0.005375
normal_operating_temperature_model = epri_kwu_ce
high_temperature_model = leistikow
use_coolant_channel = true
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = 2
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate_aux
temperature = temperature
fraction_beta_phase = fract_beta_phase
fraction_oxygen_gain = oxywtfgain_total
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0
n_startup_steps = 1
end_time = 700.
dtmax = 1.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average temperature of cladding exterior
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = cladding
[]
[max_clad_temp]
type = NodalExtremeValue
block = cladding
value_type = max
variable = temperature
[]
[max_oxygen_fract]
type = ElementExtremeValue
block = cladding
value_type = max
variable = oxywtfract_total
[]
[max_betaph_fract]
type = ElementExtremeValue
block = cladding
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
block = cladding
value_type = max
variable = creep_rate_aux
[]
[max_creep_strain_mag]
type = ElementExtremeValue
block = cladding
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
block = cladding
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
block = cladding
value_type = max
variable = hoop_stress
[]
[vonmises_stress_clad]
type = ElementAverageValue
block = cladding
variable = vonmises_stress
[]
[min_burst_stress]
type = ElementExtremeValue
block = cladding
value_type = min
variable = burst_stress
[]
[burst]
type = ElementExtremeValue
block = cladding
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = cladding
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = cladding
plenum_boundary_name = 4
external_clad_boundary_name = 2
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = rebeka_2d_06MPa_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
(assessment/LWR/validation/Super_Ramp/analysis/Super_Ramp_Base.i)
#This is a partial input file base with information/features common to several experiments within this assessment
#NOTE: This file will NOT run on its own, it requires a PK#X.params file and a PK##.params file to run
# physical constants
R = 8.3143 # (J/K*mol) -- THIS SHOULD BE EDITED TO USE PHYSICALCONSTANTS' VALUE
# fuel isotope fractions and fission energy
energy_per_fission = 3.28451e-11 # (J/fission)
isotope_fraction_Pu239 = 0.0
isotope_fraction_Pu240 = 0.0
isotope_fraction_Pu241 = 0.0
isotope_fraction_Pu242 = 0.0
# rod geometry
clad_bot_gap_height = 1.0e-3 # (m)
# variable and kernel initial values
initial_temperature = 293.15 # (K)
gravity_constant = -9.81 # (m/s^2)
# fuel/cladding contact
friction_coefficient = 0.4
c_normal = 1e+12
c_tangential = 1e+24
tangential_lm_scaling = 1.0e-16
normal_lm_scaling = 1.0e-10
roughness_secondary = 1.0e-6 # (m)
roughness_primary = 2.0e-6 # (m)
roughness_coef = 3.2
jump_distance_model = LANNING
contact_pressure = mechanical_normal_lm
thermal_lm_scaling = 1.0e-2
# plenum parameters
initial_pressure = 2.25e6 # (Pa)
startup_time = 0 # (s)
# fuel/clad material properties
fuel_cracking_stress = 1.68e8
stress_free_temperature = 293.15 # (K)
clad_density = 6550.0 # (kg/m^3)
# numerical options
l_max_its = 100
l_tol = 1e-4
nl_max_its = 30
start_time = 0.0 # s
dtmin = 1.0 # s
[GlobalParams]
density = ${fuel_density}
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
energy_per_fission = ${energy_per_fission}
volumetric_locking_correction = false
initial_porosity = ${initial_fuel_porosity}
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
converge_on = 'disp_x disp_y temperature'
[]
[Mesh]
coord_type = RZ
[smeared_pellet_mesh]
type = FuelPinMeshGenerator
pellet_quantity = ${number_pellets}
pellet_height = ${pellet_height}
pellet_outer_radius = ${pellet_outer_radius}
pellet_mesh_density = customize
nx_p = 11
ny_p = 84
clad_mesh_density = customize
nx_c = 4
ny_c = 84
clad_gap_width = ${clad_gap_width}
clad_thickness = ${clad_thickness}
clad_bot_gap_height = ${clad_bot_gap_height}
bottom_clad_height = ${bottom_clad_height}
top_clad_height = ${top_clad_height}
clad_top_gap_height = ${clad_top_gap_height}
ny_cu = 3
ny_cl = 3
elem_type = QUAD8
[]
patch_size = 10
patch_update_strategy = iteration
partitioner = centroid
centroid_partitioner_direction = y
[]
[Variables]
[temperature]
initial_condition = ${initial_temperature}
[]
[]
[Functions]
[power_history]
type = PiecewiseLinear
data_file = ${power_history_data_file}
format = columns
[]
[axial_power_factors]
type = PiecewiseBilinear
data_file = ${axial_power_factors_data_file}
axis = 1
[]
[clad_out_temp]
type = PiecewiseLinear
data_file = ${clad_out_temp_data_file}
format = columns
[]
[axial_temp_factors]
type = PiecewiseBilinear
data_file = ${axial_temp_factors_data_file}
axis = 1
[]
[clad_temp_bc]
type = CompositeFunction
functions = 'clad_out_temp axial_temp_factors'
[]
[coolant_pressure]
type = PiecewiseLinear
data_file = ${coolant_pressure_data_file}
format = columns
[]
[fast_flux]
type = PiecewiseLinear
data_file = ${fast_neutron_flux_data_file}
format = columns
[]
[]
[AuxVariables]
[gap_conductance]
block = 'mechanical_secondary_subdomain'
[]
[fast_neutron_flux]
block = clad
[]
[fast_neutron_fluence]
block = clad
[]
[grain_radius]
block = pellet
initial_condition = ${initial_grain_radius}
[]
[porosity]
order = CONSTANT
family = MONOMIAL
block = pellet
initial_condition = ${initial_fuel_porosity}
[]
[pellet_id]
order = CONSTANT
family = MONOMIAL
block = pellet
[]
[oxide_thickness]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
block = clad
[]
[gas_gen_3]
order = CONSTANT
family = MONOMIAL
block = pellet
[]
[gas_grn_3]
order = CONSTANT
family = MONOMIAL
block = pellet
[]
[gas_bdr_3]
order = CONSTANT
family = MONOMIAL
block = pellet
[]
[gas_rel_3]
order = CONSTANT
family = MONOMIAL
block = pellet
[]
[bbl_bdr_2]
order = CONSTANT
family = MONOMIAL
block = pellet
[]
[prs_bbl_bdr]
order = CONSTANT
family = MONOMIAL
block = pellet
[]
[prseq_bbl_bdr]
order = CONSTANT
family = MONOMIAL
block = pellet
[]
[rad_bbl_bdr]
order = CONSTANT
family = MONOMIAL
block = pellet
[]
[GBCoverage]
order = CONSTANT
family = MONOMIAL
block = pellet
[]
[sat_coverage]
order = CONSTANT
family = MONOMIAL
block = pellet
[]
[eff_diff_coeff]
order = CONSTANT
family = MONOMIAL
block = pellet
[]
[deltav_v0_bd]
order = CONSTANT
family = MONOMIAL
block = pellet
[]
[gaseous_porosity]
order = CONSTANT
family = MONOMIAL
block = pellet
[]
[thermal_conductivity]
order = CONSTANT
family = MONOMIAL
block = pellet
[]
[layered_average_contact_pressure]
order = CONSTANT
family = MONOMIAL
[]
[volumetric_swelling_strain]
order = CONSTANT
family = MONOMIAL
[]
[gap_cond]
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[pellets]
block = pellet
temperature = temperature
add_variables = true
strain = FINITE
eigenstrain_names = 'fuel_relocation_strain fuel_thermal_strain
fuel_volumetric_strain'
generate_output = 'vonmises_stress hydrostatic_stress stress_xx stress_yy
stress_zz strain_xx strain_yy strain_zz'
extra_vector_tags = 'ref'
[]
[clad]
block = clad
temperature = temperature
add_variables = true
strain = FINITE
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
eigenstrain_names = 'clad_thermal_eigenstrain clad_irradiation_strain'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz
creep_strain_xx creep_strain_yy creep_strain_xy creep_strain_zz strain_xx
strain_yy strain_zz hoop_stress'
extra_vector_tags = 'ref'
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
extra_vector_tags = 'ref'
block = '1 3'
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
extra_vector_tags = 'ref'
block = '1 3'
[]
[heat_source]
type = NeutronHeatSource
variable = temperature
block = pellet
burnup_function = burnup
extra_vector_tags = 'ref'
[]
[gravity]
type = Gravity
variable = disp_y
value = ${gravity_constant}
block = '1 3'
[]
[]
[AuxKernels]
[gap_conductance]
type = GapConductanceMortar
primary_boundary = 5
secondary_boundary = 10
primary_subdomain = 'mechanical_primary_subdomain'
secondary_subdomain = 'mechanical_secondary_subdomain'
heat_flux = thermal_contact_thermal_lm
temperature = temperature
variable = gap_conductance
[]
[fast_neutron_flux]
type = FastNeutronFluxAux
variable = fast_neutron_flux
block = clad
function = fast_flux
execute_on = timestep_begin
[]
[fast_neutron_fluence]
type = FastNeutronFluenceAux
variable = fast_neutron_fluence
fast_neutron_flux = fast_neutron_flux
execute_on = timestep_begin
[]
[grain_radius]
type = GrainRadiusAux
block = pellet
variable = grain_radius
temperature = temperature
execute_on = linear
[]
[porosity]
type = PorosityAuxUO2
block = pellet
variable = porosity
execute_on = linear
[]
[pelletid]
type = PelletIdAux
block = pellet
variable = pellet_id
fuel_pin_geometry = pin_geometry
number_pellets = ${number_pellets}
execute_on = initial
[]
[oxi_thickness]
type = MaterialRealAux
variable = oxide_thickness
property = oxide_scale_thickness
boundary = 2
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fggen]
type = MaterialRealAux
variable = gas_gen_3
property = gas_concentration_generated_total
[]
[fggrn]
type = MaterialRealAux
variable = gas_grn_3
property = gas_concentration_intra_total
[]
[fgbdr]
type = MaterialRealAux
variable = gas_bdr_3
property = gas_concentration_GB_bubble_volume
[]
[fgrel]
type = MaterialRealAux
variable = gas_rel_3
property = gas_concentration_release_total
[]
[nbbl2]
type = MaterialRealAux
variable = bbl_bdr_2
property = bubble_GB_surface_density
[]
[prsbbl]
type = MaterialRealAux
variable = prs_bbl_bdr
property = bubble_GB_pressure
[]
[prseqbbl]
type = MaterialRealAux
variable = prseq_bbl_bdr
property = bubble_GB_pressure_equilibrium
[]
[radbbl]
type = MaterialRealAux
variable = rad_bbl_bdr
property = bubble_radius_GB
[]
[frcvrg]
type = MaterialRealAux
variable = GBCoverage
property = GBCoverage
[]
[stcvrg]
type = MaterialRealAux
variable = sat_coverage
property = sat_coverage
[]
[diffc]
type = MaterialRealAux
variable = eff_diff_coeff
property = eff_diff_coeff
[]
[dvv0bd]
type = MaterialRealAux
variable = deltav_v0_bd
property = deltav_v0_bubble_GB
[]
[gaspor]
type = MaterialRealAux
variable = gaseous_porosity
property = gaseous_porosity
[]
[fuel_conductivity]
type = MaterialRealAux
variable = thermal_conductivity
property = thermal_conductivity
[]
[layered_average_contact_pressure]
type = SpatialUserObjectAux
block = pellet
variable = layered_average_contact_pressure
execute_on = nonlinear
user_object = layered_average_contact_pressure
[]
[volumetric_swelling_strain]
type = MaterialRealAux
variable = volumetric_swelling_strain
property = volumetric_swelling_strain
block = pellet
execute_on = nonlinear
[]
[]
[Burnup]
[burnup]
block = pellet
rod_ave_lin_pow = power_history
axial_power_profile = axial_power_factors
num_radial = 80
num_axial = 20
isotopes = 'U235 U238 Pu239 Pu240 Pu241 Pu242'
isotope_fractions = '${isotope_fraction_U235} ${isotope_fraction_U238} ${isotope_fraction_Pu239} ${isotope_fraction_Pu240} ${isotope_fraction_Pu241} ${isotope_fraction_Pu242}'
RPF = RPF
fuel_pin_geometry = pin_geometry
fuel_volume_ratio = 1.0
[]
[]
[Contact]
[mechanical]
model = coulomb
formulation = mortar
primary = 5
secondary = 10
friction_coefficient = ${friction_coefficient}
c_normal = ${c_normal}
c_tangential = ${c_tangential}
tangential_lm_scaling = ${tangential_lm_scaling}
normal_lm_scaling = ${normal_lm_scaling}
[]
[]
[ThermalContactMortar]
[thermal_contact]
secondary_variable = temperature
primary_boundary = '5'
secondary_boundary = '10'
initial_moles = initial_moles
gas_released = fission_gas_released
roughness_secondary = ${roughness_secondary}
roughness_primary = ${roughness_primary}
roughness_coef = ${roughness_coef}
plenum_pressure = plenum_pressure
jump_distance_model = ${jump_distance_model}
contact_pressure = ${contact_pressure}
thermal_lm_scaling = ${thermal_lm_scaling}
[]
[]
[PlenumTemperature]
[plenum_temp]
boundary = 5
inner_surfaces = 5
outer_surfaces = 10
temperature = temperature
[]
[]
[BCs]
[no_x_all]
type = DirichletBC
variable = disp_x
boundary = 12
value = 0.0
[]
[no_y_clad_bottom]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[]
[no_y_fuel_bottom]
type = DirichletBC
variable = disp_y
boundary = 1020
value = 0.0
[]
[temp]
type = FunctionDirichletBC
boundary = '1 2 3'
variable = temperature
function = clad_temp_bc
[]
[Pressure]
[coolantPressure]
boundary = '1 2 3'
function = coolant_pressure
[]
[]
[PlenumPressure]
[plenumPressure]
boundary = 9
initial_pressure = ${initial_pressure}
startup_time = ${startup_time}
R = ${R}
output_initial_moles = initial_moles
temperature = plenum_temp
volume = plenum_volume
material_input = fission_gas_released
output = plenum_pressure
[]
[]
[]
[Materials]
[fuel_thermal]
type = UO2Thermal
block = pellet
thermal_conductivity_model = NFIR
temperature = temperature
burnup_function = burnup
[]
[fuel_volumetric_swelling]
type = UO2VolumetricSwellingEigenstrain
gas_swelling_model_type = SIFGRS
block = pellet
temperature = temperature
burnup_function = burnup
initial_fuel_density = ${fuel_density}
eigenstrain_name = fuel_volumetric_strain
[]
[fuel_elasticity_tensor]
type = UO2ElasticityTensor
block = pellet
density = ${fuel_density}
temperature = temperature
matpro_youngs_modulus = true
matpro_poissons_ratio = true
[]
[fuel_creep]
type = UO2CreepUpdate
block = pellet
temperature = temperature
burnup_function = burnup
initial_grain_radius = ${initial_grain_radius}
[]
[fuel_stress]
type = ComputeSmearedCrackingStress
block = pellet
cracking_stress = ${fuel_cracking_stress}
inelastic_models = 'fuel_creep'
softening_models = exponential_softening
shear_retention_factor = 0.1
max_stress_correction = 0
cracked_elasticity_type = DIAGONAL
output_properties = crack_damage
outputs = exodus
[]
[exponential_softening]
type = ExponentialSoftening
[]
[fuel_relocation]
type = UO2RelocationEigenstrain
block = pellet
burnup_function = burnup
rod_ave_lin_pow = power_history
axial_power_profile = axial_power_factors
relocation_activation1 = 5000
relocation_model = ESCORE_modified
eigenstrain_name = fuel_relocation_strain
fuel_pin_geometry = pin_geometry
model_relocation_recovery = true
max_relocation_recovery_fraction = 0.5
relocation_scaling_factor = 1
volumetric_swelling_increment = vol_swell_increment
layered_average_contact_pressure = layered_average_contact_pressure
outputs = all
output_properties = 'relocation_strain recovered_relocation_strain'
[]
[fuel_thermal_expansion]
type = UO2ThermalExpansionMATPROEigenstrain
block = pellet
temperature = temperature
stress_free_temperature = ${stress_free_temperature}
eigenstrain_name = fuel_thermal_strain
[]
[fission_gas_release]
type = UO2Sifgrs
block = pellet
hydrostatic_stress = hydrostatic_stress
diff_coeff_option = TURNBULL_D1_4D2_D3
transient_option = MICROCRACKING_BURNUP
res_param_option = HETEROGENEOUS_WHITE
ig_bubble_model = NUCLEATION_RESOLUTION
ig_diff_algorithm = polypole2
temperature = temperature
burnup_function = burnup
grain_radius = grain_radius
gbs_model = true
pellet_id = pellet_id
pellet_brittle_zone = pbz
ath_model = true
rod_ave_lin_pow = power_history
axial_power_profile = axial_power_factors
[]
[fuel_density]
type = Density
block = pellet
[]
[clad_thermal]
type = ZryThermal
block = clad
temperature = temperature
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = clad
fast_neutron_fluence = fast_neutron_fluence
temperature = temperature
matpro_youngs_modulus = true
matpro_poissons_ratio = true
[]
[clad_stress]
type = ComputeMultipleInelasticStress
tangent_operator = nonlinear
inelastic_models = 'clad_zrycreep'
block = clad
[]
[clad_zrycreep]
type = ZryCreepLimbackHoppeUpdate
block = clad
temperature = temperature
fast_neutron_flux = fast_neutron_flux
fast_neutron_fluence = fast_neutron_fluence
model_irradiation_creep = true
model_primary_creep = true
model_thermal_creep = true
zircaloy_material_type = stress_relief_annealed
[]
[thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = clad
temperature = temperature
stress_free_temperature = ${stress_free_temperature}
eigenstrain_name = clad_thermal_eigenstrain
[]
[irradiation_swelling]
type = ZryIrradiationGrowthEigenstrain
block = clad
fast_neutron_fluence = fast_neutron_fluence
zircaloy_material_type = stress_relief_annealed
eigenstrain_name = clad_irradiation_strain
[]
[clad_density]
type = Density
block = clad
density = ${clad_density}
[]
[clad_oxidation]
type = ZryOxidation
boundary = 2
temperature = temperature
normal_operating_temperature_model = epri_kwu_ce
high_temperature_model = leistikow
fuel_pin_geometry = pin_geometry
[]
[]
[Preconditioning]
[SMP]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_converged_reason -ksp_converged_reason -snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package -mat_mffd_err -pc_factor_shift_type -pc_factor_shift_amount'
petsc_options_value = ${petsc_options_value}
line_search = 'none'
verbose = true
l_max_its = ${l_max_its}
l_tol = ${l_tol}
nl_max_its = ${nl_max_its}
nl_rel_tol = ${nl_rel_tol}
nl_abs_tol = ${nl_abs_tol}
start_time = ${start_time}
n_startup_steps = 1
end_time = ${end_time}
dtmax = ${dtmax}
dtmin = ${dtmin}
[TimeStepper]
type = IterationAdaptiveDT
dt = 100
optimal_iterations = ${optimal_iterations}
iteration_window = ${iteration_window}
timestep_limiting_function = power_history
force_step_every_function_point = true
[]
[]
[Postprocessors]
[avg_gap_conductance]
type = ElementAverageValue
block = 'mechanical_secondary_subdomain'
variable = gap_conductance
execute_on = 'initial timestep_end'
[]
[central_fuel_temp]
type = NodalVariableValue
variable = temperature
nodeid = 3110 #Mesh dependent!
execute_on = 'initial timestep_end'
[]
[max_fuel_temp]
type = NodalExtremeValue
block = pellet
value_type = max
variable = temperature
execute_on = 'initial timestep_end'
[]
[max_clad_temp]
type = NodalExtremeValue
block = clad
value_type = max
variable = temperature
execute_on = 'initial timestep_end'
[]
[midplane_hoop_strain_inner_clad]
type = ElementalVariableValue
elementid = 209 # Mesh dependent
variable = strain_zz
execute_on = 'initial timestep_end'
[]
[midplane_hoop_stress_inner_clad]
type = ElementalVariableValue
elementid = 209 # Mesh dependent
variable = hoop_stress
execute_on = 'initial timestep_end'
[]
[midplane_contact_pressure]
type = NodalVariableValue
variable = contact_pressure
nodeid = 3141 # Mesh dependent
execute_on = 'initial timestep_end'
[]
[total_rod_integral_power]
type = ElementIntegralPower
variable = temperature
burnup_function = burnup
block = pellet
[]
[total_rod_input_power]
type = FunctionValuePostprocessor
function = power_history
scale_factor = ${scale_factor}
[]
[vol_swell_increment]
type = SideAverageIncrementTensorComponent
boundary = 10
variable = volumetric_swelling_strain
execute_on = nonlinear
[]
[midplane_clad_outer_temp]
type = NodalVariableValue
nodeid = 757 # Mesh dependent
variable = temperature
[]
[midplane_clad_inner_temp]
type = NodalVariableValue
nodeid = 747 # Mesh dependent
variable = temperature
[]
[]
[StandardLWRFuelRodOutputs]
fuel_pellet_blocks = 3
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
color = false
[csv]
type = CSV
file_base = '${id}_csv'
[]
[exodus]
type = Exodus
file_base = '${id}_exodus'
[]
[console]
type = Console
max_rows = 25
[]
[chkfile]
type = CSV
file_base = '${id}_chkfile'
show = 'average_burnup fission_gas_released_percentage central_fuel_temp midplane_contact_pressure'
execute_on = 'FINAL'
[]
[]
[UserObjects]
[pin_geometry]
type = FuelPinGeometry
[]
[pbz]
type = PelletBrittleZone
block = pellet
pellet_id = pellet_id
temperature = temperature
fuel_pin_geometry = pin_geometry
number_pellets = ${number_pellets}
execute_on = 'initial linear'
[]
[layered_average_contact_pressure]
type = LayeredSideAverage
variable = contact_pressure
direction = y
num_layers = 1
execute_on = timestep_end
boundary = 10
[]
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-24/puzry-24.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-24.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 6000. '
y = '1.e+05 1.e+05 9.05e+06' # Linear increase at 0.0179 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 6000. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = EigenSolution
[]
[]
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = MaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = FunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = DirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = DirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1.e+11
poissons_ratio = 0.3
block = 1
[]
[creep_update]
type = ZryCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 1.e-04
temperature = temperature
temperature_standard_thermal_creep_end = 700
temperature_loca_creep_begin = 900.
[]
[creep]
type = ComputeMultipleInelasticStress
block = 1
tangent_operator = elastic
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = Density
block = 1
[]
[phase]
type = ZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
active = 'smp'
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0.
n_startup_steps = 1
end_time = 6000.
dtmax = 1.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-24_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-21/puzry-21_aniso.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-21.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 4000. '
y = '1.e+05 1.e+05 5.14e+06' # Linear increase at 0.0168 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 4000. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
# Circumferential steady-state creep test and analysis of Zircaloy-4 fuel cladding
# Nuclear Engineering and Design, 53, 2312-2322 (2021)
[F]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.738 0.738 0.57'
[]
[G]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.174 0.174 0.45'
[]
[H]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.588 0.588 0.48'
[]
[L]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[M]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[N]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = TaylorExpansion
use_automatic_differentiation = true
[]
[]
[]
[]
[Kernels]
[heat]
type = ADHeatConduction
variable = temperature
[]
[heat_ie]
type = ADHeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = ADMaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = ADMaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = ADMaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = ADMaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = ADMaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = ADFunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = ADDirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = ADDirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ADZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1.e+11
poissons_ratio = 0.3
block = 1
[]
[hill_constants]
type = ADHillConstants
hill_constants = "0.738 0.174 0.588 1.0 1.0 1.0"
function_names = "F G H L M N"
temperature = temperature
[]
[creep_update]
type = ADZryAnisoCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 1.5e-05
temperature = temperature
temperature_standard_thermal_creep_end = 700
temperature_loca_creep_begin = 900.
fract_beta_phase_name = 'fract_beta_phase'
max_integration_error = 1000000.0
absolute_tolerance = 1e-13
relative_tolerance = 1e-11
[]
[creep]
type = ADComputeMultipleInelasticStress
block = 1
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ADZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = ADDensity
block = 1
[]
[phase]
type = ADZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ADZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = NEWTON
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-07
start_time = 0.
n_startup_steps = 1
end_time = 2500.
dtmax = 1.
dtmin = 1.0e-9
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-21_aniso_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(examples/accident_tolerant_fuel/uo2_coated_zircaloy/uo2_coated_zircaloy.i)
[GlobalParams]
# Set initial fuel density, other global parameters
density = 10431.0
order = SECOND
family = LAGRANGE
energy_per_fission = 3.2e-11 # J/fission
displacements = 'disp_x disp_y'
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
[]
[Mesh]
coord_type = RZ
[smeared_pellet_mesh]
type = FuelPinMeshGenerator
clad_top_gap_height = 0.026
pellet_height = 0.1186
pellet_quantity = 1
clad_bot_gap_height = 0
pellet_outer_radius = 4.1e-3
clad_gap_width = 80e-6
clad_thickness = 0.57e-3
coating_thickness = 40e-6
clad_mesh_density = customize
pellet_mesh_density = customize
nx_c = 3
ny_c = 40
nx_p = 11
ny_p = 40
nx_coating = 2
elem_type = QUAD8
[]
patch_update_strategy = auto
partitioner = centroid
centroid_partitioner_direction = y
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 293.0
[]
[]
[UserObjects]
[pin_geometry]
type = FuelPinGeometry
clad_inner_wall = 5
clad_outer_wall = 2
clad_top = 3
clad_bottom = 1
pellet_exteriors = 8
[]
[]
[AuxVariables]
[fast_neutron_flux]
block = clad
[]
[fast_neutron_fluence]
block = clad
[]
[grain_radius]
block = pellet
initial_condition = 10e-6
[]
[gap_cond]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[oxide_thickness]
order = CONSTANT
family = MONOMIAL
[]
[total_hoop_strain]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_hoop]
order = CONSTANT
family = MONOMIAL
[]
[hoop_stress]
order = CONSTANT
family = MONOMIAL
[]
[]
[Functions]
[power_history]
type = PiecewiseLinear
x = '0 1e4 1e8'
y = '0 2.5e4 2.5e4'
scale_factor = 1
[]
[axial_peaking_factors]
type = ParsedFunction
expression = 1
[]
[pressure_ramp]
type = PiecewiseLinear
x = '-200 0 1e8'
y = '6.537e-3 1 1'
scale_factor = 15.5e6
[]
[mass_flux_func]
type = PiecewiseLinear
x = '-200 0 1e8'
y = '3800. 3800. 3800.'
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[pellets]
block = pellet
strain = FINITE
eigenstrain_names = 'fuel_relocation_strain fuel_thermal_strain fuel_volumetric_strain'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz'
extra_vector_tags = 'ref'
[]
[clad]
block = clad
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain clad_irradiation_strain'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz'
extra_vector_tags = 'ref'
[]
[coating]
block = coating
strain = FINITE
eigenstrain_names = 'coating_thermal_eigenstrain'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz'
extra_vector_tags = 'ref'
[]
[]
[Kernels]
[gravity]
type = Gravity
variable = disp_y
value = -9.81
extra_vector_tags = 'ref'
[]
[heat]
type = HeatConduction
variable = temperature
extra_vector_tags = 'ref'
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
extra_vector_tags = 'ref'
[]
[heat_source]
type = NeutronHeatSource
variable = temperature
block = pellet
burnup_function = burnup
extra_vector_tags = 'ref'
[]
[]
[Burnup]
[burnup]
block = pellet
rod_ave_lin_pow = power_history
axial_power_profile = axial_peaking_factors
num_radial = 81
num_axial = 11
fuel_pin_geometry = pin_geometry
fuel_volume_ratio = 1.0
RPF = RPF
[]
[]
[AuxKernels]
[fast_neutron_flux]
type = FastNeutronFluxAux
variable = fast_neutron_flux
block = clad
rod_ave_lin_pow = power_history
axial_power_profile = axial_peaking_factors
factor = 3e13
execute_on = timestep_begin
[]
[fast_neutron_fluence]
type = FastNeutronFluenceAux
variable = fast_neutron_fluence
block = clad
fast_neutron_flux = fast_neutron_flux
execute_on = timestep_begin
[]
[grain_radius]
type = GrainRadiusAux
block = pellet
variable = grain_radius
temperature = temperature
execute_on = linear
[]
[hoop_stress]
type = RankTwoScalarAux
rank_two_tensor = stress
variable = hoop_stress
scalar_type = HoopStress
execute_on = timestep_end
[]
[total_hoop_strain]
type = RankTwoScalarAux
rank_two_tensor = total_strain
variable = total_hoop_strain
scalar_type = HoopStress
execute_on = timestep_end
[]
[creep_strain_hoop]
type = RankTwoScalarAux
rank_two_tensor = creep_strain
variable = creep_strain_hoop
scalar_type = HoopStress
block = clad
execute_on = timestep_end
[]
[conductance]
type = MaterialRealAux
property = gap_conductance
variable = gap_cond
boundary = 10
[]
[coolant_htc]
type = MaterialRealAux
property = coolant_channel_htc
variable = coolant_htc
boundary = 2
[]
[]
[Contact]
[pellet_clad_mechanical]
primary = 5
secondary = 10
normal_smoothing_distance = 0.1
penalty = 1e7
[]
[]
[ThermalContact]
[thermal_contact]
type = GasGapHeatTransfer
variable = temperature
primary = 5
secondary = 10
initial_moles = initial_moles
gas_released = fis_gas_released
contact_pressure = contact_pressure
quadrature = true
[]
[]
[BCs]
[no_x_all]
type = DirichletBC
variable = disp_x
boundary = 12
value = 0.0
[]
[no_y_clad_bottom]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[]
[no_y_fuel_bottom]
type = DirichletBC
variable = disp_y
boundary = 1020
value = 0.0
[]
[Pressure]
[coolantPressure]
boundary = '1 2 3'
function = pressure_ramp
[]
[]
[PlenumPressure]
[plenumPressure]
boundary = 9
initial_pressure = 2.0e6
startup_time = 0
R = 8.3143
output_initial_moles = initial_moles
temperature = ave_temp_interior
volume = gas_volume
material_input = fis_gas_released
output = plenum_pressure
[]
[]
[]
[CoolantChannel]
[convective_clad_surface]
boundary = '1 2 3'
variable = temperature
inlet_temperature = 580
inlet_pressure = pressure_ramp
inlet_massflux = mass_flux_func
rod_diameter = 9.54e-3
rod_pitch = 1.26e-2
linear_heat_rate = power_history
axial_power_profile = axial_peaking_factors
oxide_thickness = oxide_thickness
[]
[]
[Materials]
# Fuel
[fuel_thermal]
type = UO2Thermal
block = pellet
thermal_conductivity_model = NFIR
temperature = temperature
burnup_function = burnup
[]
[fuel_elasticity_tensor]
type = ComputeIsotropicElasticityTensor
block = pellet
youngs_modulus = 2.0e11
poissons_ratio = 0.345
[]
[elastic_stress]
type = ComputeSmearedCrackingStress
block = pellet
cracking_stress = 1.68e8
inelastic_models = 'fuel_creep'
softening_models = exponential_softening
shear_retention_factor = 0.1
max_stress_correction = 0
cracked_elasticity_type = DIAGONAL
output_properties = crack_damage
outputs = exodus
[]
[exponential_softening]
type = ExponentialSoftening
[]
[fuel_creep]
type = UO2CreepUpdate
block = pellet
burnup_function = burnup
temperature = temperature
[]
[fuel_relocation]
type = UO2RelocationEigenstrain
block = pellet
burnup_function = burnup
rod_ave_lin_pow = power_history
axial_power_profile = axial_peaking_factors
fuel_pin_geometry = 'pin_geometry'
relocation_activation1 = 5000
relocation_model = ESCORE_modified
eigenstrain_name = fuel_relocation_strain
[]
[fuel_thermal_expansion]
type = UO2ThermalExpansionMATPROEigenstrain
block = pellet
temperature = temperature
stress_free_temperature = 295.0
eigenstrain_name = fuel_thermal_strain
[]
[fuel_volumetric_swelling]
type = UO2VolumetricSwellingEigenstrain
gas_swelling_model_type = SIFGRS
block = pellet
temperature = temperature
burnup_function = burnup
initial_fuel_density = 10431.0
eigenstrain_name = fuel_volumetric_strain
[]
[fission_gas_release]
type = UO2Sifgrs
block = pellet
temperature = temperature
burnup_function = burnup
grain_radius = grain_radius
gbs_model = true
[]
[fuel_density]
type = Density
block = pellet
[]
# Clad
[clad_thermal]
type = ZryThermal
temperature = temperature
block = clad
[]
[clad_elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 7.5e10
poissons_ratio = 0.3
block = clad
[]
[clad_stress]
type = ComputeMultipleInelasticStress
tangent_operator = elastic
inelastic_models = 'clad_zrycreep clad_plasticity'
block = clad
[]
[clad_zrycreep]
type = ZryCreepLimbackHoppeUpdate
block = clad
temperature = temperature
fast_neutron_flux = fast_neutron_flux
fast_neutron_fluence = fast_neutron_fluence
model_irradiation_creep = true
model_primary_creep = true
model_thermal_creep = true
max_inelastic_increment = 1e-4
zircaloy_material_type = stress_relief_annealed
[]
[thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = clad
temperature = temperature
stress_free_temperature = 295.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[irradiation_swelling]
type = ZryIrradiationGrowthEigenstrain
block = clad
fast_neutron_fluence = fast_neutron_fluence
zircaloy_material_type = stress_relief_annealed
eigenstrain_name = clad_irradiation_strain
[]
[clad_plasticity]
type = ZryPlasticityUpdate
block = clad
temperature = temperature
fast_neutron_flux = fast_neutron_flux
fast_neutron_fluence = fast_neutron_fluence
cold_work_factor = 0.5
plasticity_model_type = MATPRO
zircaloy_alloy_type = 4
[]
[clad_density]
type = Density
block = clad
density = 6511.0
[]
# Coating
[coat_thermal]
type = ChromiumThermal
block = coating
temperature = temperature
[]
[coating_elasticity_tensor]
type = ChromiumElasticityTensor
temperature = temperature
block = coating
[]
[coat_stress]
type = ComputeMultipleInelasticStress
tangent_operator = elastic
inelastic_models = 'coat_creep coat_plasticity'
block = coating
[]
[coat_creep]
type = ChromiumCreepUpdate
temperature = temperature
block = coating
[]
[coat_plasticity]
type = ChromiumPlasticityUpdate
temperature = temperature
block = coating
fast_neutron_fluence = 0.0
hardening_constant = 2e9
[]
[coat_thermal_expansion]
type = ChromiumThermalExpansionEigenstrain
block = coating
temperature = temperature
stress_free_temperature = 293.0
eigenstrain_name = coating_thermal_eigenstrain
[]
[density_coat]
type = Density
block = coating
density = 7190.0
[]
[]
[Dampers]
[limitT]
type = BoundingValueNodalDamper
max_value = 3200.0
min_value = 293.0
variable = temperature
[]
[limitX]
type = MaxIncrement
max_increment = 1e-5
variable = disp_x
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package -ksp_gmres_restart'
petsc_options_value = 'lu superlu_dist 51'
line_search = 'none'
l_max_its = 100
l_tol = 8e-3
nl_max_its = 25
nl_rel_tol = 1e-5
nl_abs_tol = 1e-10
start_time = -200
n_startup_steps = 1
end_time = 5e7
dtmax = 1e6
dtmin = 1
[TimeStepper]
type = IterationAdaptiveDT
dt = 2.0e2
force_step_every_function_point = true
timestep_limiting_function = power_history
max_function_change = 5e5
optimal_iterations = 10
iteration_window = 2
linear_iteration_ratio = 100
growth_factor = 2.0
timestep_limiting_postprocessor = material_timestep
[]
[Quadrature]
order = FIFTH
side_order = SEVENTH
[]
[]
[Postprocessors]
[ave_temp_interior]
type = SideAverageValue
boundary = 9
variable = temperature
execute_on = 'initial linear'
[]
[avg_clad_temp]
type = SideAverageValue
boundary = 7
variable = temperature
[]
[fis_gas_produced]
type = ElementIntegralFisGasGeneratedSifgrs
block = pellet
[]
[fis_gas_released]
type = ElementIntegralFisGasReleasedSifgrs
block = pellet
[]
[fis_gas_grain]
type = ElementIntegralFisGasGrainSifgrs
block = pellet
[]
[fis_gas_boundary]
type = ElementIntegralFisGasBoundarySifgrs
block = pellet
[]
[gas_volume]
type = InternalVolume
boundary = 9
execute_on = 'initial linear'
[]
[_dt]
type = TimestepSize
[]
[num_lin_it]
type = NumLinearIterations
[]
[num_nonlin_it]
type = NumNonlinearIterations
[]
[tot_lin_it]
type = CumulativeValuePostprocessor
postprocessor = num_lin_it
[]
[tot_nonlin_it]
type = CumulativeValuePostprocessor
postprocessor = num_nonlin_it
[]
[alive_time]
type = PerfGraphData
section_name = Root
data_type = TOTAL
[]
[rod_total_power]
type = ElementIntegralPower
variable = temperature
burnup_function = burnup
block = pellet
[]
[alhr_input]
type = FunctionValuePostprocessor
function = power_history
[]
[average_burnup]
type = ElementAverageValue
block = pellet
variable = burnup
[]
[oxide_thickness]
type = ElementExtremeValue
block = clad
variable = oxide_thickness
[]
[fis_gas_percent]
type = FGRPercent
fission_gas_released = fis_gas_released
fission_gas_generated = fis_gas_produced
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = clad
[]
[]
[Outputs]
perf_graph = true
time_step_interval = 1
exodus = true
csv = true
print_linear_residuals = true
color = false
[console]
type = Console
max_rows = 25
[]
[]
(assessment/LWR/validation/LOCA_ANL_cladding_burst_tests/analysis/OCL5_8/OCL5_8_ad.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
displacements = 'disp_x disp_y'
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
[]
[Mesh]
coord_type = RZ
[smeared_pellet_mesh]
type = FuelPinMeshGenerator
pellet_quantity = 1
pellet_height = 0.270
pellet_outer_radius = 4.78e-3
clad_bot_gap_height = 0.001
clad_top_gap_height = 0.013
clad_thickness = 0.71e-3
clad_gap_width = 0.1e-3
pellet_mesh_density = coarse
clad_mesh_density = coarse
elem_type = QUAD8
[]
patch_size = 10
patch_update_strategy = auto
partitioner = centroid
centroid_partitioner_direction = y
[]
[Variables]
[temperature]
initial_condition = 300.0
[]
[]
[Functions]
[temperature_func]
type = PiecewiseLinear
x = '0 496.02 520.74 528.12 545.94 551.28 671.52 885.3 1195.74 1410.36 1657.86 1680 1690 1700 1710 1720 1730 1740 1750 1760 1770 1780 1790 1800 1810 1820 1830 1840 1848'
y = '300 300 405.465 482.048 583.351 632.287 634.297 632.825 630.378 631.059 632.59 633 683 733 783 833 883 933 983 1033 1083 1133 1183 1233 1283 1333 1383 1433 1477'
[]
[temperature_profile]
type = PiecewiseBilinear
data_file = 'temp_profile.csv'
axis = 1
[]
[cladding_temperature]
type = CompositeFunction
functions = 'temperature_func temperature_profile'
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[pellets]
block = pellet
use_automatic_differentiation = true
add_variables = true
strain = FINITE
decomposition_method = TaylorExpansion
eigenstrain_names = 'fuel_thermal_strain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
generate_output = 'vonmises_stress hydrostatic_stress stress_xx stress_yy
stress_zz strain_xx strain_yy strain_zz hoop_stress'
extra_vector_tags = 'ref'
[]
[clad]
block = clad
use_automatic_differentiation = true
add_variables = true
strain = FINITE
decomposition_method = TaylorExpansion
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz hoop_stress'
extra_vector_tags = 'ref'
[]
[]
[AuxVariables]
[creep_rate_aux]
order = CONSTANT
family = MONOMIAL
block = clad
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
block = clad
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
block = clad
[]
[burst_stress]
order = CONSTANT
family = MONOMIAL
block = clad
[]
[burst]
order = CONSTANT
family = MONOMIAL
block = clad
[]
[]
[Kernels]
[heat]
type = ADHeatConduction
variable = temperature
extra_vector_tags = 'ref'
[]
[heat_ie]
type = ADHeatConductionTimeDerivative
variable = temperature
extra_vector_tags = 'ref'
[]
[]
[AuxKernels]
[creep_rate_aux]
type = ADMaterialRealAux
variable = creep_rate_aux
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = ADMaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
block = clad
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = clad_outside_right
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = clad_outside_right
execute_on = timestep_end
[]
[]
[ThermalContact]
[thermal_contact]
type = GapHeatTransfer
primary = 5
secondary = 10
variable = temperature
gap_conductivity = 0.15 # k of He per Netzsch
[]
[]
[BCs]
[clad_surface_temperature]
type = ADFunctionDirichletBC
variable = temperature
boundary = '2'
function = cladding_temperature
[]
[no_x_all]
type = ADDirichletBC
variable = disp_x
boundary = 12
value = 0.0
[]
[no_y_clad_bottom]
type = ADDirichletBC
variable = disp_y
boundary = '1'
value = 0.0
[]
[no_y_fuel_bottom]
type = ADDirichletBC
variable = disp_y
boundary = '1020'
value = 0.0
[]
[Pressure]
[outer_pressure]
boundary = '1 2 3'
factor = 101325
[]
[inner_pressure]
boundary = '4 5 6'
factor = 8.28e6
[]
[]
[]
[PlenumTemperature]
[plenum_temp]
boundary = 5
inner_surfaces = '5'
outer_surfaces = '10'
temperature = temperature
[]
[]
[Materials]
[fuel_thermal]
type = ADHeatConductionMaterial
block = pellet
thermal_conductivity = 3.5
specific_heat = 330.0
[]
[fuel_elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
block = pellet
youngs_modulus = 2.0e11
poissons_ratio = 0.345
[]
[fuel_elastic_stress]
type = ADComputeFiniteStrainElasticStress
block = pellet
[]
[fuel_thermal_expansion]
type = ADComputeThermalExpansionEigenstrain
block = pellet
thermal_expansion_coeff = 10.0e-6
temperature = temperature
stress_free_temperature = 300.0
eigenstrain_name = fuel_thermal_strain
[]
[fuel_density]
type = ADDensity
block = pellet
density = 10980.0 #perfectly dense UO2
[]
[clad_thermal]
type = ADZryThermal
block = clad
temperature = temperature
[]
[clad_elasticity_tensor]
type = ADZryElasticityTensor
block = clad
matpro_youngs_modulus = false
matpro_poissons_ratio = false
[]
[clad_stress]
type = ADComputeMultipleInelasticStress
inelastic_models = 'clad_zrycreep'
block = clad
[]
[hill_constants]
type = ADHillConstants
hill_constants = "0.5 0.5 0.5 1.0 1.0 1.0"
#hill_constants = "0.738 0.174 0.588 1.0 1.0 1.0"
#function_names = "F G H L M N"
[]
[clad_zrycreep]
type = ADZryAnisoCreepLOCAUpdate
block = clad
temperature = temperature
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
temperature_loca_creep_begin = 301
temperature_standard_thermal_creep_end = 300
fract_beta_phase_name = 'ad_fract_beta_phase'
[]
[thermal_expansion]
type = ADZryThermalExpansionMATPROEigenstrain
block = clad
temperature = temperature
stress_free_temperature = 300.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[clad_density]
type = ADDensity
block = clad
density = 6550.0
[]
[phase]
type = ZrPhase
block = clad
temperature = temperature
numerical_method = 2
[]
[phase_converter]
type = MaterialADConverter
block = clad
reg_props_in = 'fract_beta_phase'
ad_props_out = 'ad_fract_beta_phase'
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = clad_outside_right
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate_aux
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
verbose = true
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.0e-04
nl_abs_tol = 1.0e-08
start_time = 0
n_startup_steps = 1
end_time = 1800.0
dtmax = 100
dtmin = 0.0001
[TimeStepper]
type = IterationAdaptiveDT
timestep_limiting_postprocessor = material_timestep
dt = 10.0
time_dt = '100 10'
time_t = '10 400'
[]
[]
[Postprocessors]
[ave_clad_temp]
type = SideAverageValue
boundary = clad_outside_right
variable = temperature
[]
[gas_volume]
type = InternalVolume
boundary = 9
execute_on = 'initial linear'
[]
[max_clad_temp]
type = NodalExtremeValue
block = clad
value_type = max
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = clad
[]
[max_hoop_stress]
type = ElementExtremeValue
block = clad
value_type = max
variable = hoop_stress
[]
[vonmises_stress_clad]
type = ElementAverageValue
block = clad
variable = vonmises_stress
[]
[min_burst_stress]
type = ElementExtremeValue
block = clad
value_type = min
variable = burst_stress
[]
[burst]
type = ElementExtremeValue
block = clad
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = clad
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
[]
[PerformanceMetricOutputs]
[]
[Outputs]
exodus = true
csv = true
color = false
perf_graph = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
show = 'max_clad_temp max_hoop_stress vonmises_stress_clad'
execute_on = 'FINAL'
[]
[]
[UserObjects]
[terminator1]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
[]
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-14/puzry-14.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-14.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 2500. '
y = '1.e+05 1.e+05 1.795e+07' # Linear increase at 0.1190 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 2500. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = EigenSolution
[]
[]
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = MaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = FunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = DirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = DirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1.e+11
poissons_ratio = 0.3
block = 1
[]
[creep_update]
type = ZryCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 1.e-04
temperature = temperature
temperature_standard_thermal_creep_end = 700
temperature_loca_creep_begin = 900.
[]
[creep]
type = ComputeMultipleInelasticStress
block = 1
tangent_operator = elastic
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = Density
block = 1
[]
[phase]
type = ZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
active = 'smp'
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0.
n_startup_steps = 1
end_time = 2500.
dtmax = 1.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-14_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-04/puzry-04.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-04.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 2000. '
y = '1.e+05 1.e+05 7.2e+05' # Linear increase at 0.0062 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 2000. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = EigenSolution
[]
[]
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = MaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = FunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = DirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = DirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1.e+11
poissons_ratio = 0.3
block = 1
[]
[creep_update]
type = ZryCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 1.e-04
temperature = temperature
temperature_standard_thermal_creep_end = 700
temperature_loca_creep_begin = 900.
[]
[creep]
type = ComputeMultipleInelasticStress
block = 1
tangent_operator = elastic
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = Density
block = 1
[]
[phase]
type = ZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
active = 'smp'
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0.
n_startup_steps = 1
end_time = 2000.
dtmax = 1.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-04_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-28/puzry-28.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-28.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 2500. '
y = '1.e+05 1.e+05 6.475e+06' # Linear increase at 0.0425 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 2500. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = EigenSolution
[]
[]
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = MaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = FunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = DirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = DirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1.e+11
poissons_ratio = 0.3
block = 1
[]
[creep_update]
type = ZryCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 1.e-04
temperature = temperature
temperature_standard_thermal_creep_end = 700
temperature_loca_creep_begin = 900.
[]
[creep]
type = ComputeMultipleInelasticStress
block = 1
tangent_operator = elastic
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = Density
block = 1
[]
[phase]
type = ZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
active = 'smp'
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0.
n_startup_steps = 1
end_time = 2500.
dtmax = 1.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-28_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(test/tests/zry_oxidation_cladding/oxide_coolant_couple.i)
################################################################################
#
# This case is prepared to test coupling coolant channel model with Zry Oxide
# corrosion model
#
# The test case is a segment of fuel clad with an axial length of 0.3 meter and
# a diameter of 1.10 cm; rod-to-rod pitch is 1.26 cm; inlet temperature is 553 K;
# heat flux at cladding OD is 578745.25 W/m^2.
#
# The geometry clad_rz_short_rev2.e has:
# Number of dimensions = 2
# Number of element blocks = 1
# Number of sidesets = 4
# Number of nodesets = 0
# Number of bc sets = 1
# Number of elements = 10
# Number of nodes = 18
#
# Number of elements in radial direction = 2
# Number of elements in axial direction = 5
#
# In considering the corrosion effects, an effective heat transfer coefficent
# is derived; when used in the CoolantChannel model, the temperature at cladding
# ID is same as the temperature in heat conduction through layered structure of
# zry and zirconium oxide.
#
# This simulation is run for 3 days, using a time step of 1 day (86400 seconds).
# The hand calculations for normal operating temperature oxide thickness and total
# gained oxygen concentration are listed below for element 9 in the mesh.
#
# Time (days) oxide thickness (m) total oxygen concentration (kg/m^2)
# 1 1.784e-8 2.632e-5
# 2 3.689e-7 5.442e-4
# 3 4.649e-7 6.859e-4
#
# Because no oxygen concentration is gained in the metal (a low temperature
# assumption in the code), the total gained oxygen concentration is equal to the
# gained oxygen concentration in the scale oxide.
#
#--------------------------------------------------------------------------------
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = clad_rz_short_rev2.e
[]
[]
[DefaultElementQuality]
aspect_ratio_upper_bound = 241
[]
# Define dependent variables, element order and shape function family,
# and initial conditions
[Variables]
[temp]
order = FIRST
family = LAGRANGE
initial_condition = 300 # K, initial temperature
[]
[]
[AuxVariables]
[oxide_thickness]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[oxyconc2_scale] # Oxygen concentration in ZrO2 scale (kg/m**2)
order = CONSTANT
family = MONOMIAL
[]
[oxyconc2_metal] # Oxygen concentration in metal (kg/m**2)
order = CONSTANT
family = MONOMIAL
[]
[oxyconc2_total] # Total oxygen concentration (oxide + metal) (kg/m**2)
order = CONSTANT
family = MONOMIAL
[]
[]
[Kernels]
[heat] # gradient term in heat conduction equation
type = HeatConduction
variable = temp
[]
[heat_ie] # time term in heat conduction equation
type = HeatConductionTimeDerivative
variable = temp
[]
[]
[AuxKernels]
[oxide]
type = MaterialRealAux
variable = oxide_thickness
property = oxide_scale_thickness
boundary = 3
[]
[coolant_htc]
type = MaterialRealAux
property = coolant_channel_htc
variable = coolant_htc
boundary = 3
[]
[oconc_scale]
type = MaterialRealAux
variable = oxyconc2_scale
property = gained_oxygen_concentration_scale
boundary = 3
[]
[oconc_metal]
type = MaterialRealAux
variable = oxyconc2_metal
property = gained_oxygen_concentration_metal_wall
boundary = 3
[]
[oconc_total]
type = MaterialRealAux
variable = oxyconc2_total
property = gained_oxygen_concentration_total
boundary = 3
[]
[]
# Define boundary conditions
[BCs]
[clad_inner_surface]
type = NeumannBC
boundary = 1
value = 636619.77 # heat flux from fuel
variable = temp
[]
[top_clad]
type = NeumannBC
boundary = 2
value = 0
variable = temp
[]
[bottom_clad]
type = NeumannBC
boundary = 4
value = 0
variable = temp
[]
[]
[CoolantChannel]
# convective boundary condition at clad outer surface
[clad_outer_surface]
boundary = 3
variable = temp
inlet_temperature = 553 # K
inlet_pressure = 15.5E6 # Pa
inlet_massflux = 1000 # kg/m^2-sec
rod_diameter = 1.10e-2 # m
rod_pitch = 1.26e-2 # m
heat_flux = 578745.25 # W/m^2
heat_transfer_mode = 2 # D-B correlation
oxide_thickness = oxide_thickness # coupled oxide_thickness
[]
[]
[Materials]
[clad_thermal]
type = ZryThermal
block = 1
temperature = temp
[]
[density]
type = Density
block = 1
density = 6551.0 # kg/m^3
[]
[oxidation_zry]
type = ZryOxidation
boundary = 3
clad_inner_radius = 0
clad_outer_radius = 0
normal_operating_temperature_model = epri_kwu_ce
high_temperature_model = leistikow
use_coolant_channel = true
temperature = temp
# outputs = all
# output_properties = 'oxide_scale_thickness'
[]
[]
[Executioner]
type = Transient
# PETSC options
solve_type = 'PJFNK'
# controls for linear iterations
l_max_its = 200
l_tol = 1e-6 #8e-3
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-8
nl_abs_tol = 1e-10
# time control
start_time = 0.0
dt = 86400
end_time = 259200 # 3 days
[]
[Postprocessors]
[oxide_thickness] #
type = ElementalVariableValue
variable = oxide_thickness
elementid = 9
[]
[oxyconc2_scale]
type = ElementalVariableValue
elementid = 9
variable = oxyconc2_scale
[]
[oxyconc2_metal]
type = ElementalVariableValue
elementid = 9
variable = oxyconc2_metal
[]
[oxyconc2_total]
type = ElementalVariableValue
elementid = 9
variable = oxyconc2_total
[]
[]
# Define output file(s)
[Outputs]
exodus = true
file_base = oxide_coolant_coupled_out
[]
(assessment/LWR/validation/RIA_CABRI_REP_Na4/analysis/REP_Na_4/RIA/REP_Na_4_RIA.i)
# REP Na 4 RIA
[GlobalParams]
density = 10476.35 # assumed TD = 10970
order = SECOND
family = LAGRANGE
energy_per_fission = 3.2e-11 # J/fission
displacements = 'disp_x disp_y'
[]
[Problem]
coord_type = RZ
type = AugmentedLagrangianContactProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
maximum_lagrangian_update_iterations = 200
acceptable_iterations = 30
acceptable_multiplier = 10
[]
[Mesh]
patch_size = 40
#patch_update_strategy = auto
#partitioner = centroid
#centroid_partitioner_direction = y
[mesh]
type = FileMeshGenerator
file = REP_Na4.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temp]
[]
[]
[UserObjects]
[pin_geometry]
type = FuelPinGeometry
clad_inner_wall = 5
clad_outer_wall = 2
clad_top = 3
clad_bottom = 1
pellet_exteriors = 8
[]
[]
[AuxVariables]
[fast_neutron_flux]
block = 'clad'
[]
[fast_neutron_fluence]
block = 'clad'
[]
[grain_radius]
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
[]
[gap_cond]
order = CONSTANT
family = MONOMIAL
[]
[fuel_cond]
order = CONSTANT
family = MONOMIAL
[]
[swelling_strain]
order = CONSTANT
family = MONOMIAL
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
[]
[hoop_creep_strain]
order = CONSTANT
family = MONOMIAL
[]
[axial_creep_strain]
order = CONSTANT
family = MONOMIAL
[]
[hoop_plastic_strain]
order = CONSTANT
family = MONOMIAL
[]
[axial_plastic_strain]
order = CONSTANT
family = MONOMIAL
[]
[total_hoop_strain]
order = CONSTANT
family = MONOMIAL
[]
[total_axial_strain]
order = CONSTANT
family = MONOMIAL
[]
[hoop_elastic_strain]
order = CONSTANT
family = MONOMIAL
[]
[axial_elastic_strain]
order = CONSTANT
family = MONOMIAL
[]
[clad_coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[coolant_temp]
order = CONSTANT
family = MONOMIAL
[]
[clad_coolant_flux]
order = CONSTANT
family = MONOMIAL
[]
[coolant_channel_hmode]
order = CONSTANT
family = MONOMIAL
[]
[coolant_channel_htype]
order = CONSTANT
family = MONOMIAL
[]
[critical_heat_flux]
order = CONSTANT
family = MONOMIAL
[]
[oxide_thickness]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[plastic_strain_mag]
order = CONSTANT
family = MONOMIAL
block = 'clad'
[]
[SED]
order = CONSTANT
family = MONOMIAL
block = 'clad'
[]
[oxywtfract_total]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfgain_total]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[]
[Functions]
[power_profile]
type = PiecewiseLinear # reads and interpolates an input file containing rod average linear power vs time
data_file = REPNa4_power_history_Full.csv
format = columns
scale_factor = 1
[]
[axial_peaking_factors] # reads and interpolates an input file containing the axial power profile vs time
type = PiecewiseBilinear
data_file = REPNa4_axial_peaking_Full.csv
scale_factor = 1
axis = 1
[]
[pressure_ramp] # inlet coolant pressure evolution
type = PiecewiseLinear
format = columns
scale_factor = 1.0
xy_data = '0 101325
8640 15499970
124675200 15499970
124718400 101325
125193600 101325
125193610 101325
125193650 500008
125193700 500008
125193900 500008
125194000 101325
125194100 101325'
[]
[temp_ramp] # inlet coolant temp evolution
type = PiecewiseLinear
format = columns
scale_factor = 1.0
xy_data = '0 293.15
8640 591
20476800 591
21859200 600
47692800 600
51840000 593
72144000 593
73440000 586
96940800 586
99360000 583
124675200.0 583
124761600.0 293.150
125193600.0 293.150
125193650.0 553.150
125193900.0 553.150
125194000.0 293.150
125194100.0 293.150'
[]
[burnup_GWd]
type = ParsedFunction
expression = bu*950
symbol_names = 'bu'
symbol_values = 'average_burnup'
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[pellets]
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
strain = FINITE
eigenstrain_names = 'fuel_thermal_strain fuel_relocation_strain
fuel_volumetric_strain'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz axial_stress'
extra_vector_tags = 'ref'
[]
[clad]
block = 'clad'
strain = FINITE
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
eigenstrain_names = 'clad_thermal_eigenstrain clad_irradiation_strain'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz plastic_strain_xx plastic_strain_yy plastic_strain_zz
creep_strain_xx creep_strain_yy creep_strain_zz elastic_strain_xx
elastic_strain_yy elastic_strain_zz hoop_stress axial_stress'
extra_vector_tags = 'ref'
[]
[]
[Kernels]
[heat] # gradient term in heat conduction equation
type = HeatConduction
variable = temp
extra_vector_tags = 'ref'
[]
[heat_ie] # time term in heat conduction equation
type = HeatConductionTimeDerivative
variable = temp
extra_vector_tags = 'ref'
[]
[heat_source_fuel] # source term in heat conduction equation
type = NeutronHeatSource
variable = temp
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
burnup_function = burnup
extra_vector_tags = 'ref'
[]
[]
[Burnup]
[burnup]
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
rod_ave_lin_pow = power_profile
axial_power_profile = axial_peaking_factors
num_radial = 80
num_axial = 11
a_upper = 0.5678974
a_lower = 0.0045
fuel_inner_radius = 0
fuel_outer_radius = 0.0040959
fuel_volume_ratio = 1
isotopes = 'U235 U238 Pu239 Pu240 Pu241 Pu242'
isotope_fractions = '0.0449 0.9551 0 0 0 0'
RPF = RPF
order = CONSTANT
family = MONOMIAL
[]
[]
[AuxKernels]
[fast_neutron_flux]
type = FastNeutronFluxAux
variable = fast_neutron_flux
axial_power_profile = axial_peaking_factors
rod_ave_lin_pow = power_profile
factor = 3e13 #n/m2-s
block = 'clad'
execute_on = timestep_begin
[]
[fast_neutron_fluence]
type = FastNeutronFluenceAux
variable = fast_neutron_fluence
fast_neutron_flux = fast_neutron_flux
block = 'clad'
execute_on = timestep_begin
[]
[grain_radius]
type = GrainRadiusAux
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
variable = grain_radius
temperature = temp
execute_on = linear
[]
[gap_conductance]
type = MaterialRealAux
property = gap_conductance
variable = gap_cond
boundary = 10
[]
[fuel_conductance]
type = MaterialRealAux
property = thermal_conductivity
variable = fuel_cond
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
[]
[swelling_strain]
type = MaterialRealAux
property = volumetric_swelling_strain
variable = swelling_strain
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
[]
[vonmises_stress]
type = RankTwoScalarAux
rank_two_tensor = stress
variable = vonmises_stress
scalar_type = VonMisesStress
execute_on = timestep_end
[]
[hoop_creep_strain]
type = RankTwoAux
rank_two_tensor = creep_strain
variable = hoop_creep_strain
index_i = 2
index_j = 2
execute_on = timestep_end
block = 'clad'
[]
[axial_creep_strain]
type = RankTwoAux
rank_two_tensor = creep_strain
variable = axial_creep_strain
index_i = 1
index_j = 1
execute_on = timestep_end
block = 'clad'
[]
[hoop_plastic_strain]
type = RankTwoAux
rank_two_tensor = plastic_strain
variable = hoop_plastic_strain
index_i = 2
index_j = 2
execute_on = timestep_end
block = 'clad'
[]
[axial_plastic_strain]
type = RankTwoAux
rank_two_tensor = plastic_strain
variable = axial_plastic_strain
index_i = 1
index_j = 1
execute_on = timestep_end
block = 'clad'
[]
[total_hoop_strain]
type = RankTwoAux
rank_two_tensor = total_strain
variable = total_hoop_strain
index_i = 2
index_j = 2
execute_on = timestep_end
block = 'clad'
[]
[total_axial_strain]
type = RankTwoAux
rank_two_tensor = total_strain
variable = total_axial_strain
index_i = 1
index_j = 1
execute_on = timestep_end
block = 'clad'
[]
[hoop_elastic_strain]
type = RankTwoAux
rank_two_tensor = elastic_strain
variable = hoop_elastic_strain
index_i = 2
index_j = 2
execute_on = timestep_end
block = 'clad'
[]
[axial_elastic_strain]
type = RankTwoAux
rank_two_tensor = elastic_strain
variable = axial_elastic_strain
index_i = 1
index_j = 1
execute_on = timestep_end
block = 'clad'
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
block = clad
execute_on = timestep_end
[]
[plastic_strain_mag]
type = MaterialRealAux
property = effective_plastic_strain
variable = plastic_strain_mag
block = clad
execute_on = timestep_end
[]
[clad_coolant_htc]
type = MaterialRealAux
property = coolant_channel_htc
variable = clad_coolant_htc
boundary = 2
[]
[coolant_temp]
type = MaterialRealAux
property = coolant_temperature
variable = coolant_temp
boundary = 2
[]
[clad_coolant_flux]
type = MaterialRealAux
property = output_heat_flux
variable = clad_coolant_flux
boundary = 2
[]
[coolant_channel_hmode]
type = MaterialRealAux
property = coolant_channel_hmode
variable = coolant_channel_hmode
boundary = 2
[]
[coolant_channel_htype]
type = MaterialRealAux
property = coolant_channel_htype
variable = coolant_channel_htype
boundary = 2
[]
[critical_heat_flux]
type = MaterialRealAux
property = critical_heat_flux
variable = critical_heat_flux
boundary = 2
[]
[oxide]
type = MaterialRealAux
property = oxide_scale_thickness
variable = oxide_thickness
boundary = 2
[]
[SED]
type = MaterialRealAux
variable = SED
property = strain_energy_density
execute_on = timestep_end
[]
[ofract_total]
type = MaterialRealAux
property = current_oxygen_weight_frac_total
variable = oxywtfract_total
execute_on = timestep_end
boundary = 2
[]
[ofgain_total]
type = MaterialRealAux
property = oxygen_weight_frac_gained_total
variable = oxywtfgain_total
execute_on = timestep_end
boundary = 2
[]
[fract_bphase]
type = MaterialRealAux
property = fract_beta_phase
variable = fract_beta_phase
block = 'clad'
[]
[]
# Define mechanical contact between the fuel (sideset=10) and the clad (sideset=5)
[Contact]
[pellet_clad_mechanical]
primary = 5
secondary = 210 #10
penalty = 1e9
model = coulomb
formulation = augmented_lagrange
friction_coefficient = 0.3
tangential_tolerance = 1e-3
normal_smoothing_distance = 0.1
al_penetration_tolerance = 1e-6
al_incremental_slip_tolerance = 1e-6
al_frictional_force_tolerance = 5e-2
[]
[pellet_clad_mechanical_2]
primary = 5
secondary = 410
penalty = 1e9
model = coulomb
formulation = augmented_lagrange
friction_coefficient = 0.0
tangential_tolerance = 1e-3
normal_smoothing_distance = 0.1
al_penetration_tolerance = 1e-6
al_incremental_slip_tolerance = 1e-6
al_frictional_force_tolerance = 5e-2
[]
[]
# Define thermal contact between the fuel (sideset=10) and the clad (sideset=5)
[ThermalContact]
[thermal_contact]
type = GasGapHeatTransfer
variable = temp
primary = 5
secondary = 10
initial_moles = initial_moles # coupling to a postprocessor which supplies the initial plenum/gap gas mass
gas_released = fis_gas_released # coupling to a postprocessor which supplies the fission gas addition
jump_distance_model = LANNING
plenum_pressure = plenum_pressure
contact_pressure = contact_pressure
roughness_primary = 0.1e-6 #2.0e-6
roughness_secondary = 0.1e-6 #0.5e-6
roughness_coef = 3.2
normal_smoothing_distance = 0.1
quadrature = true
emissivity_primary = 0.800 #Emissivity for fuel
emissivity_secondary = 0.325 #Emissivity for clad
refab_time = 125107200
refab_gas_types = He
refab_fractions = 1
contact_coef = 20 #10 default
[]
[]
[BCs]
# pin pellets and clad along axis of symmetry (y)
[no_x_all]
type = DirichletBC
variable = disp_x
boundary = 12
value = 0.0
[]
# pin clad bottom in the axial direction (y)
[no_y_clad_bottom]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[]
# pin fuel bottom in the axial direction (y)
[no_y_fuel_bottom]
type = DirichletBC
variable = disp_y
boundary = 20
value = 0.0
[]
[Pressure]
# apply coolant pressure on clad outer walls
[coolantPressure]
boundary = '1 2 3'
factor = 1
function = pressure_ramp # use the pressure_ramp function defined above
[]
[]
[PlenumPressure]
# apply plenum pressure on clad inner walls and pellet surfaces
[plenumPressure]
boundary = 9
initial_temperature = 293.15
initial_pressure = 2.60e6
startup_time = 0
R = 8.3143
output_initial_moles = initial_moles # coupling to post processor to get initial fill gas mass
temperature = ave_temp_interior #plenumTemp
volume = gas_volume # coupling to post processor to get gas volume
material_input = fis_gas_released # coupling to post processor to get fission gas added
output = plenum_pressure # coupling to post processor to output plenum/gap pressure
displacements = 'disp_x disp_y'
# extra_vector_tags = 'ref'
refab_time = 125107200
refab_pressure = 0.301e6
refab_temperature = 293.15
refab_volume = 2.0e-6
[]
[]
[]
[CoolantChannel]
# [convective_clad_surface_water] # apply convective boundary to clad outer surface
# boundary = '1 2 3'
# variable = temp
# inlet_temperature = temp_ramp # K
# inlet_pressure = pressure_ramp # Pa
# inlet_massflux = 3244.044104 # kg/m^2-sec
# rod_diameter = 0.00951 # m
# rod_pitch = 1.26e-2 # m
# coolant_material = 'water'
# compute_enthalpy = true
# oxide_thickness = oxide_thickness # coupled oxide_thickness
# number_axial_zone = 50
# []
#
[convective_clad_surface] # apply convective boundary to clad outer surface
boundary = '1 2 3'
variable = temp
inlet_temperature = temp_ramp # K
inlet_pressure = pressure_ramp # Pa
inlet_massflux = 3533 # kg/m^2-sec Based on flow rate provided and flow area and estimated density of 885.1 kg/m^3
flow_area = 8.74855e-5 #m^2
heated_diameter = 1.172526e-2 #m
hydraulic_diameter = 4.7e-3 #m
heated_perimeter = 2.984513e-2 #m
coolant_material = 'sodium'
compute_enthalpy = true
heat_transfer_mode = 0
oxide_thickness = oxide_thickness # coupled oxide_thickness
number_axial_zone = 50
rod_diameter = 0.0095 # m
htc_correlation_type = 2
[]
[]
[Materials]
[fuel_density]
type = Density
#density = 10476.35
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
[]
[fuel_thermal]
type = UO2Thermal
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
temperature = temp
burnup_function = burnup
thermal_conductivity_model = NFIR
initial_porosity = 0.045
[]
[fuel_elasticity_tensor]
type = UO2ElasticityTensor
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
matpro_poissons_ratio = 1
matpro_youngs_modulus = 1
temperature = temp
[]
[fuel_elastic_stress]
type = ComputeFiniteStrainElasticStress
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
[]
[fuel_thermal_expansion]
type = UO2ThermalExpansionMATPROEigenstrain
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
temperature = temp
stress_free_temperature = 293.15
eigenstrain_name = fuel_thermal_strain
[]
[fuel_relocation]
type = UO2RelocationEigenstrain
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
burnup_function = burnup
rod_ave_lin_pow = power_profile
axial_power_profile = axial_peaking_factors
relocation_activation1 = 5000
burnup_relocation_stop = 0.0 #0.0208
relocation_model = ESCORE_modified
eigenstrain_name = fuel_relocation_strain
fuel_pin_geometry = 'pin_geometry'
[]
[fuel_volumetric_swelling]
type = UO2VolumetricSwellingEigenstrain
gas_swelling_model_type = SIFGRS
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
temperature = temp
burnup_function = burnup
initial_fuel_density = 10476.35
total_densification = 0.00675
initial_porosity = 0.045
eigenstrain_name = fuel_volumetric_strain
[]
[fission_gas_release]
type = UO2Sifgrs
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
temperature = temp
fission_rate = fission_rate
burnup_function = burnup
initial_porosity = 0.045
grain_radius_const = 5.0e-6
gbs_model = false
transient_option = MICROCRACKING_BURNUP
[]
[clad_density]
type = Density
block = 'clad'
density = 6550
[]
[clad_thermal]
type = ZryThermal
block = 'clad'
temperature = temp
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
temperature = temp
matpro_poissons_ratio = true
matpro_youngs_modulus = true
cold_work_factor = 0.5
fast_neutron_fluence = fast_neutron_fluence
block = 'clad'
[]
[clad_stress]
type = ComputeMultipleInelasticStress
tangent_operator = elastic
#inelastic_models = 'clad_zrycreep clad_zryplasticity'
inelastic_models = 'clad_zryplasticity'
block = 'clad'
[]
[clad_zrycreep]
type = ZryCreepLimbackHoppeUpdate
block = 'clad'
temperature = temp
fast_neutron_flux = fast_neutron_flux
fast_neutron_fluence = fast_neutron_fluence
#creeprate_scale_factor = 1
model_irradiation_creep = 1
model_primary_creep = 1
model_thermal_creep = 1
max_inelastic_increment = 0.0001
creeprate_scale_factor = 0
enable = 0
[]
[clad_zryplasticity]
type = ZryPlasticityUpdate
block = 'clad'
temperature = temp
fast_neutron_flux = fast_neutron_flux
fast_neutron_fluence = fast_neutron_fluence
cold_work_factor = 0.5
plasticity_model_type = MATPRO
zircaloy_alloy_type = 4
max_inelastic_increment = 0.0001
[]
[clad_thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = 'clad'
temperature = temp
stress_free_temperature = 293.15
eigenstrain_name = clad_thermal_eigenstrain
[]
[clad_irradiation_swelling]
type = ZryIrradiationGrowthEigenstrain
block = 'clad'
fast_neutron_fluence = fast_neutron_fluence
zircaloy_material_type = stress_relief_annealed
eigenstrain_name = clad_irradiation_strain
compute = 0
[]
[clad_oxidation]
type = ZryOxidation
boundary = 2
clad_inner_radius = 0.00417789
clad_outer_radius = 0.00475615
use_coolant_channel = true
temperature = temp
fast_neutron_flux = fast_neutron_flux
oxygen_weight_fraction_initial = 0.0012
[]
[phase]
type = ZrPhase
block = 'clad'
numerical_method = 2
temperature = temp
[]
[StrainEnergyDensity]
type = StrainEnergyDensity
block = 'clad'
incremental = 1
[]
[]
[Dampers]
[BoundingValueNodalDamper]
type = BoundingValueNodalDamper
max_value = 3200 # The maximum permissible iterative value for the variable.
min_value = 200 # The minimum permissible iterative value for the variable.
variable = temp # The name of the variable that this damper operates on
[]
[contact_slip]
type = ContactSlipDamper
primary = 5
secondary = 10
min_damping_factor = 0.05
[]
[]
[Preconditioning]
[SMP]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'contact'
contact_line_search_allowed_lambda_cuts = 0
contact_line_search_ltol = 0.5
verbose = true
l_max_its = 100
l_tol = 1e-3
nl_max_its = 40
nl_rel_tol = 1e-4
nl_abs_tol = 1e-10
start_time = 0
end_time = 125194100 #125193600 #125194100 is the end time for the RIA
dtmax = 10
dtmin = 1e-7
[TimeStepper]
type = IterationAdaptiveDT
dt = 10
optimal_iterations = 20
iteration_window = 4
linear_iteration_ratio = 100
timestep_limiting_function = power_profile
max_function_change = 5e5
force_step_every_function_point = true
timestep_limiting_postprocessor = material_timestep
time_t = '125193610 125193620 125193630 125193640 125193650 125193660 125193670 125193680'
time_dt = '10 10 10 10 10 10 10 10'
[]
[Quadrature]
order = FIFTH #SEVENTH
side_order = SEVENTH #Comment out if order = SEVENTH
[]
[]
[Postprocessors]
# [ave_temp_interior] # average temperature of the cladding interior and all pellet exteriors
# type = SideAverageValue
# boundary = 9 #For RIA the node number is ##***8479***##
# variable = temp
# execute_on = 'initial linear'
# []
[ave_temp_interior]
type = NodalVariableValue
variable = temp
nodeid = 8479
execute_on = 'initial linear'
[]
[clad_inner_vol] # volume inside of cladding
type = InternalVolume
boundary = 7
execute_on = 'initial linear'
[]
[avg_clad_temp] # average temperature of cladding interior
type = SideAverageValue
boundary = 7
variable = temp
execute_on = 'initial timestep_end'
[]
[max_fuel_temp]
type = NodalExtremeValue
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
value_type = max
variable = temp
execute_on = 'initial timestep_end'
[]
[min_fuel_temp]
type = NodalExtremeValue
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
value_type = min
variable = temp
execute_on = 'initial timestep_end'
[]
[max_clad_temp]
type = NodalExtremeValue
block = 'clad'
value_type = max
variable = temp
execute_on = 'initial timestep_end'
[]
[min_clad_temp]
type = NodalExtremeValue
block = 'clad'
value_type = min
variable = temp
execute_on = 'initial timestep_end'
[]
[fis_gas_generated]
type = ElementIntegralFisGasGeneratedSifgrs
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
[]
[fis_gas_released]
type = ElementIntegralFisGasReleasedSifgrs
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
[]
[fis_gas_grain]
type = ElementIntegralFisGasGrainSifgrs
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
outputs = exodus
[]
[fis_gas_boundary]
type = ElementIntegralFisGasBoundarySifgrs
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
outputs = exodus
[]
[gas_volume] # gas volume
type = InternalVolume
boundary = 9
execute_on = 'initial linear'
[]
[flux_from_clad] # area integrated heat flux from the cladding
type = SideDiffusiveFluxIntegral
variable = temp
boundary = 5
diffusivity = thermal_conductivity
[]
[flux_from_fuel] # area integrated heat flux from the fuel
type = SideDiffusiveFluxIntegral
variable = temp
boundary = 10
diffusivity = thermal_conductivity
[]
[1_rod_input_power]
type = FunctionValuePostprocessor
function = power_profile
[]
[3_burnup_GWd]
type = FunctionValuePostprocessor
function = burnup_GWd
[]
[fis_gas_percent]
type = FGRPercent
fission_gas_released = fis_gas_released
fission_gas_generated = fis_gas_generated
[]
[vonmises_stress_fuel]
type = ElementAverageValue
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
variable = vonmises_stress
[]
[vonmises_stress_clad]
type = ElementAverageValue
block = 'clad'
variable = vonmises_stress
[]
[z_average_RPF]
type = ElementAverageValue
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
variable = RPF
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = 'clad'
[]
## Nodal values
[FCT] #fuel centerline temperature
type = NodalVariableValue
variable = temp
nodeid = 3866 #(0, 0.303375, 0)
[]
[FST] #fuel surface temperature
type = NodalVariableValue
variable = temp
nodeid = 3823 #(0.0040959, 0.303375, 0)
[]
[CIST] #clad inner surface temperature
type = NodalVariableValue
variable = temp
nodeid = 9557 #(0.0041779, 0.305106, 0)
[]
[COST] #clad outer surface temperature
type = NodalVariableValue
variable = temp
nodeid = 9547 #(0.00475615, 0.305106, 0)
[]
[gap]
type = NodalVariableValue
variable = penetration
nodeid = 3823 #(0.0040959, 0.303375, 0)
use_displaced_mesh = true
[]
#######################################
[qpoint_penetration] #FOCE
type = ElementalVariableValue
variable = qpoint_penetration
elementid = 1200
use_displaced_mesh = 1
[]
[penetration] #FOCN
type = NodalVariableValue
variable = penetration
nodeid = 3823
use_displaced_mesh = 1
[]
[contact_pressure] #FOCN
type = NodalVariableValue
variable = contact_pressure
nodeid = 3823
use_displaced_mesh = 1
[]
[gap_cond] #FOCE
type = ElementalVariableValue
variable = gap_cond
elementid = 1200
use_displaced_mesh = 1
[]
[creep_hoop_strain] #COCE
type = ElementalVariableValue
variable = hoop_creep_strain
elementid = 2981
use_displaced_mesh = 1
[]
[elastic_hoop_strain] #COCE
type = ElementalVariableValue
variable = hoop_elastic_strain
elementid = 2981
use_displaced_mesh = 1
[]
[plastic_hoop_strain] #COCE
type = ElementalVariableValue
variable = hoop_plastic_strain
elementid = 2981
use_displaced_mesh = 1
[]
[total_hoop_strain] #COCE
type = ElementalVariableValue
variable = total_hoop_strain
elementid = 2981
use_displaced_mesh = 1
[]
[clad_hoop_stress] #COCE
type = ElementalVariableValue
variable = hoop_stress
elementid = 2981
use_displaced_mesh = 1
[]
[clad_axial_elongation] #COTN
type = NodalVariableValue
variable = disp_y
nodeid = 10755
use_displaced_mesh = 1
[]
[clad_oxide_thickness] #COCE
type = ElementalVariableValue
variable = oxide_thickness
elementid = 2981
use_displaced_mesh = 1
[]
[clad_coolant_htc] #COCE
type = ElementalVariableValue
variable = clad_coolant_htc
elementid = 2981
use_displaced_mesh = 1
[]
[coolant_temp] #COCE
type = ElementalVariableValue
variable = coolant_temp
elementid = 2981
use_displaced_mesh = 1
[]
[clad_coolant_flux] #COCE
type = ElementalVariableValue
variable = clad_coolant_flux
elementid = 2981
use_displaced_mesh = 1
[]
[coolant_channel_hmode] #COCE
type = ElementalVariableValue
variable = coolant_channel_hmode
elementid = 2981
use_displaced_mesh = 1
[]
[coolant_channel_htype] #COCE
type = ElementalVariableValue
variable = coolant_channel_htype
elementid = 2981
use_displaced_mesh = 1
[]
[critical_heat_flux] #COCE
type = ElementalVariableValue
variable = critical_heat_flux
elementid = 2981
use_displaced_mesh = 1
[]
[fuel_centerline_temp] #FICN
type = NodalVariableValue
variable = temp
nodeid = 3866
[]
[fuel_surface_temp] #FOCN
type = NodalVariableValue
variable = temp
nodeid = 3823
[]
[clad_inner_surface_temp] #CICN
type = NodalVariableValue
variable = temp
nodeid = 9557
[]
[clad_outer_surface_temp] #COCN
type = NodalVariableValue
variable = temp
nodeid = 9547
[]
[fuel_axial_elongation] #FOTN
type = NodalVariableValue
variable = disp_y
nodeid = 7739
[]
[clad_radial_elongation] #COCN
type = NodalVariableValue
variable = disp_x
nodeid = 9547
[]
[fuel_radial_elongation] #FOCN
type = NodalVariableValue
variable = disp_x
nodeid = 3823
[]
[SED_PPN_O] #COCE
type = ElementalVariableValue
variable = SED
elementid = 2981
use_displaced_mesh = 1
[]
[SED_PPN_I] #CICE
type = ElementalVariableValue
variable = SED
elementid = 2984
use_displaced_mesh = 1
[]
[zz_OFract_PPN_O] #COCE
type = ElementalVariableValue
variable = oxywtfract_total
elementid = 2981
use_displaced_mesh = 1
[]
[zz_OGain_PPN_O] #COCE
type = ElementalVariableValue
variable = oxywtfgain_total
elementid = 2981
use_displaced_mesh = 1
[]
#######################################
[max_clad_SED]
type = ElementExtremeValue
block = 'clad'
variable = SED
value_type = max
[]
#Post processor to calculate radial average enthalpy. This postprocessor isnt available yet in BISON
[z_RAE]
type = RadialAverageEnthalpy
vector_postprocessor = rad_temp
radial_direction = x
axial_direction = y
axial_position = 0.3
temperature_name = temp
[]
[peak_RAE]
type = TimeExtremeValue
postprocessor = z_RAE
[]
[]
[VectorPostprocessors]
[clad_dia]
type = NodalValueSampler
variable = disp_x
boundary = 2
sort_by = y
outputs = 'outfile_clad_diameter'
[]
[pellet_dia]
type = NodalValueSampler
variable = disp_x
boundary = 10
sort_by = y
outputs = 'outfile_pellet_diameter'
[]
#Location of peak power node at appoximately 0.3 m in mesh
[rad_temp]
type = NodalValueSampler
block = 3
sort_by = y
variable = temp
execute_on = timestep_end
outputs = 'outfile_radial_temp'
[]
[]
[StandardLWRFuelRodOutputs]
fuel_pellet_blocks = 'pellet_type_1 pellet_type_2 pellet_type_3'
temperature = temp
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
time_step_interval = 1
csv = true
#exodus = true
color = false
[outfile_clad_diameter]
type = CSV
sync_times = '125194100'
sync_only = true
[]
[outfile_pellet_diameter]
type = CSV
sync_times = '125194100'
sync_only = true
[]
[outfile_radial_temp]
type = CSV
end_time = -100000
[]
[console]
type = Console
output_linear = true
max_rows = 10
[]
[checkpoint]
type = Checkpoint
num_files = 2
file_base = recover_files
[]
[chkfile]
type = CSV
show = 'ave_temp_interior fis_gas_released FCT average_burnup peak_RAE'
execute_on = 'FINAL'
[]
[exodus]
type = Exodus
time_step_interval = 4
end_time = 125193700
[]
[exodus_RIA]
type = Exodus
time_step_interval = 3
start_time = 125193695
[]
[checkpoint_RIA]
type = Checkpoint
file_base = recover_files_RIA
sync_times = '124761600 125107200 125193600 125193650 125193700 125193700.06 125193700.07 125193700.08 125193700.09 125193700.10 125193700.20 125193700.30 125193700.40 125193700.50 125193700.60 125193700.70 125193700.80 125193700.90 125193701.00 125193701.25 125193701.50 125193701.75 125193702.00 125193702.25 125193702.50 125193702.75 125193703.00 125193704.00 125193705.00'
sync_only = true
[]
[]
[Debug]
show_var_residual = 'disp_x disp_y temp'
show_var_residual_norms = true
show_material_props = true
[]
(assessment/LWR/validation/LOCA_ORNL_cladding_burst_tests/analysis/Zr2_1/ornl_zr2_1_aniso.i)
# Simulation ORNL burst tests Zr2_1
[GlobalParams]
density = 6550.
order = SECOND
family = LAGRANGE
displacements = 'disp_x disp_y'
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = zr2_ornl_burst_test_mesh.e
[]
[]
[Variables]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func] # only 10 inches of the rod are within the heated zone (cf. Terrani email)
type = PiecewiseBilinear
data_file = temperature_ornl_zr2_1.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
data_file = pressure_inner_ornl_zr2_1.csv
scale_factor = 1.e+06
format = columns
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 400. '
y = '0.1 0.1 ' # atmospheric pressure
scale_factor = 1.e+06
[]
# Circumferential steady-state creep test and analysis of Zircaloy-4 fuelcladding
# Nuclear Engineering and Design, 53, 2312-2322 (2021)
[F]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.738 0.57 0.57'
[]
[G]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.174 0.45 0.45'
[]
[H]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.588 0.48 0.48'
[]
[L]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[M]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[N]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[clad]
use_automatic_differentiation = true
block = cladding
add_variables = true
strain = FINITE
decomposition_method = TaylorExpansion
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
eigenstrain_names = 'clad_thermal_eigenstrain'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz hoop_stress'
[]
[]
[AuxVariables]
[creep_rate_aux]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[scale_thickness]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfract_total]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfgain_total]
order = CONSTANT
family = MONOMIAL
[]
[burst_stress]
order = CONSTANT
family = MONOMIAL
[]
[burst]
order = CONSTANT
family = MONOMIAL
[]
[]
[Kernels]
[heat]
type = ADHeatConduction
variable = temperature
[]
[heat_ie]
type = ADHeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate_aux]
type = ADMaterialRealAux
variable = creep_rate_aux
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = ADMaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[scl_thickness]
type = ADMaterialRealAux
variable = scale_thickness
property = oxide_scale_thickness
boundary = 2
[]
[ofract_total]
type = ADMaterialRealAux
variable = oxywtfract_total
property = current_oxygen_weight_frac_total
boundary = 2
[]
[ofgain_total]
type = ADMaterialRealAux
boundary = 2
variable = oxywtfgain_total
property = oxygen_weight_frac_gained_total
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = 2
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = 2
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = ADFunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 4'
preset = false
[]
[no_y_top]
type = ADDirichletBC
variable = disp_y
boundary = 3
value = 0.
preset = false
[]
[Pressure]
[outer_pressure] # apply steam pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[mid_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 2 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
type = ADZryThermal
block = cladding
temperature = temperature
[]
[clad_elasticity_tensor]
type = ADZryElasticityTensor
block = cladding
matpro_youngs_modulus = false
matpro_poissons_ratio = false
[]
[clad_stress]
type = ADComputeMultipleInelasticStress
inelastic_models = 'clad_zrycreep'
block = cladding
[]
[hill_constants]
type = ADHillConstants
hill_constants = "0.738 0.174 0.588 1.0 1.0 1.0"
function_names = "F G H L M N"
temperature = temperature
[]
[clad_zrycreep]
type = ADZryAnisoCreepLOCAUpdate
block = cladding
temperature = temperature
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
temperature_loca_creep_begin = 301
temperature_standard_thermal_creep_end = 300
fract_beta_phase_name = 'ad_fract_beta_phase'
[]
[thermal_expansion]
type = ADZryThermalExpansionMATPROEigenstrain
block = cladding
temperature = temperature
stress_free_temperature = 300.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[density]
type = ADDensity
block = cladding
[]
[phase]
type = ZrPhase
block = cladding
temperature = temperature
numerical_method = 2
[]
[phase_converter]
type = MaterialADConverter
reg_props_in = 'fract_beta_phase'
ad_props_out = 'ad_fract_beta_phase'
[]
[oxidation]
type = ADZryOxidation
boundary = 2
temperature = temperature
clad_inner_radius = 0.004875
clad_outer_radius = 0.005580
normal_operating_temperature_model = epri_kwu_ce
high_temperature_model = leistikow
#use_coolant_channel = true
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = 2
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate_aux
temperature = temperature
fraction_beta_phase = fract_beta_phase
fraction_oxygen_gain = oxywtfgain_total
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = PJFNK
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0
n_startup_steps = 1
end_time = 400.
dtmax = 1.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[Postprocessors]
[pressure_inner]
type = FunctionValuePostprocessor
function = inner_pressure_func
execute_on = 'initial timestep_end'
[]
[pressure_outer]
type = FunctionValuePostprocessor
function = outer_pressure_func
execute_on = 'initial timestep_end'
[]
[ave_clad_temp]
type = SideAverageValue
boundary = 2
variable = temperature
execute_on = 'initial timestep_end'
[]
[max_clad_temp]
type = NodalExtremeValue
block = cladding
value_type = max
variable = temperature
execute_on = 'initial timestep_end'
[]
[min_clad_temp]
type = NodalExtremeValue
block = cladding
value_type = min
variable = temperature
execute_on = 'initial timestep_end'
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = cladding
[]
[max_oxygen_fract]
type = ElementExtremeValue
block = cladding
value_type = max
variable = oxywtfract_total
execute_on = 'initial timestep_end'
[]
[max_betaph_fract]
type = ElementExtremeValue
block = cladding
value_type = max
variable = fract_beta_phase
execute_on = 'initial timestep_end'
[]
[max_creep_rate]
type = ElementExtremeValue
block = cladding
value_type = max
variable = creep_rate_aux
execute_on = 'initial timestep_end'
[]
[max_creep_strain_mag]
type = ElementExtremeValue
block = cladding
value_type = max
variable = creep_strain_mag
execute_on = 'initial timestep_end'
[]
[max_hoop_strain]
type = ElementExtremeValue
block = cladding
value_type = max
variable = strain_zz
execute_on = 'initial timestep_end'
[]
[max_hoop_stress]
type = ElementExtremeValue
block = cladding
value_type = max
variable = hoop_stress
[]
[vonmises_stress_clad]
type = ElementAverageValue
block = cladding
variable = vonmises_stress
execute_on = 'initial timestep_end'
[]
[min_burst_stress]
type = ElementExtremeValue
block = cladding
value_type = min
variable = burst_stress
execute_on = 'initial timestep_end'
[]
[burst]
type = ElementExtremeValue
block = cladding
value_type = max
variable = burst
execute_on = 'initial timestep_end'
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = cladding
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[mid_disp_r_clad]
type = NodalVariableValue
variable = disp_x
nodeid = 22
[]
[stress_xx_midplane] # stress in the mid Element
type = ElementalVariableValue
variable = stress_xx
elementid = 19
[]
[stress_yy_midplane] # stress in the mid Element
type = ElementalVariableValue
variable = stress_yy
elementid = 19
[]
[stress_zz_midplane] # stress in the mid Element
type = ElementalVariableValue
variable = stress_zz
elementid = 19
[]
[strain_zz_midplane] # strain in the mid Element
type = ElementalVariableValue
variable = strain_zz
elementid = 19
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
plenum_boundary_name = 4
cladding_blocks = cladding
[]
[PerformanceMetricOutputs]
[]
[Outputs]
exodus = true
perf_graph = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 20
[]
[chkfile]
type = CSV
file_base = ornl_zr2_1_aniso_chkfile
show = 'pressure_inner max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/LOCA_REBEKA_cladding_burst_tests/analysis/rebeka_2d_01MPa/rebeka_singlerod_2d_01MPa.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.0
order = SECOND
family = LAGRANGE
displacements = 'disp_x disp_y'
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = rebeka_singlerod.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 573.0
[]
[]
[Functions]
[temperature_func]
type = PiecewiseLinear
x = '0. 700. '
y = '573. 1273.' # From 300 to 1000 C at 1 K/s
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 700. '
y = '1.e+06 1.e+06' # 10 bar
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 700. '
y = '1.e+05 1.e+05' # atmospheric pressure
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[clad]
block = cladding
add_variables = false
strain = FINITE
decomposition_method = EigenSolution
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz hoop_stress'
[]
[]
[AuxVariables]
[creep_rate_aux]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[scale_thickness]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfract_total]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfgain_total]
order = CONSTANT
family = MONOMIAL
[]
[burst_stress]
order = CONSTANT
family = MONOMIAL
[]
[burst]
order = CONSTANT
family = MONOMIAL
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate_aux]
type = MaterialRealAux
variable = creep_rate_aux
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[scl_thickness]
type = MaterialRealAux
variable = scale_thickness
property = oxide_scale_thickness
boundary = 2
[]
[ofract_total]
type = MaterialRealAux
variable = oxywtfract_total
property = current_oxygen_weight_frac_total
boundary = 2
[]
[ofgain_total]
type = MaterialRealAux
boundary = 2
variable = oxywtfgain_total
property = oxygen_weight_frac_gained_total
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = 2
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = 2
execute_on = timestep_end
[]
[]
[BCs]
[inner_temperature]
type = REBEKADirichletBC
variable = temperature
function_tempm = temperature_func
minimum_temperature = 573.
translation = 0.1625
boundary = 4
[]
[no_y_midsection]
type = DirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply steam pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 101 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[CoolantChannel]
[convective_clad_surface]
boundary = 2
variable = temperature
inlet_temperature = 473.
inlet_pressure = 1.e+05
inlet_massflux = 1.0 # kg/m^2-sec # almost stagnant steam
rod_diameter = 10.75e-03
rod_pitch = 1.26e-02
number_axial_zone = 15
oxide_thickness = scale_thickness
[]
[]
[Materials]
[thermal]
type = ZryThermal
block = cladding
temperature = temperature
[]
[clad_elasticity_tensor]
type = ComputeIsotropicElasticityTensor
block = cladding
youngs_modulus = 1.0e11
poissons_ratio = 0.3
[]
[clad_stress]
type = ComputeMultipleInelasticStress
tangent_operator = elastic
inelastic_models = 'clad_zrycreep'
block = cladding
[]
[clad_zrycreep]
type = ZryCreepLOCAUpdate
block = cladding
temperature = temperature
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
temperature_loca_creep_begin = 501 # see Erbacher et al., 1982
temperature_standard_thermal_creep_end = 500
[]
[thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = cladding
temperature = temperature
stress_free_temperature = 573.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[density]
type = Density
block = cladding
[]
[phase]
type = ZrPhase
block = cladding
temperature = temperature
numerical_method = 2
[]
[oxidation]
type = ZryOxidation
boundary = 2
temperature = temperature
clad_inner_radius = 0.00465
clad_outer_radius = 0.005375
normal_operating_temperature_model = epri_kwu_ce
high_temperature_model = leistikow
use_coolant_channel = true
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = 2
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate_aux
temperature = temperature
fraction_beta_phase = fract_beta_phase
fraction_oxygen_gain = oxywtfgain_total
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0
n_startup_steps = 1
end_time = 700.
dtmax = 1.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average temperature of cladding exterior
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = cladding
[]
[max_clad_temp]
type = NodalExtremeValue
block = cladding
value_type = max
variable = temperature
[]
[max_oxygen_fract]
type = ElementExtremeValue
block = cladding
value_type = max
variable = oxywtfract_total
[]
[max_betaph_fract]
type = ElementExtremeValue
block = cladding
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
block = cladding
value_type = max
variable = creep_rate_aux
[]
[max_creep_strain_mag]
type = ElementExtremeValue
block = cladding
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
block = cladding
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
block = cladding
value_type = max
variable = hoop_stress
[]
[vonmises_stress_clad]
type = ElementAverageValue
block = cladding
variable = vonmises_stress
[]
[min_burst_stress]
type = ElementExtremeValue
block = cladding
value_type = min
variable = burst_stress
[]
[burst]
type = ElementExtremeValue
block = cladding
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = cladding
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = cladding
plenum_boundary_name = 4
external_clad_boundary_name = 2
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = rebeka_2d_01MPa_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-05/puzry-05_aniso.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-05.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 2000. '
y = '1.e+05 1.e+05 7.2e+05' # Linear increase at 0.062 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 2000. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
# Circumferential steady-state creep test and analysis of Zircaloy-4 fuel cladding
# Nuclear Engineering and Design, 53, 2312-2322 (2021)
[F]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.738 0.738 0.57'
[]
[G]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.174 0.174 0.45'
[]
[H]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.588 0.588 0.48'
[]
[L]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[M]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[N]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = TaylorExpansion
use_automatic_differentiation = true
[]
[]
[]
[]
[Kernels]
[heat]
type = ADHeatConduction
variable = temperature
[]
[heat_ie]
type = ADHeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = ADMaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = ADMaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = ADMaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = ADMaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = ADMaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = ADFunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = ADDirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = ADDirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ADZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1.e+11
poissons_ratio = 0.3
block = 1
[]
[hill_constants]
type = ADHillConstants
hill_constants = "0.738 0.174 0.588 1.0 1.0 1.0"
function_names = "F G H L M N"
temperature = temperature
[]
[creep_update]
type = ADZryAnisoCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 1.5e-05
temperature = temperature
temperature_standard_thermal_creep_end = 700
temperature_loca_creep_begin = 900.
fract_beta_phase_name = 'fract_beta_phase'
max_integration_error = 1000000.0
absolute_tolerance = 1e-07
relative_tolerance = 1e-07
[]
[creep]
type = ADComputeMultipleInelasticStress
block = 1
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ADZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = ADDensity
block = 1
[]
[phase]
type = ADZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ADZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = NEWTON
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0.
n_startup_steps = 1
end_time = 2500.
dtmax = 1.
dtmin = 1.0e-9
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-05_aniso_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/LOCA_ANL_cladding_burst_tests/analysis/OCL5_8/OCL5_8_aniso.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
displacements = 'disp_x disp_y'
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
[]
[Mesh]
coord_type = RZ
[smeared_pellet_mesh]
type = FuelPinMeshGenerator
pellet_quantity = 1
pellet_height = 0.270
pellet_outer_radius = 4.78e-3
clad_bot_gap_height = 0.001
clad_top_gap_height = 0.013
clad_thickness = 0.71e-3
clad_gap_width = 0.1e-3
pellet_mesh_density = coarse
clad_mesh_density = coarse
elem_type = QUAD8
[]
patch_size = 10
patch_update_strategy = auto
partitioner = centroid
centroid_partitioner_direction = y
[]
[Variables]
[temperature]
initial_condition = 300.0
[]
[]
[Functions]
[temperature_func]
type = PiecewiseLinear
x = '0 496.02 520.74 528.12 545.94 551.28 671.52 885.3 1195.74 1410.36 1657.86 1680 1690 1700 1710 1720 1730 1740 1750 1760 1770 1780 1790 1800 1810 1820 1830 1840 1848'
y = '300 300 405.465 482.048 583.351 632.287 634.297 632.825 630.378 631.059 632.59 633 683 733 783 833 883 933 983 1033 1083 1133 1183 1233 1283 1333 1383 1433 1477'
[]
[temperature_profile]
type = PiecewiseBilinear
data_file = 'temp_profile.csv'
axis = 1
[]
[cladding_temperature]
type = CompositeFunction
functions = 'temperature_func temperature_profile'
[]
# Circumferential steady-state creep test and analysis of Zircaloy-4 fuelcladding
# Nuclear Engineering and Design, 53, 2312-2322 (2021)
[F]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.738 0.57 0.57'
[]
[G]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.174 0.45 0.45'
[]
[H]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.588 0.48 0.48'
[]
[L]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[M]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[N]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[pellets]
block = pellet
use_automatic_differentiation = true
add_variables = true
strain = FINITE
decomposition_method = TaylorExpansion
eigenstrain_names = 'fuel_thermal_strain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
generate_output = 'vonmises_stress hydrostatic_stress stress_xx stress_yy
stress_zz strain_xx strain_yy strain_zz hoop_stress'
extra_vector_tags = 'ref'
[]
[clad]
block = clad
use_automatic_differentiation = true
add_variables = true
strain = FINITE
decomposition_method = TaylorExpansion
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz hoop_stress'
extra_vector_tags = 'ref'
[]
[]
[AuxVariables]
[creep_rate_aux]
order = CONSTANT
family = MONOMIAL
block = clad
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
block = clad
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
block = clad
[]
[burst_stress]
order = CONSTANT
family = MONOMIAL
block = clad
[]
[burst]
order = CONSTANT
family = MONOMIAL
block = clad
[]
[]
[Kernels]
[heat]
type = ADHeatConduction
variable = temperature
extra_vector_tags = 'ref'
[]
[heat_ie]
type = ADHeatConductionTimeDerivative
variable = temperature
extra_vector_tags = 'ref'
[]
[]
[AuxKernels]
[creep_rate_aux]
type = ADMaterialRealAux
variable = creep_rate_aux
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = ADMaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
block = clad
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = clad_outside_right
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = clad_outside_right
execute_on = timestep_end
[]
[]
[ThermalContact]
[thermal_contact]
type = GapHeatTransfer
primary = 5
secondary = 10
variable = temperature
gap_conductivity = 0.15 # k of He per Netzsch
[]
[]
[BCs]
[clad_surface_temperature]
type = ADFunctionDirichletBC
variable = temperature
boundary = '2'
function = cladding_temperature
[]
[no_x_all]
type = ADDirichletBC
variable = disp_x
boundary = 12
value = 0.0
[]
[no_y_clad_bottom]
type = ADDirichletBC
variable = disp_y
boundary = '1'
value = 0.0
[]
[no_y_fuel_bottom]
type = ADDirichletBC
variable = disp_y
boundary = '1020'
value = 0.0
[]
[Pressure]
[outer_pressure]
boundary = '1 2 3'
factor = 101325
[]
[inner_pressure]
boundary = '4 5 6'
factor = 8.28e6
[]
[]
[]
[PlenumTemperature]
[plenum_temp]
boundary = 5
inner_surfaces = '5'
outer_surfaces = '10'
temperature = temperature
[]
[]
[Materials]
[fuel_thermal]
type = ADHeatConductionMaterial
block = pellet
thermal_conductivity = 3.5
specific_heat = 330.0
[]
[fuel_elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
block = pellet
youngs_modulus = 2.0e11
poissons_ratio = 0.345
[]
[fuel_elastic_stress]
type = ADComputeFiniteStrainElasticStress
block = pellet
[]
[fuel_thermal_expansion]
type = ADComputeThermalExpansionEigenstrain
block = pellet
thermal_expansion_coeff = 10.0e-6
temperature = temperature
stress_free_temperature = 300.0
eigenstrain_name = fuel_thermal_strain
[]
[fuel_density]
type = ADDensity
block = pellet
density = 10980.0 #perfectly dense UO2
[]
[clad_thermal]
type = ADZryThermal
block = clad
temperature = temperature
[]
[clad_elasticity_tensor]
type = ADZryElasticityTensor
block = clad
matpro_youngs_modulus = false
matpro_poissons_ratio = false
[]
[clad_stress]
type = ADComputeMultipleInelasticStress
inelastic_models = 'clad_zrycreep'
block = clad
[]
[hill_constants]
type = ADHillConstants
#hill_constants = "0.5 0.5 0.5 1.0 1.0 1.0"
hill_constants = "0.738 0.174 0.588 1.0 1.0 1.0"
function_names = "F G H L M N"
[]
[clad_zrycreep]
type = ADZryAnisoCreepLOCAUpdate
block = clad
temperature = temperature
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
temperature_loca_creep_begin = 301
temperature_standard_thermal_creep_end = 300
fract_beta_phase_name = 'ad_fract_beta_phase'
[]
[thermal_expansion]
type = ADZryThermalExpansionMATPROEigenstrain
block = clad
temperature = temperature
stress_free_temperature = 300.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[clad_density]
type = ADDensity
block = clad
density = 6550.0
[]
[phase]
type = ZrPhase
block = clad
temperature = temperature
numerical_method = 2
[]
[phase_converter]
type = MaterialADConverter
block = clad
reg_props_in = 'fract_beta_phase'
ad_props_out = 'ad_fract_beta_phase'
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = clad_outside_right
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate_aux
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
verbose = true
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.0e-04
nl_abs_tol = 1.0e-08
start_time = 0
n_startup_steps = 1
end_time = 1800.0
dtmax = 100
dtmin = 0.0001
[TimeStepper]
type = IterationAdaptiveDT
timestep_limiting_postprocessor = material_timestep
dt = 10.0
time_dt = '100 10'
time_t = '10 400'
[]
[]
[Postprocessors]
[ave_clad_temp]
type = SideAverageValue
boundary = clad_outside_right
variable = temperature
[]
[gas_volume]
type = InternalVolume
boundary = 9
execute_on = 'initial linear'
[]
[max_clad_temp]
type = NodalExtremeValue
block = clad
value_type = max
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = clad
[]
[max_hoop_stress]
type = ElementExtremeValue
block = clad
value_type = max
variable = hoop_stress
[]
[vonmises_stress_clad]
type = ElementAverageValue
block = clad
variable = vonmises_stress
[]
[min_burst_stress]
type = ElementExtremeValue
block = clad
value_type = min
variable = burst_stress
[]
[burst]
type = ElementExtremeValue
block = clad
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = clad
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
[]
[PerformanceMetricOutputs]
[]
[Outputs]
exodus = true
csv = true
color = false
perf_graph = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
show = 'max_clad_temp max_hoop_stress vonmises_stress_clad'
execute_on = 'FINAL'
[]
[]
[UserObjects]
[terminator1]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
[]
[]
(assessment/LWR/validation/LOCA_Studsvik/analysis/rod_191/Studsvik_191_part2_1p5d_fr_frd.i)
[GlobalParams]
density = 10431.0
initial_porosity = 0.05
order = SECOND
family = LAGRANGE
energy_per_fission = 3.2e-11 # J/fission
volumetric_locking_correction = false
displacements = 'disp_x'
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
restart_file_base = 'Studsvik_191_part1_1p5d_fr_frd_checkpoint_cp/LATEST'
[]
[Mesh]
coord_type = RZ
[layered1D_mesh]
type = Layered1DMeshGenerator
slices_per_block = 10
clad_gap_width = 8.0e-5
clad_thickness = 0.57e-3
fuel_height = 0.265388558
plenum_height = 0.034861442
elem_type = EDGE3
nx_p = 11
pellet_mesh_density = customize
[]
patch_update_strategy = auto
partitioner = centroid
centroid_partitioner_direction = y
[]
[Variables]
[temperature]
[]
[]
[AuxVariables]
[strain_yy_0]
order = CONSTANT
family = MONOMIAL
[]
[tangential_contact_pressure_aux]
block = fuel
[]
# Define auxilary variables
[fast_neutron_flux]
block = clad
[]
[fast_neutron_fluence]
block = clad
[]
[grain_radius]
block = fuel
[]
[creep_strain_rate]
order = CONSTANT
family = MONOMIAL
[]
[effective_creep_strain]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[hoop_strain]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[scale_thickness] # ZrO2 scale thickness (m)
order = CONSTANT
family = MONOMIAL
[]
[oxywtfract_total] # Current oxigen weight fraction (oxide+metal) (/)
order = CONSTANT
family = MONOMIAL
[]
[oxywtfgain_total] # Gained oxygen weight fraction (oxide+metal) (/)
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[gap_cond]
order = CONSTANT
family = MONOMIAL
[]
[]
[Functions]
[power_history]
type = PiecewiseLinear
data_file = power_history.csv
format = columns
scale_factor = 1
[]
[axial_peaking_factors]
type = ParsedFunction
expression = 1
[]
[pressure_ramp] # reads and interpolates input data defining amplitude curve for fill gas pressure
type = PiecewiseLinear
x = '-200 0 166755600 166842000'
y = '0.006537 1 1 0.006537'
scale_factor = 15.5e6
[]
[forced_times]
type = PiecewiseLinear
data_file = timestep_limiting.csv
scale_factor = 1
format = columns
[]
# Add this to accident part
[clad_surface_temperature]
type = PiecewiseBilinear
axis = 1
data_file = clad_temperature.csv
[]
[clad_axial_pressure]
type = CladdingAxialPressureFunction
plenum_pressure = plenum_pressure
coolant_pressure = pressure_ramp
coolant_pressure_scaling_factor = 1.0
fuel_pin_geometry = fuel_pin_geometry
[]
[fuel_axial_pressure]
type = ParsedFunction
expression = plenum_pressure
symbol_names = plenum_pressure
symbol_values = plenum_pressure
[]
[]
[Physics]
[SolidMechanics]
[Layered1D]
[fuel]
block = fuel
add_variables = true
add_scalar_variables = true
strain = FINITE
out_of_plane_strain_name = strain_yy
eigenstrain_names = 'fuel_thermal_eigenstrain fuel_volumetric_eigenstrain '
'axial_relocation_eigenstrain'
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress strain_xx hoop_stress '
'creep_strain_zz strain_zz'
extra_vector_tags = 'ref'
fuel_pin_geometry = fuel_pin_geometry
group_scalar_vars_in_reference_residual = true
mesh_generator = layered1D_mesh
decomposition_method = EigenSolution
layer_friction_user_object = 1DFriction_secondary
temperature = temperature
out_of_plane_pressure_function = fuel_axial_pressure
[]
[clad]
block = clad
add_variables = true
add_scalar_variables = true
strain = FINITE
out_of_plane_strain_name = strain_yy
eigenstrain_names = 'clad_thermal_eigenstrain clad_irradiation_eigenstrain'
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress strain_xx hoop_stress '
'creep_strain_zz strain_zz'
extra_vector_tags = 'ref'
fuel_pin_geometry = fuel_pin_geometry
group_scalar_vars_in_reference_residual = true
mesh_generator = layered1D_mesh
decomposition_method = EigenSolution
layer_friction_user_object = 1DFriction_primary
temperature = temperature
out_of_plane_pressure_function = clad_axial_pressure
[]
[]
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
extra_vector_tags = 'ref'
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
extra_vector_tags = 'ref'
[]
[heat_source]
type = NeutronHeatSource
variable = temperature
extra_vector_tags = 'ref'
block = fuel
burnup_function = burnup
axial_relocation_object = axial_relocation
[]
[]
[Burnup]
[burnup]
block = fuel
rod_ave_lin_pow = power_history # using the power function defined above
axial_power_profile = axial_peaking_factors # using the axial power profile function defined above
num_radial = 80
num_axial = 11
fuel_pin_geometry = fuel_pin_geometry
fuel_volume_ratio = 1.0 # for use with dished pellets (ratio of actual volume to cylinder volume)
order = CONSTANT
family = MONOMIAL
RPF = RPF
isotopes = 'U235 U238 Pu239 Pu240 Pu241 Pu242'
isotope_fractions = '0.05 0.95 0 0 0 0'
[]
[]
[AuxKernels]
# Define auxilliary kernels for each of the aux variables
[tangential_contact_pressure_aux]
type = SpatialUserObjectAux
variable = tangential_contact_pressure_aux
user_object = 1DFriction_secondary
block = fuel
execute_on = 'TIMESTEP_END'
[]
[fast_neutron_flux]
type = FastNeutronFluxAux
variable = fast_neutron_flux
block = clad
rod_ave_lin_pow = power_history
axial_power_profile = axial_peaking_factors
factor = 3e13
execute_on = timestep_begin
[]
[fast_neutron_fluence]
type = FastNeutronFluenceAux
variable = fast_neutron_fluence
block = clad
fast_neutron_flux = fast_neutron_flux
execute_on = timestep_begin
[]
[grain_radius]
type = GrainRadiusAux
block = fuel
variable = grain_radius
temperature = temperature
execute_on = linear
[]
[creep_strain_rate]
type = MaterialRealAux
property = creep_rate
variable = creep_strain_rate
block = clad
[]
[effective_creep_strain]
type = MaterialRealAux
property = effective_creep_strain
variable = effective_creep_strain
block = clad
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
block = clad
variable = fract_beta_phase
property = fract_beta_phase
[]
[scl_thickness]
type = MaterialRealAux
boundary = 2
variable = scale_thickness
property = oxide_scale_thickness
[]
[ofract_total]
type = MaterialRealAux
boundary = 2
variable = oxywtfract_total
property = current_oxygen_weight_frac_total
[]
[ofgain_total]
type = MaterialRealAux
boundary = 2
variable = oxywtfgain_total
property = oxygen_weight_frac_gained_total
[]
[sigmaburst]
type = MaterialRealAux
boundary = 2
variable = burst_stress
property = burst_stress
[]
[hasburst]
type = MaterialRealAux
boundary = 2
variable = burst
property = failed
execute_on = timestep_end
[]
[conductance]
type = MaterialRealAux
property = gap_conductance
variable = gap_cond
boundary = 10
execute_on = 'linear'
[]
[]
[Contact]
[pellet_clad_mechanical]
primary = 5
secondary = 10
formulation = kinematic
model = frictionless
penalty = 1e7
[]
[]
[ThermalContact]
[thermal_contact]
type = GasGapHeatTransfer
variable = temperature
primary = 5
secondary = 10
initial_moles = initial_moles
gas_released = fission_gas_released
quadrature = true
contact_pressure = contact_pressure
refab_gas_types = He
refab_fractions = 1
refab_time = 166842000
refab_type = 0
[]
[]
[BCs]
[no_x_all]
type = DirichletBC
variable = disp_x
boundary = 12
value = 0.0
[]
[Pressure]
[coolantPressure]
boundary = '2'
function = pressure_ramp
[]
[]
[PlenumPressure]
[plenumPressure]
boundary = 9
initial_pressure = 3.44738e6
startup_time = 0
R = 8.3143
output_initial_moles = initial_moles
temperature = plenum_temp
volume = plenum_volume
material_input = fission_gas_released
output = plenum_pressure
refab_time = 166842000
refab_pressure = 11e6
refab_temperature = 295.0
refab_volume = 1.04e-05
cladding_failure_status = burst
equilibrium_pressure = equilibrium_pressure
additional_volumes = additional_volume
temperature_of_additional_volumes = addition_temperature
[]
[]
[clad_temp]
type = FunctionDirichletBC
function = clad_surface_temperature
variable = temperature
boundary = 2
[]
[]
[UserObjects]
# Fuel dispersal
[layered_average_hoop_strain]
type = LayeredAverage
block = clad
num_layers = 10
direction = y
variable = strain_zz
[]
[cladding_strain_yy]
type = LayeredAverage
block = clad
num_layers = 11
direction = y
variable = strain_yy
execute_on = 'initial timestep_end'
[]
[fuel_strain_yy]
type = LayeredAverage
block = fuel
num_layers = 10
direction = y
variable = strain_yy
execute_on = 'initial timestep_end'
[]
# We could have two element UOs to obtain interface stress
[1DContactStressOOP_fuel]
type = Layered1DContactInterfaceStress
direction = y
stress_name = stress
num_layers = 10
# If we do not provide the numbers below, it will look at the mesh, in all blocks to set the layer number. Then, it will
# be wrong because the cladding has more height and won't be able to identify layers in the fuel.
direction_min = 0.0165094
direction_max = 0.255359
block = fuel
execute_on = 'LINEAR NONLINEAR'
[]
[1DContactStressOOP_cladding]
type = Layered1DContactInterfaceStress
direction = y
stress_name = stress
num_layers = 10
# If we do not provide the numbers below, it will look at the mesh, in all blocks to set the layer number. Then, it will
# be wrong because the cladding has more height and won't be able to identify layers in the fuel.
direction_min = 0.0165094
direction_max = 0.255359
block = clad
execute_on = 'LINEAR NONLINEAR'
[]
[1DFriction_secondary]
type = Layered1DFrictionalForce
force_postaux = true
contact_pressure = contact_pressure
direction = y
boundary = pellet_outer_radial_surface
num_layers = 10
interface_oop_stress_provider_fuel = 1DContactStressOOP_fuel
interface_oop_stress_provider_cladding = 1DContactStressOOP_cladding
is_secondary_side = true
tangential_pressure = tangential_contact_pressure_aux
friction_coefficient = 0.2
thickness = 0.0265
penalty_factor = 1.0e13
# If we do not provide the numbers below, it will look at the mesh, in all blocks to set the layer number. Then, it will
# be wrong because the cladding has more height and won't be able to identify layers in the fuel.
direction_min = 0.0165094
direction_max = 0.255359
scalar_var_name_base_fuel = scalar_strain_yy_fuel
scalar_num_variable_fuel = 10
scalar_var_name_base_cladding = scalar_strain_yy_clad
scalar_num_variable_cladding = 10
execute_on = 'LINEAR NONLINEAR'
[]
[1DFriction_primary]
type = Layered1DFrictionalForce
force_postaux = true
contact_pressure = contact_pressure
direction = y
boundary = clad_inside_right
num_layers = 10
# If we do not provide the numbers below, it will look at the mesh, in all blocks to set the layer number. Then, it will
# be wrong because the cladding has more height and won't be able to identify layers in the fuel.
direction_min = 0.0165094
direction_max = 0.255359
interface_oop_stress_provider_fuel = 1DContactStressOOP_fuel
interface_oop_stress_provider_cladding = 1DContactStressOOP_cladding
is_secondary_side = false
secondary_side_frictional_user_object = 1DFriction_secondary
friction_coefficient = 0.2
thickness = 0.0265
penalty_factor = 1.0e13
scalar_var_name_base_fuel = scalar_strain_yy_fuel
scalar_num_variable_fuel = 10
scalar_var_name_base_cladding = scalar_strain_yy_clad
scalar_num_variable_cladding = 10
execute_on = 'LINEAR NONLINEAR'
[]
# Axial relocation object is created by axial relocation action
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[]
[PlenumTemperature]
[plenum_temp]
boundary = 5
inner_surfaces = '5'
outer_surfaces = '10'
temperature = temperature
[]
[]
[CoolantChannel]
[convective_clad_surface] # apply convective boundary to clad outer surface
boundary = 2
variable = temperature
inlet_temperature = 580
inlet_pressure = 15.5e6 # Pa
inlet_massflux = 3800 # kg/m^2-sec
rod_diameter = 0.0095 # m
rod_pitch = 1.26e-2 # m
compute_enthalpy = false
linear_heat_rate = power_history
axial_power_profile = axial_peaking_factors
output_properties = 'coolant_channel_htype coolant_channel_hmode'
[]
[]
[Materials]
[fuel_dispersal]
type = UO2Dispersal
block = fuel
axial_relocation_object = axial_relocation
layered_average_burnup = layered_average_burnup
layered_average_hoop_strain = layered_average_hoop_strain
dispersal_model = ONE_MM_TWO_PERCENT_STRAIN
[]
# Define material behavior models and input material property data
[fuel_thermal] # temperature and burnup dependent thermal properties of UO2 (BISON kernel)
type = UO2Thermal
block = fuel
thermal_conductivity_model = NFIR
temperature = temperature
burnup_function = burnup
axial_relocation_object = axial_relocation
gap_thermal_conductivity = layered_average_gap_conductivity
[]
[fuel_elasticity_tensor]
type = UO2IsotropicDamageElasticityTensor
block = fuel
fragmentation_model = BARANI
temperature = temperature
rod_ave_lin_pow = power_history
axial_relocation_object = axial_relocation
[]
[fuel_elastic_stress]
type = ComputeMultipleInelasticStress
tangent_operator = elastic
inelastic_models = 'fuel_creep'
block = fuel
[]
[fuel_creep]
type = UO2CreepUpdate
block = fuel
temperature = temperature
fission_rate = fission_rate
initial_grain_radius = 10.0e-6
oxygen_to_metal_ratio = 2.0
[]
[fuel_thermal_expansion]
type = ComputeThermalExpansionEigenstrain
block = fuel
thermal_expansion_coeff = 10.0e-6
temperature = temperature
stress_free_temperature = 295.0
eigenstrain_name = fuel_thermal_eigenstrain
[]
[fuel_volumetric_swelling]
type = UO2VolumetricSwellingEigenstrain
gas_swelling_model_type = SIFGRS
block = fuel
temperature = temperature
burnup_function = burnup
initial_fuel_density = 10431.0
eigenstrain_name = fuel_volumetric_eigenstrain
[]
[fission_gas_release]
type = UO2Sifgrs
block = fuel
temperature = temperature
burnup_function = burnup
grain_radius = grain_radius
gbs_model = true
[]
[clad_density]
type = Density
block = clad
density = 6550.
[]
[clad_thermal]
block = clad
type = ZryThermal
temperature = temperature
[]
[clad_thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = clad
temperature = temperature
stress_free_temperature = 295.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = clad
temperature = temperature
[]
[zry_thermal_creep]
type = ZryCreepLOCAUpdate
block = clad
temperature = temperature
model_irradiation_creep = true
model_primary_creep = true
model_thermal_creep = true
max_inelastic_increment = 5e-4
fast_neutron_flux = fast_neutron_flux
fast_neutron_fluence = fast_neutron_fluence
zircaloy_material_type = zirlo
[]
[clad_stress]
type = ComputeMultipleInelasticStress
tangent_operator = elastic
inelastic_models = 'zry_thermal_creep'
block = clad
[]
[clad_irradiation_growth]
type = ZryIrradiationGrowthEigenstrain
block = clad
fast_neutron_fluence = fast_neutron_fluence
zircaloy_material_type = zirlo
eigenstrain_name = clad_irradiation_eigenstrain
[]
[clad_phase]
type = ZrPhase
block = clad
temperature = temperature
numerical_method = 2
[]
[clad_oxidation]
type = ZryOxidation
boundary = 2
temperature = temperature
clad_inner_radius = 4.18e-03
clad_outer_radius = 4.75e-03
normal_operating_temperature_model = epri_kwu_ce
high_temperature_model = leistikow
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = 2
failure_criterion = overstrain
# effective_strain_rate_creep = creep_strain_rate
# failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
hoop_creep_strain = creep_strain_zz
fraction_beta_phase = fract_beta_phase
fraction_oxygen_gain = oxywtfract_total
temperature = temperature
[]
[fuel_density]
type = Density
block = fuel
[]
[]
##
[AxialRelocation]
[relocation]
rod_ave_lin_pow = power_history
axial_direction = y
fuel_blocks = fuel
clad_blocks = clad
contact_pressure_variable = contact_pressure
out_of_plane_strain_variable = strain_yy_0
penetration_variable = penetration
clad_inner_volume_addition = 0
burnup_variable = burnup
temperature = temperature
axial_relocation_output_options = MASS_FRACTION
mesh_generator = layered1D_mesh
gap_thickness_threshold = 0.00005
[]
[]
[Postprocessors]
[volume_fuel_dispersed]
type = LayeredElementIntegralMaterialProperty
block = fuel
mat_prop = dispersed
fuel_pin_geometry = fuel_pin_geometry
execute_on = 'initial timestep_end'
[]
[mass_fuel_dispersed]
type = ParsedPostprocessor
pp_names = volume_fuel_dispersed
expression = '10431 * volume_fuel_dispersed'
execute_on = 'initial timestep_end'
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
l_max_its = 50
l_tol = 8e-3
nl_max_its = 15
nl_rel_tol = 1e-4
nl_abs_tol = 1e-8
n_startup_steps = 1
end_time = 166843509.6
dtmax = 20
dtmin = 1e-6
[TimeStepper]
type = IterationAdaptiveDT
timestep_limiting_postprocessor = material_timestep
dt = 10
optimal_iterations = 20
iteration_window = 4
linear_iteration_ratio = 100
growth_factor = 2
cutback_factor = .5
timestep_limiting_function = forced_times
force_step_every_function_point = true
[]
[Quadrature]
order = FIFTH
side_order = SEVENTH
[]
[]
[Postprocessors]
[ave_temp_interior]
type = SideAverageValue
boundary = 9
variable = temperature
execute_on = 'initial linear'
[]
[clad_inner_vol]
type = InternalVolume
boundary = 7
#outputs = exodus
execute_on = 'initial timestep_end'
[]
[fission_gas_produced] # fission gas produced (moles)
type = ElementIntegralFisGasGeneratedSifgrs
block = fuel
execute_on = 'linear'
[]
[fission_gas_grain]
type = ElementIntegralFisGasGrainSifgrs
block = fuel
outputs = exodus
execute_on = 'linear'
[]
[fission_gas_boundary]
type = ElementIntegralFisGasBoundarySifgrs
block = fuel
outputs = exodus
execute_on = 'linear'
[]
[flux_from_clad] # area integrated heat flux from the cladding
type = SideDiffusiveFluxIntegral
variable = temperature
boundary = 5
diffusivity = thermal_conductivity
[]
[flux_from_fuel] # area integrated heat flux from the fuel
type = SideDiffusiveFluxIntegral
variable = temperature
boundary = 10
diffusivity = thermal_conductivity
[]
[rod_total_power]
type = ElementIntegralPower
variable = temperature
burnup_function = burnup
block = fuel
[]
[max_fuel_temp]
type = NodalExtremeValue
block = fuel
value_type = max
variable = temperature
[]
[max_clad_temp]
type = NodalExtremeValue
block = clad
value_type = max
variable = temperature
[]
[max_clad_hoop_strain]
type = ElementExtremeValue
block = clad
value_type = max
variable = strain_zz
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = clad
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
block = clad
execute_on = 'initial timestep_end'
[]
[volume_pulverized]
type = ElementIntegralMaterialProperty
mat_prop = pulverized
block = fuel
[]
[max_fuel_temp_periphery]
type = NodalExtremeValue
value_type = max
variable = temperature
boundary = 10
[]
[additional_volume]
type = FunctionValuePostprocessor
function = 8.5e-6
execute_on = 'initial linear'
[]
[addition_temperature]
type = FunctionValuePostprocessor
function = 300.0
execute_on = 'initial linear'
[]
[equilibrium_pressure]
type = FunctionValuePostprocessor
function = 101325.0
execute_on = 'initial linear'
[]
[]
[VectorPostprocessors]
[cladding_outer]
type = NodalValueSampler
boundary = 5
variable = disp_x
sort_by = y
[]
[]
[PerformanceMetricOutputs]
[]
[StandardLWRFuelRodOutputs]
temperature = temperature
layered = true
fuel_pin_geometry = fuel_pin_geometry
fuel_pellet_blocks = 'fuel'
[]
[Outputs]
perf_graph = true
exodus = true
color = false
csv = true
[checkpoint]
type = Checkpoint
num_files = 2
[]
[chkfile]
type = CSV
execute_on = FINAL
show = 'volume_pulverized'
[]
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-23/puzry-23_aniso.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-23.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 2500. '
y = '1.e+05 1.e+05 1.0855e+07' # Linear increase at 0.0717 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 2500. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
# Circumferential steady-state creep test and analysis of Zircaloy-4 fuel cladding
# Nuclear Engineering and Design, 53, 2312-2322 (2021)
[F]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.738 0.738 0.57'
[]
[G]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.174 0.174 0.45'
[]
[H]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.588 0.588 0.48'
[]
[L]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[M]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[N]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = TaylorExpansion
use_automatic_differentiation = true
[]
[]
[]
[]
[Kernels]
[heat]
type = ADHeatConduction
variable = temperature
[]
[heat_ie]
type = ADHeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = ADMaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = ADMaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = ADMaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = ADMaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = ADMaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = ADFunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = ADDirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = ADDirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ADZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1.e+11
poissons_ratio = 0.3
block = 1
[]
[hill_constants]
type = ADHillConstants
hill_constants = "0.738 0.174 0.588 1.0 1.0 1.0"
function_names = "F G H L M N"
temperature = temperature
[]
[creep_update]
type = ADZryAnisoCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 1.5e-05
temperature = temperature
temperature_standard_thermal_creep_end = 700
temperature_loca_creep_begin = 900.
fract_beta_phase_name = 'fract_beta_phase'
max_integration_error = 1000000.0
absolute_tolerance = 1e-13
relative_tolerance = 1e-11
[]
[creep]
type = ADComputeMultipleInelasticStress
block = 1
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ADZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = ADDensity
block = 1
[]
[phase]
type = ADZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ADZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = NEWTON
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-07
start_time = 0.
n_startup_steps = 1
end_time = 2500.
dtmax = 1.
dtmin = 1.0e-9
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-23_aniso_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(examples/multiapp/pin1.i)
## In this example the multiapp system is called to run another BISON simulation.
## (input1.i calls input2.i) An application of this might be multiple fuel pins
## in an assembly. This example also demonstrates the internal mesh maker.
[GlobalParams]
density = 10200
displacements = 'disp_x disp_y'
order = FIRST
family = LAGRANGE
energy_per_fission = 3.2e-11 # J/fission
a_lower = 0.06951
a_upper = 3.72711
initial_porosity = 0.04
[]
# ==================================================== #
# Mesh (and Geometry, internally-meshed)
# ==================================================== #
[Mesh]
coord_type = RZ
[smeared_pellet_mesh]
type = FuelPinMeshGenerator
clad_mesh_density = customize
pellet_mesh_density = customize
clad_thickness = 0.0005
pellet_outer_radius = 0.0041
clad_bot_gap_height = 0.00152
clad_top_gap_height = 0.16
pellet_quantity = 1
pellet_height = 3.6576
clad_gap_width = 8.0e-05
bottom_clad_height = 0.0167
top_clad_height = 0.0167
nx_p = 6 # number of radial elements in the fuel
ny_p = 48 # number of axial elements in the fuel
nx_c = 3 # number of elements in the clad thickness
ny_c = 48 # number of elements in the axially in the clad
ny_cu = 1
ny_cl = 1
intervals = '0.03866 0.08211 0.08211 0.08211 0.08212 0.08211 0.08211 0.08211 0.0381 0.08065 0.08065 0.08065 0.08065 0.08065 0.08065 0.0381 0.08065 0.08065 0.08065 0.08065 0.08065 0.08065 0.0381 0.08065 0.08065 0.08065 0.08065 0.08065 0.08065 0.0381 0.08065 0.08065 0.08065 0.08065 0.08065 0.08065 0.0381 0.08065 0.08065 0.08065 0.08065 0.08065 0.08065 0.0381 0.079212 0.079212 0.079212 0.079212 0.079212'
elem_type = QUAD4
[]
partitioner = centroid
centroid_partitioner_direction = y
patch_size = 10
patch_update_strategy = auto
[]
[DefaultElementQuality]
aspect_ratio_upper_bound = 493
[]
# ==================================================== #
# Dimensions and Primary Variables
# ==================================================== #
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
group_variables = 'disp_x disp_y'
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temp]
initial_condition = 3.000000e+02
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[pellets]
block = 3
add_variables = false
strain = FINITE
eigenstrain_names = 'fuel_relocation_strain fuel_thermal_strain fuel_volumetric_strain'
generate_output = 'vonmises_stress hydrostatic_stress stress_xx stress_yy stress_zz strain_xx strain_yy strain_zz'
extra_vector_tags = 'ref'
[]
[clad]
block = 1
add_variables = false
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain clad_irradiation_strain'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz creep_strain_xx creep_strain_yy creep_strain_xy creep_strain_zz strain_xx strain_yy strain_zz'
extra_vector_tags = 'ref'
[]
[]
# ==================================================== #
# Auxiliary Variables
# ==================================================== #
[AuxVariables]
# ================================================== #
# Nodal Quantities
# ================================================== #
[htcl]
initial_condition = 500.0
[]
[htcv]
initial_condition = 0.0
[]
[Tl]
initial_condition = 565.0
[]
[Tv]
initial_condition = 565.0
[]
[burnup]
block = 3
[]
[fast_neutron_flux]
block = 1
[]
[fast_neutron_fluence]
block = 1
[]
[grain_radius]
block = 3
initial_condition = 5.240000e-06
[]
# ================================================== #
# Constant Monomial Quantities (Non-Mechanics)
# ================================================== #
[pellet_id]
order = CONSTANT
family = MONOMIAL
block = 3
[]
[axial_fission_rate]
order = CONSTANT
family = MONOMIAL
[]
[axial_burnup]
order = CONSTANT
family = MONOMIAL
[]
[axial_temperature]
order = CONSTANT
family = MONOMIAL
[]
[gap_conductivity]
order = CONSTANT
family = MONOMIAL
[]
[porosity]
order = CONSTANT
family = MONOMIAL
initial_condition = 0.04
[]
[]
# ==================================================== #
# Time- and Space-Dependent Source and BCs
# ==================================================== #
[Functions]
[linear_heat_rate_profile]
type = PiecewiseLinear
x = '-100 0 5000'
y = '0 0 25000'
scale_factor = 1
[]
[axial_peaking_factors]
type = ParsedFunction
expression = 1
[]
[coolant_temperature]
type = PiecewiseLinear
x = '-100 0'
y = '293 565'
axis = y
[]
[coolant_pressure_ramp]
# used in coolantPressure BC
type = PiecewiseLinear
scale_factor = 1
x = '0 10000.0'
y = '0 1.0'
[]
[]
# ==================================================== #
# Burnup Equation Set
# ==================================================== #
[Burnup]
[burnup]
block = 3
rod_ave_lin_pow = linear_heat_rate_profile
axial_power_profile = axial_peaking_factors
num_radial = 80
num_axial = 49
fuel_inner_radius = 0.0
fuel_outer_radius = 0.0041
fuel_volume_ratio = 1.0
isotopes = 'U235 U238'
isotope_fractions = '3.100e-02 9.690e-01'
RPF = RPF
[]
[]
# ==================================================== #
# Primary Kernels used in Heat Transfer
# ==================================================== #
[Kernels]
[gravity]
type = Gravity
variable = disp_y
value = -9.81
[]
[heat]
# gradient term in heat conduction equation
type = HeatConduction
variable = temp
extra_vector_tags = 'ref'
[]
[heat_ie]
# time term in heat conduction equation
type = HeatConductionTimeDerivative
variable = temp
extra_vector_tags = 'ref'
[]
[heat_source]
type = NeutronHeatSource
fission_rate = fission_rate
variable = temp
extra_vector_tags = 'ref'
block = 3
[]
[]
[AuxKernels]
# ================================================== #
# Pre-Defined Types
# ================================================== #
[pelletid]
type = PelletIdAux
block = 3
variable = pellet_id
number_pellets = 1
execute_on = initial
[]
[fast_neutron_flux]
type = FastNeutronFluxAux
variable = fast_neutron_flux
block = 1
rod_ave_lin_pow = linear_heat_rate_profile
axial_power_profile = axial_peaking_factors
factor = 1.27e+14 # (n/m2-s per W/m)
execute_on = timestep_begin
[]
[fast_neutron_fluence]
type = FastNeutronFluenceAux
variable = fast_neutron_fluence
block = 1
fast_neutron_flux = fast_neutron_flux
execute_on = timestep_begin
[]
[fuel_porosity]
type = PorosityAuxUO2
block = 3
variable = porosity
execute_on = linear
[]
[grain_radius]
type = GrainRadiusAux
block = 3
variable = grain_radius
temperature = temp
execute_on = linear
[]
[gap_conductance]
type = MaterialRealAux
property = gap_conductance
variable = gap_conductivity
boundary = 10
execute_on = linear
[]
[conductance]
type = MaterialRealAux
property = gap_conductance
variable = gap_conductivity
boundary = 10
execute_on = linear
[]
# ================================================== #
# Other General Types
# ================================================== #
[axial_burnup]
type = SpatialUserObjectAux
block = 3
variable = axial_burnup
user_object = axial_burnup
execute_on = timestep_begin
[]
[axial_temperature]
type = SpatialUserObjectAux
block = 3
variable = axial_temperature
user_object = axial_temperature
execute_on = timestep_begin
[]
[]
# ==================================================== #
# Mechanical and Thermal Contact
# ==================================================== #
[Contact]
[pellet_clad_mechanical]
primary = 5
secondary = 10
penalty = 1e14
normalize_penalty = true
normal_smoothing_distance = 0.1
model = frictionless
formulation = Kinematic
[]
[]
[ThermalContact]
[thermal_contact]
type = GasGapHeatTransfer
variable = temp
primary = 5
secondary = 10
roughness_coef = 3.200000e+00
roughness_primary = 1.8e-06
roughness_secondary = 8e-07
jump_distance_model = LANNING
plenum_pressure = plenum_pressure
contact_pressure = contact_pressure
initial_moles = initial_moles
gas_released = fission_gas_released
tangential_tolerance = 0.0001
normal_smoothing_distance = 0.1
order = FIRST
[]
[]
[BCs]
[no_x_all]
type = DirichletBC
variable = disp_x
boundary = 12
value = 0.0
[]
[no_y_fuel_bottom]
type = DirichletBC
variable = disp_y
boundary = 20
value = 0.0
[]
[no_y_clad_bottom]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[]
[convective_clad_surface_bottom]
type = ConvectiveFluxBC
boundary = '1 2 3'
variable = temp
rate = 38200.0 #convection coefficient (h)
initial = 565.0
final = 585.0
duration = 1.0e4 #duration of initial power ramp
[]
[Pressure]
[coolantPressure]
boundary = '1 2 3'
factor = 1.55132e+07
function = coolant_pressure_ramp
[]
[]
[PlenumPressure]
# apply plenum pressure on clad inner walls and pellet surfaces
[plenumPressure]
boundary = 9
initial_pressure = 1.99948e+06
startup_time = 0
R = 8.314462
output_initial_moles = initial_moles
temperature = ave_temp_interior
volume = gas_volume
material_input = fission_gas_released
output = plenum_pressure
[]
[]
[]
# ==================================================== #
# Specification of Material Properties
# ==================================================== #
[Materials]
[fuel_thermal]
type = UO2Thermal
thermal_conductivity_model = NFIR
block = 3
temperature = temp
burnup = burnup
[]
[fuel_elasticity_tensor]
type = ComputeIsotropicElasticityTensor
block = 3
youngs_modulus = 2.0e11
poissons_ratio = 0.345
[]
[fuel_elastic_stress]
type = ComputeFiniteStrainElasticStress
block = 3
[]
[fuel_thermal_expansion]
type = ComputeThermalExpansionEigenstrain
block = 3
thermal_expansion_coeff = 10.0e-6
temperature = temp
stress_free_temperature = 300.0
eigenstrain_name = fuel_thermal_strain
[]
[fuel_relocation]
type = UO2RelocationEigenstrain
block = 3
burnup = burnup
rod_ave_lin_pow = linear_heat_rate_profile
axial_power_profile = axial_peaking_factors
relocation_activation1 = 5000
relocation_model = ESCORE_modified
eigenstrain_name = fuel_relocation_strain
diameter = 0.008192
diametral_gap =0.000168
# Average burnup at which fuel comes into contact with clad at 25kW/m
burnup_relocation_stop = 0.0315
[]
[fuel_volumetric_swelling]
type = UO2VolumetricSwellingEigenstrain
gas_swelling_model_type = SIFGRS
block = 3
temperature = temp
burnup = burnup
initial_fuel_density = 10200.0
eigenstrain_name = fuel_volumetric_strain
total_densification = 0.01
[]
[fission_gas_release]
type = UO2Sifgrs
axial_power_profile = axial_peaking_factors
block = 3
burnup = burnup
fission_rate = fission_rate
hydrostatic_stress = hydrostatic_stress
grain_radius = grain_radius
pellet_brittle_zone = pbz
pellet_id = pellet_id
rod_ave_lin_pow = linear_heat_rate_profile
temperature = temp
[]
[fuel_density]
type = Density
block = 3
[]
[clad_thermal]
type = ZryThermal
block = 1
temperature = temp
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = 1
[]
[clad_stress]
type = ComputeMultipleInelasticStress
tangent_operator = elastic
inelastic_models = 'clad_zrycreep'
block = 1
[]
[clad_zrycreep]
type = ZryCreepLimbackHoppeUpdate
block = 1
temperature = temp
fast_neutron_flux = fast_neutron_flux
fast_neutron_fluence = fast_neutron_fluence
model_irradiation_creep = true
model_primary_creep = true
model_thermal_creep = true
[]
[thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = 1
temperature = temp
stress_free_temperature = 300.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[irradiation_swelling]
type = ZryIrradiationGrowthEigenstrain
block = 1
fast_neutron_fluence = fast_neutron_fluence
zircaloy_material_type = stress_relief_annealed
eigenstrain_name = clad_irradiation_strain
[]
[clad_density]
type = Density
block = 1
density = 7833
[]
[]
# ==================================================== #
# User Objects for Output Processing
# ==================================================== #
[UserObjects]
[pbz]
type = PelletBrittleZone
block = 3
pellet_id = pellet_id
temperature = temp
pellet_radius = 0.0041
number_pellets = 1
execute_on = linear
[]
[averagefissionrate]
type = LayeredAverage
block = 3
variable = fission_rate
direction = y
num_layers = 49
execute_on = timestep_begin
[]
[average_temp]
type = LayeredAverage
block = 3
variable = temp
direction = y
num_layers = 49
execute_on = timestep_begin
[]
[averagebu]
type = LayeredAverage
block = 3
variable = burnup
direction = y
num_layers = 49
execute_on = timestep_begin
[]
[casl_average_fission_rate]
variable = fission_rate
type = LayeredAverage
block = 3
direction = y
bounds = '0.01822 0.05688 0.13899 0.2211 0.30321 0.38533 0.46744 0.54955 0.63166 0.66976 0.75041 0.83106 0.91171 0.99236 1.07301 1.15366 1.19176 1.27241 1.35306 1.43371 1.51436 1.59501 1.67566 1.71376 1.79441 1.87506 1.95571 2.03636 2.11701 2.19766 2.23576 2.31641 2.39706 2.47771 2.55836 2.63901 2.71966 2.75776 2.83841 2.91906 2.99971 3.08036 3.16101 3.24166 3.27976 3.35897 3.43818 3.5174 3.59661 3.67582'
execute_on = timestep_begin
[]
[surface_temp]
type = LayeredSideAverage
boundary = 2
variable = temp
direction = y
bounds = '0.01822 0.05688 0.13899 0.2211 0.30321 0.38533 0.46744 0.54955 0.63166 0.66976 0.75041 0.83106 0.91171 0.99236 1.07301 1.15366 1.19176 1.27241 1.35306 1.43371 1.51436 1.59501 1.67566 1.71376 1.79441 1.87506 1.95571 2.03636 2.11701 2.19766 2.23576 2.31641 2.39706 2.47771 2.55836 2.63901 2.71966 2.75776 2.83841 2.91906 2.99971 3.08036 3.16101 3.24166 3.27976 3.35897 3.43818 3.5174 3.59661 3.67582'
use_displaced_mesh = 0
execute_on = timestep_begin
[]
[axial_temperature]
type = LayeredAverage
block = 3
variable = temp
direction = y
bounds = '0.01822 0.05688 0.13899 0.2211 0.30321 0.38533 0.46744 0.54955 0.63166 0.66976 0.75041 0.83106 0.91171 0.99236 1.07301 1.15366 1.19176 1.27241 1.35306 1.43371 1.51436 1.59501 1.67566 1.71376 1.79441 1.87506 1.95571 2.03636 2.11701 2.19766 2.23576 2.31641 2.39706 2.47771 2.55836 2.63901 2.71966 2.75776 2.83841 2.91906 2.99971 3.08036 3.16101 3.24166 3.27976 3.35897 3.43818 3.5174 3.59661 3.67582'
execute_on = timestep_begin
[]
[axial_burnup]
type = LayeredAverage
block = 3
variable = burnup
direction = y
bounds = '0.01822 0.05688 0.13899 0.2211 0.30321 0.38533 0.46744 0.54955 0.63166 0.66976 0.75041 0.83106 0.91171 0.99236 1.07301 1.15366 1.19176 1.27241 1.35306 1.43371 1.51436 1.59501 1.67566 1.71376 1.79441 1.87506 1.95571 2.03636 2.11701 2.19766 2.23576 2.31641 2.39706 2.47771 2.55836 2.63901 2.71966 2.75776 2.83841 2.91906 2.99971 3.08036 3.16101 3.24166 3.27976 3.35897 3.43818 3.5174 3.59661 3.67582'
execute_on = timestep_begin
[]
[integral_temperature]
type = LayeredAverage
block = 3
variable = temp
direction = y
num_layers = 1
execute_on = timestep_begin
[]
[integral_burnup]
type = LayeredAverage
block = 3
variable = burnup
direction = y
num_layers = 1
execute_on = timestep_begin
[]
[average]
type = LayeredAverage
block = 3
variable = temp
direction = y
bounds = '0.01822 0.05688 0.13899 0.2211 0.30321 0.38533 0.46744 0.54955 0.63166 0.66976 0.75041 0.83106 0.91171 0.99236 1.07301 1.15366 1.19176 1.27241 1.35306 1.43371 1.51436 1.59501 1.67566 1.71376 1.79441 1.87506 1.95571 2.03636 2.11701 2.19766 2.23576 2.31641 2.39706 2.47771 2.55836 2.63901 2.71966 2.75776 2.83841 2.91906 2.99971 3.08036 3.16101 3.24166 3.27976 3.35897 3.43818 3.5174 3.59661 3.67582'
execute_on = timestep_begin
[]
[axial_surface_temperature]
type = LayeredSideAverage
boundary = 2
variable = temp
direction = y
bounds = '0.01822 0.05688 0.13899 0.2211 0.30321 0.38533 0.46744 0.54955 0.63166 0.66976 0.75041 0.83106 0.91171 0.99236 1.07301 1.15366 1.19176 1.27241 1.35306 1.43371 1.51436 1.59501 1.67566 1.71376 1.79441 1.87506 1.95571 2.03636 2.11701 2.19766 2.23576 2.31641 2.39706 2.47771 2.55836 2.63901 2.71966 2.75776 2.83841 2.91906 2.99971 3.08036 3.16101 3.24166 3.27976 3.35897 3.43818 3.5174 3.59661 3.67582'
use_displaced_mesh = 0
execute_on = timestep_begin
[]
[rod_avg_fast_fluence]
type = LayeredSideAverage
boundary = 2
variable = fast_neutron_fluence
direction = y
num_layers = 1
use_displaced_mesh = 0
execute_on = timestep_begin
[]
[casl_clad_surface_heat_flux]
type = LayeredSideDiffusiveFluxAverage
variable = temp
boundary = 2
direction = y
bounds = '0.01822 0.05688 0.13899 0.2211 0.30321 0.38533 0.46744 0.54955 0.63166 0.66976 0.75041 0.83106 0.91171 0.99236 1.07301 1.15366 1.19176 1.27241 1.35306 1.43371 1.51436 1.59501 1.67566 1.71376 1.79441 1.87506 1.95571 2.03636 2.11701 2.19766 2.23576 2.31641 2.39706 2.47771 2.55836 2.63901 2.71966 2.75776 2.83841 2.91906 2.99971 3.08036 3.16101 3.24166 3.27976 3.35897 3.43818 3.5174 3.59661 3.67582'
diffusivity = thermal_conductivity
execute_on = timestep_begin
[]
[]
[Dampers]
[BoundingValueNodalDamper]
type = BoundingValueNodalDamper
variable = temp
max_value = 3200
min_value = 293
[]
[]
# ==================================================== #
# Solver Options
# ==================================================== #
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package -ksp_gmres_restart'
petsc_options_value = 'lu superlu_dist 51'
verbose = true
line_search = 'none'
# controls for linear iterations
l_max_its = 100
l_tol = 8e-3
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-6
nl_abs_tol = 1e-10
# ================================================== #
# Time Step Control
# ================================================== #
start_time = -100
end_time = 5e6
dtmin = 0.1
dtmax = 1e6
dt = 10
[TimeStepper]
type = IterationAdaptiveDT
dt = 1.0e2
optimal_iterations = 1000
time_t = '0 1.0e4 53200 1.0e5'
time_dt = '1.0e3 1.0e3 1.0e3 1.0e5'
[]
[]
[Postprocessors]
# ================================================== #
# Required for Fission Gas Release Models
# ================================================== #
[ave_temp_interior]
# used to compute temperature of plenum
type = SideAverageValue
boundary = 9
variable = temp
outputs = exodus
execute_on = 'initial linear'
[]
[fission_gas_released]
type = ElementIntegralFisGasReleasedSifgrs
block = 3
outputs = exodus
execute_on = linear
[]
[gas_volume]
type = InternalVolume
boundary = 9
outputs = exodus
execute_on = 'initial linear'
[]
[fis_gas_grain]
type = ElementIntegralFisGasGrainSifgrs
block = 3
outputs = exodus
execute_on = linear
[]
[fis_gas_boundary]
type = ElementIntegralFisGasBoundarySifgrs
block = 3
outputs = exodus
execute_on = linear
[]
[_dt]
type = TimestepSize
execute_on = timestep_end
[]
[num_lin_it]
type = NumLinearIterations
[]
[num_nonlin_it]
type = NumNonlinearIterations
[]
[tot_lin_it]
type = CumulativeValuePostprocessor
postprocessor = num_lin_it
[]
[tot_nonlin_it]
type = CumulativeValuePostprocessor
postprocessor = num_nonlin_it
[]
[alive_time]
type = PerfGraphData
section_name = Root
data_type = TOTAL
[]
[]
# ==================================================== #
# Location and format of output
# ==================================================== #
[Outputs]
perf_graph = true
exodus = true
file_base = pin1_output
time_step_interval = 1
[console]
type = Console
max_rows = 25
output_linear = true
[]
[]
[MultiApps]
[sub]
type = TransientMultiApp
app_type = BisonApp
execute_on = timestep_end
positions = '10 0 0'
input_files = 'pin2.i'
[]
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-04/puzry-04_aniso.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-04.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 2000. '
y = '1.e+05 1.e+05 7.2e+05' # Linear increase at 0.062 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 2000. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
# Circumferential steady-state creep test and analysis of Zircaloy-4 fuel cladding
# Nuclear Engineering and Design, 53, 2312-2322 (2021)
[F]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.738 0.738 0.57'
[]
[G]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.174 0.174 0.45'
[]
[H]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.588 0.588 0.48'
[]
[L]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[M]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[N]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = TaylorExpansion
use_automatic_differentiation = true
[]
[]
[]
[]
[Kernels]
[heat]
type = ADHeatConduction
variable = temperature
[]
[heat_ie]
type = ADHeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = ADMaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = ADMaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = ADMaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = ADMaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = ADMaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = ADFunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = ADDirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = ADDirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ADZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1.e+11
poissons_ratio = 0.3
block = 1
[]
[hill_constants]
type = ADHillConstants
hill_constants = "0.738 0.174 0.588 1.0 1.0 1.0"
function_names = "F G H L M N"
temperature = temperature
[]
[creep_update]
type = ADZryAnisoCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 1.5e-05
temperature = temperature
temperature_standard_thermal_creep_end = 700
temperature_loca_creep_begin = 900.
fract_beta_phase_name = 'fract_beta_phase'
max_integration_error = 1000000.0
absolute_tolerance = 1e-13
relative_tolerance = 1e-11
[]
[creep]
type = ADComputeMultipleInelasticStress
block = 1
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ADZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = ADDensity
block = 1
[]
[phase]
type = ADZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ADZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = NEWTON
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0.
n_startup_steps = 1
end_time = 2500.
dtmax = 1.
dtmin = 1.0e-9
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-04_aniso_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-08/puzry-08_aniso.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-08.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 1200. '
y = '1.e+05 1.e+05 1.626e+06' # Linear increase at 0.0763 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 1200. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
# Circumferential steady-state creep test and analysis of Zircaloy-4 fuel cladding
# Nuclear Engineering and Design, 53, 2312-2322 (2021)
[F]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.738 0.738 0.57'
[]
[G]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.174 0.174 0.45'
[]
[H]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.588 0.588 0.48'
[]
[L]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[M]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[N]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = TaylorExpansion
use_automatic_differentiation = true
[]
[]
[]
[]
[Kernels]
[heat]
type = ADHeatConduction
variable = temperature
[]
[heat_ie]
type = ADHeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = ADMaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = ADMaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = ADMaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = ADMaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = ADMaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = ADFunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = ADDirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = ADDirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ADZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1.e+11
poissons_ratio = 0.3
block = 1
[]
[hill_constants]
type = ADHillConstants
hill_constants = "0.738 0.174 0.588 1.0 1.0 1.0"
function_names = "F G H L M N"
temperature = temperature
[]
[creep_update]
type = ADZryAnisoCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 3.45e-05
temperature = temperature
temperature_standard_thermal_creep_end = 700
temperature_loca_creep_begin = 900.
fract_beta_phase_name = 'fract_beta_phase'
max_integration_error = 1000000.0
absolute_tolerance = 1e-07
relative_tolerance = 1e-07
[]
[creep]
type = ADComputeMultipleInelasticStress
block = 1
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ADZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = ADDensity
block = 1
[]
[phase]
type = ADZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ADZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = NEWTON
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0.
n_startup_steps = 1
end_time = 2500.
dtmax = 1.
dtmin = 1.0e-9
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-08_aniso_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/LOCA_Hardy_cladding_test/analysis/13pt8MPa/25C_sec/25C_sec_Hardy_Tube_Test_13pt8MPa.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
volumetric_locking_correction = false
displacements = 'disp_x disp_y'
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
group_variables = 'disp_x disp_y'
[]
[Mesh]
coord_type = RZ
patch_size = 10
patch_update_strategy = iteration
partitioner = centroid
centroid_partitioner_direction = y
[gen]
type = FuelPinMeshGenerator
include_fuel = false
include_clad = true
pellet_outer_radius = 0.0072527
clad_gap_width = 0.0
clad_top_gap_height = 0.0
clad_bot_gap_height = 0.0
clad_thickness = 0.38e-3
pellet_height = 0.5
pellet_quantity = 1
clad_mesh_density = customize
nx_c = 2
ny_c = 50
elem_type = QUAD8
[]
[]
[Variables]
[temperature]
initial_condition = 600.0
[]
[]
[AuxVariables]
[creep_rate_aux]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[total_hoop_strain]
order = CONSTANT
family = MONOMIAL
[]
[burst_stress]
order = CONSTANT
family = MONOMIAL
[]
[burst]
order = CONSTANT
family = MONOMIAL
[]
[]
[Functions]
[pressure_function]
type = PiecewiseLinear
x = '0 40'
y = '1 1'
[]
[temp_function]
type = PiecewiseLinear
y = '600 1600'
[]
[temperature_profile]
type = PiecewiseBilinear
y = '0 40'
x = '0 0.25224 0.50448'
z = '0.995 1.01 0.995 0.995 1.01 0.995'
axis = 1
[]
[inner_temperature]
type = CompositeFunction
functions = 'temp_function temperature_profile'
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[clad]
block = clad
add_variables = true
strain = FINITE
decomposition_method = EigenSolution
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz elastic_strain_xx elastic_strain_yy elastic_strain_zz
creep_strain_xx creep_strain_yy creep_strain_zz hoop_stress'
extra_vector_tags = 'ref'
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
extra_vector_tags = 'ref'
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
extra_vector_tags = 'ref'
[]
[]
[AuxKernels]
[creep_rate_aux]
type = MaterialRealAux
variable = creep_rate_aux
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[creep_rate]
type = MaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[total_hoop_strain]
type = RankTwoAux
rank_two_tensor = total_strain
variable = total_hoop_strain
index_i = 2
index_j = 2
execute_on = timestep_end
block = clad
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = clad_outside_right
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = clad_outside_right
execute_on = timestep_end
[]
[]
[BCs]
[Pressure]
[outer_surface]
boundary = 'clad_outside_bottom clad_outside_right clad_outside_top'
factor = 0.0
function = pressure_function
[]
[inner_surface]
boundary = 'clad_inside_right clad_inside_bottom clad_inside_top'
function = pressure_function
[]
[]
[u_bottom_fix]
type = DirichletBC
variable = disp_y
boundary = 1001
value = 0.0
[]
[x_fix]
type = DirichletBC
variable = disp_x
boundary = centerline
value = 0.0
[]
[temp_bc]
type = FunctionDirichletBC
function = inner_temperature
variable = temperature
boundary = 'clad_inside_bottom clad_inside_right clad_inside_top'
[]
[]
[Materials]
[clad_thermal]
type = ZryThermal
block = clad
zry_thermal_properties_model = MATPRO
temperature = temperature
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = clad
matpro_youngs_modulus = true
matpro_poissons_ratio = true
temperature = temperature
[]
[clad_stress]
type = ComputeMultipleInelasticStress
inelastic_models = 'clad_zrycreep'
block = clad
tangent_operator = nonlinear
[]
[clad_zrycreep]
type = ZryCreepLOCAUpdate
block = clad
temperature = temperature
model_irradiation_creep = false
model_primary_creep = true
model_thermal_creep = true
temperature_loca_creep_begin = 840 # values from the report
temperature_standard_thermal_creep_end = 975
[]
[thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = clad
temperature = temperature
stress_free_temperature = 600.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[clad_density]
type = Density
block = clad
density = 6550.0
[]
[phase]
type = ZrPhase
block = clad
temperature = temperature
numerical_method = 2
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = clad_outside_right
failure_criterion = combined_overstress_and_overstrain
hoop_stress = hoop_stress
hoop_creep_strain = creep_strain_zz
effective_strain_rate_creep = creep_rate_aux
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.0e-5
nl_abs_tol = 1.0e-8
start_time = 0
n_startup_steps = 1
end_time = 40
dtmax = 1
dtmin = 0.0000001
[TimeStepper]
type = IterationAdaptiveDT
timestep_limiting_postprocessor = material_timestep
dt = 1.0
[]
[]
[Postprocessors]
[ave_clad_temp]
type = SideAverageValue
boundary = clad_outside_right
variable = temperature
[]
[gas_volume]
type = InternalVolume
boundary = all_clad_interior
execute_on = 'initial linear'
[]
[max_clad_temp]
type = NodalExtremeValue
block = clad
value_type = max
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = clad
[]
[max_hoop_stress]
type = ElementExtremeValue
block = clad
value_type = max
variable = hoop_stress
[]
[vonmises_stress_clad]
type = ElementAverageValue
block = clad
variable = vonmises_stress
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = total_hoop_strain
[]
[max_disp_x]
type = NodalExtremeValue
block = clad
value_type = max
variable = disp_x
[]
[min_burst_stress]
type = ElementExtremeValue
block = clad
value_type = min
variable = burst_stress
[]
[burst]
type = ElementExtremeValue
block = clad
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = clad
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
[]
[PerformanceMetricOutputs]
[]
[Outputs]
color = false
perf_graph = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[csv]
type = CSV
[]
[chkfile]
type = CSV
show = 'max_disp_x max_hoop_stress vonmises_stress_clad'
execute_on = 'FINAL'
[]
[]
[UserObjects]
[terminator1]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '5'
include_fuel = false
[]
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-10/puzry-10.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-10.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 1200. '
y = '1.e+05 1.e+05 1.52e+06' # Linear increase at 0.0710 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 1200. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = EigenSolution
[]
[]
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = MaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = FunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = DirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = DirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1.e+11
poissons_ratio = 0.3
block = 1
[]
[creep_update]
type = ZryCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 1.e-04
temperature = temperature
temperature_standard_thermal_creep_end = 700
temperature_loca_creep_begin = 900.
[]
[creep]
type = ComputeMultipleInelasticStress
block = 1
tangent_operator = elastic
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = Density
block = 1
[]
[phase]
type = ZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
active = 'smp'
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0.
n_startup_steps = 1
end_time = 1200.
dtmax = 1.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-10_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-12/puzry-12.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-12.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 1200. '
y = '1.e+05 1.e+05 1.546e+06' # Linear increase at 0.0723 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 1200. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = EigenSolution
[]
[]
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = MaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = FunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = DirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = DirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1.e+11
poissons_ratio = 0.3
block = 1
[]
[creep_update]
type = ZryCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 1.e-04
temperature = temperature
temperature_standard_thermal_creep_end = 700
temperature_loca_creep_begin = 900.
[]
[creep]
type = ComputeMultipleInelasticStress
block = 1
tangent_operator = elastic
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = Density
block = 1
[]
[phase]
type = ZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
active = 'smp'
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0.
n_startup_steps = 1
end_time = 1200.
dtmax = 1.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-12_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/RIA_NSRR_FK/analysis/FK9/FK09.i)
# This file was created using BIF with the following inputs:
# FK06/FK06.var - md5sum: 5a60c05af67ba840a89caacf70b852e2
# pulse.tpl - md5sum: 37e5a6b8a0c63ad020906dada3472585
[GlobalParams]
density = 10310.8809782
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
energy_per_fission = 3.2e-11
a_lower = 0.01822
a_upper = 0.12422
temperature = temp
volumetric_locking_correction = false
[]
[Mesh]
coord_type = RZ
[smeared_pellet_mesh]
type = FuelPinMeshGenerator
clad_mesh_density = customize
pellet_mesh_density = customize
elem_type = QUAD8
ny_p = 100
nx_c = 4
ny_c = 100
nx_p = 12
ny_cu = 3
ny_cl = 3
bx_p = 0.75
clad_bot_gap_height = 0.00152
bottom_clad_height = 0.0167
top_clad_height = 0.0167
clad_thickness = 0.00086
pellet_outer_radius = 0.00527
clad_top_gap_height = 0.05265
pellet_height = 0.106
clad_gap_width = 1e-05
pellet_quantity = 1
[]
patch_size = 5
patch_update_strategy = auto
partitioner = centroid
centroid_partitioner_direction = y
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
converge_on = 'disp_x disp_y temp'
[]
[Variables]
[temp]
initial_condition = 293
block = '1 3'
[]
[]
[AuxVariables]
[BuTC]
[]
[gap]
order = CONSTANT
family = MONOMIAL
[]
[fast_neutron_flux]
block = 1
[]
[fast_neutron_fluence]
block = 1
[]
[buavg]
order = CONSTANT
family = MONOMIAL
[]
[fission_rate]
initial_condition = 0
[]
[grain_radius]
block = 3
initial_condition = 5.96e-6
[]
[integral_burnup]
order = CONSTANT
family = MONOMIAL
[]
[pellet_id]
order = CONSTANT
family = MONOMIAL
block = 3
[]
[porosity]
order = CONSTANT
family = MONOMIAL
initial_condition = 0.0592261881186
[]
[SED]
order = CONSTANT
family = MONOMIAL
[]
[]
[Functions]
[linear_heat_rate_profile]
type = PiecewiseLinear
data_file = pulse.csv
format = columns
[]
[flux]
type = ConstantFunction
value = 0.0
[]
[axial_peaking_factors]
type = ConstantFunction
value = 1
[]
[coolant_pressure_ramp]
type = ConstantFunction
value = 101325
[]
[linear_heat_generation_rate]
type = CompositeFunction
functions = 'linear_heat_rate_profile axial_peaking_factors'
[]
[axial_flux]
type = CompositeFunction
functions = 'flux axial_peaking_factors'
[]
[burnup_thermal_conductivity]
type = ConstantFunction
value = 1 # should be burnup / 950
[]
[radial_power_profile]
type = PiecewiseLinear
data_file = RadialPowerProfile.csv
format = columns
axis = X
[]
[radial_burnup_profile]
type = PiecewiseLinear
data_file = RadialBurnupProfile.csv
format = columns
axis = X
[]
[initial_burnup]
type = CompositeFunction
functions = 'burnup_thermal_conductivity radial_burnup_profile'
[]
[]
[Burnup]
[burnup]
block = 3
rod_ave_lin_pow = linear_heat_rate_profile
axial_power_profile = axial_peaking_factors
rpf_input = radial_power_profile
num_radial = 80
num_axial = 49
fuel_inner_radius = 0.0
fuel_outer_radius = 0.00527
fuel_volume_ratio = 1.0
isotopes = 'U235 U238 Pu239 Pu240 Pu241 Pu242'
isotope_fractions = '0.045 0.955 0.0 0.0 0.0 0.0'
[]
[]
[Physics/SolidMechanics/QuasiStatic]
add_variables = true
[fuel]
block = 3
strain = FINITE
incremental = true
eigenstrain_names = 'fuel_thermal_eigenstrain
fuel_volumetric_swelling_eigenstrain'
extra_vector_tags = 'ref'
generate_output = 'vonmises_stress hydrostatic_stress elastic_strain_xx
elastic_strain_yy elastic_strain_zz stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz'
decomposition_method = EigenSolution
[]
[clad]
block = 1
strain = FINITE
incremental = true
eigenstrain_names = 'clad_thermal_eigenstrain'
extra_vector_tags = 'ref'
generate_output = 'vonmises_stress elastic_strain_xx
elastic_strain_yy elastic_strain_zz stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz creep_strain_xx creep_strain_yy creep_strain_zz'
decomposition_method = EigenSolution
[]
[]
[Kernels]
[gravity]
type = Gravity
variable = disp_y
value = -9.81
block = '1 3'
extra_vector_tags = 'ref'
[]
[heat]
type = HeatConduction
variable = temp
block = '1 3'
extra_vector_tags = 'ref'
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temp
block = '1 3'
extra_vector_tags = 'ref'
[]
[heat_source]
type = NeutronHeatSource
fission_rate = fission_rate
variable = temp
block = 3
extra_vector_tags = 'ref'
[]
[]
[AuxKernels]
[BuTC]
type = FunctionAux
block = 3
variable = BuTC
function = initial_burnup
[]
[pelletid]
type = PelletIdAux
block = 3
variable = pellet_id
number_pellets = 1
execute_on = initial
[]
[gap]
type = SpatialUserObjectAux
block = 3
variable = gap
execute_on = timestep_end
user_object = avg_gap
[]
[buavg]
type = SpatialUserObjectAux
block = 3
variable = buavg
execute_on = timestep_end
user_object = integral_burnup
[]
[fast_neutron_flux]
type = FastNeutronFluxAux
variable = fast_neutron_flux
function = axial_flux
block = 1
execute_on = timestep_begin
[]
[fast_neutron_fluence]
type = FastNeutronFluenceAux
variable = fast_neutron_fluence
block = 1
fast_neutron_flux = fast_neutron_flux
execute_on = timestep_begin
[]
[fuel_porosity]
type = PorosityAuxUO2
block = 3
variable = porosity
execute_on = timestep_begin
[]
[grain_radius]
type = GrainRadiusAux
block = 3
variable = grain_radius
temperature = temp
execute_on = timestep_begin
[]
[SED]
type = MaterialRealAux
variable = SED
property = strain_energy_density
execute_on = timestep_end
block = 1
[]
[]
[Contact]
[mechanical]
model = coulomb
formulation = mortar
primary = 5
secondary = 10
friction_coefficient = 0.4
c_normal = 1e+12
c_tangential = 1e+24
tangential_lm_scaling = 1.0e-16
normal_lm_scaling = 1.0e-10
[]
[]
[ThermalContactMortar]
[thermal_contact]
secondary_variable = temp
primary_boundary = '5'
secondary_boundary = '10'
layer_thickness = layer_thickness_action
roughness_coef = 3.2
roughness_primary = 1.5e-6
roughness_secondary = 1.75e-6
jump_distance_model = LANNING
plenum_pressure = plenum_pressure
initial_moles = initial_moles
initial_gas_types = 'He Ar'
initial_fractions = '0.25 0.75'
gas_released = fission_gas_released
contact_pressure = mechanical_normal_lm
thermal_lm_scaling = 1.0e-2
[]
[]
[BCs]
[no_x_all]
type = DirichletBC
variable = disp_x
boundary = 12
value = 0.0
[]
[no_y_fuel_bottom]
type = DirichletBC
variable = disp_y
boundary = 20
value = 0.0
[]
[no_y_clad_bottom]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[]
[coolant_temp]
type = DirichletBC
boundary = '1 2 3'
variable = temp
value = 293
[]
[Pressure]
[coolantPressure]
boundary = '1 2 3'
factor = 1
function = coolant_pressure_ramp
[]
[]
[PlenumPressure]
[plenumPressure]
boundary = '10 5'
initial_pressure = 0.1e6
startup_time = 0
R = 8.314462
output_initial_moles = initial_moles
temperature = plenum_temperature
volume = plenum_volume
material_input = fission_gas_released
output = plenum_pressure
initial_temperature = 293
[]
[]
[]
[Materials]
[fuel_swelling]
type = UO2VolumetricSwellingEigenstrain
block = 3
burnup = burnup
initial_fuel_density = 10310.8809782
total_densification = 0.006
gas_swelling_model_type = SIFGRS
eigenstrain_name = 'fuel_volumetric_swelling_eigenstrain'
[]
[fuel_thermal]
type = UO2Thermal
thermal_conductivity_model = NFIR
block = 3
temperature = temp
burnup = BuTC
initial_porosity = 0.0592261881186
[]
[fuel_elasticity_tensor]
type = UO2ElasticityTensor
block = 3
[]
[fuel_thermal_expansion]
type = UO2ThermalExpansionMartinEigenstrain
block = 3
stress_free_temperature = 293
eigenstrain_name = 'fuel_thermal_eigenstrain'
[]
[fuel_elastic_stress]
type = ComputeFiniteStrainElasticStress
block = '3'
[]
[clad_thermal]
type = ZryThermal
block = 1
temperature = temp
[]
[clad_inelastic_stress]
type = ComputeMultipleInelasticStress
block = 1
tangent_operator = elastic
inelastic_models ='plasticity'
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = 1
fast_neutron_fluence = fast_neutron_fluence
initial_fast_fluence = 1.30e26
cold_work_factor = 0.01
matpro_youngs_modulus = true
matpro_poissons_ratio = true
[]
## TODO: Creep is not active, but is transfered from the SM version.
## Adding creep causes the Peak Hoop strain to best match the FALCON
## results given by R. Montgomery and D. Sunderland. Only retaining
## plasticity matches the results from Wenfeng Liu, John Alvis, Robert Montgomery, and Ken Yueh
[clad_creep_stress]
type = ZryCreepLimbackHoppeUpdate
block = 1
fast_neutron_flux = fast_neutron_flux
fast_neutron_fluence = fast_neutron_fluence
initial_fast_fluence = 1.30e26
[]
[clad_thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 293.0
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[plasticity]
type = ZryPlasticityUpdate
block = 1
initial_fast_fluence = 1.30e26
fast_neutron_flux = fast_neutron_flux
fast_neutron_fluence = fast_neutron_fluence
cold_work_factor = .01
plasticity_model_type = MATPRO
output_properties = yield_stress
outputs = all
zircaloy_alloy_type = 4
[]
[fission_gas_release]
type = UO2Sifgrs
block = 3
temperature = temp
fission_rate = fission_rate
grain_radius = grain_radius
gbs_model = true
burnup = BuTC
transient_option = MICROCRACKING
[]
[clad_density]
type = Density
block = 1
density = 6551
[]
[fuel_density]
type = Density
block = 3
[]
[strain_energy_density]
type = StrainEnergyDensity
block = '1 3'
incremental = true
[]
[]
[UserObjects]
[avg_gap]
type = LayeredAverage
block = 3
variable = penetration
direction = y
num_layers = 48
[]
[pbz]
type = PelletBrittleZone
block = 3
pellet_id = pellet_id
temperature = temp
pellet_radius = 0.00527
number_pellets = 1
execute_on = timestep_begin
[]
[integral_burnup]
type = LayeredAverage
block = 3
variable = burnup
direction = y
num_layers = 1
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_converged_reason -ksp_converged_reason -snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package -mat_mffd_err -pc_factor_shift_type '
'-pc_factor_shift_amount'
petsc_options_value = 'lu superlu_dist 1e-5 NONZERO 1e-12'
line_search = 'none'
l_max_its = 40
l_tol = 8e-3
nl_max_its = 40
nl_rel_tol = 1e-3
nl_abs_tol = 1e-10
dtmin = 0.00001
dtmax = 1.0
start_time = 0
end_time = 100
[TimeStepper]
type = IterationAdaptiveDT
dt = 0.0001
optimal_iterations = 200
linear_iteration_ratio = 100
timestep_limiting_function = linear_heat_rate_profile
max_function_change = 500000
force_step_every_function_point = true
[]
[]
[Dampers]
[limitT]
type = MaxIncrement
max_increment = 200.0
variable = temp
[]
[limitX]
type = MaxIncrement
max_increment = 1e-4
variable = disp_x
[]
[]
[Postprocessors]
[max_hoop_strain]
type = ElementExtremeValue
variable = strain_zz
block = 1
[]
[max_SED]
type = ElementExtremeValue
variable = SED
block = 1
[]
[average_grain_radius]
type = ElementAverageValue
block = 3
outputs = 'exodus'
variable = grain_radius
[]
[clad_inner_vol]
type = InternalVolume
boundary = 7
outputs = 'exodus'
execute_on = 'timestep_begin initial'
[]
[flux_from_clad]
type = SideDiffusiveFluxIntegral
variable = temp
boundary = 5
diffusivity = thermal_conductivity
outputs = 'exodus'
[]
[flux_from_fuel]
type = SideDiffusiveFluxIntegral
variable = temp
boundary = 10
diffusivity = thermal_conductivity
outputs = 'exodus'
[]
[rod_total_power]
type = ElementIntegralPower
variable = temp
fission_rate = fission_rate
block = 3
[]
[rod_input_power]
type = FunctionValuePostprocessor
function = linear_heat_rate_profile
scale_factor = 0.106
[]
[average_fission_rate]
type = ElementAverageValue
variable = fission_rate
block = '3'
[]
[RAE]
type = RadialAverageEnthalpy
vector_postprocessor = rad_temp
radial_direction = x
axial_direction = y
axial_position = 0.0503
temperature_name = temp
[]
[peak_RAE]
type = TimeExtremeValue
postprocessor = RAE
[]
[]
[VectorPostprocessors]
[rad_temp]
type = NodalValueSampler
block = 3
sort_by = y
variable = temp
execute_on = timestep_end
outputs = dummy
[]
[]
[StandardLWRFuelRodOutputs]
fuel_pellet_blocks = 3
cladding_blocks = 1
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[chkfile]
type = CSV
show = 'average_centerline_fuel_temperature average_fission_rate fission_gas_released_percentage peak_RAE rod_total_power'
execute_on = 'FINAL'
[]
[console]
type = Console
max_rows = 25
output_linear = true
[]
[dummy]
type = CSV
enable = false
[]
[]
(assessment/LWR/validation/LOCA_REBEKA_cladding_burst_tests/analysis/rebeka_2d_04MPa/rebeka_singlerod_2d_04MPa.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
order = SECOND
family = LAGRANGE
displacements = 'disp_x disp_y'
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = rebeka_singlerod.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 573.0
[]
[]
[Functions]
[temperature_func]
type = PiecewiseLinear
x = '0. 700. '
y = '573. 1273.' # From 300 to 1000 C at 1 K/s
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 700. '
y = '4.e+06 4.e+06' # 40 bar
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 700. '
y = '1.e+05 1.e+05' # atmospheric pressure
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[clad]
block = cladding
add_variables = false
strain = FINITE
decomposition_method = EigenSolution
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz hoop_stress'
[]
[]
[AuxVariables]
[creep_rate_aux]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[scale_thickness]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfract_total]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfgain_total]
order = CONSTANT
family = MONOMIAL
[]
[burst_stress]
order = CONSTANT
family = MONOMIAL
[]
[burst]
order = CONSTANT
family = MONOMIAL
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate_aux]
type = MaterialRealAux
variable = creep_rate_aux
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[scl_thickness]
type = MaterialRealAux
variable = scale_thickness
property = oxide_scale_thickness
boundary = 2
[]
[ofract_total]
type = MaterialRealAux
variable = oxywtfract_total
property = current_oxygen_weight_frac_total
boundary = 2
[]
[ofgain_total]
type = MaterialRealAux
boundary = 2
variable = oxywtfgain_total
property = oxygen_weight_frac_gained_total
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = 2
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = 2
execute_on = timestep_end
[]
[]
[BCs]
[inner_temperature]
type = REBEKADirichletBC
variable = temperature
function_tempm = temperature_func
minimum_temperature = 573.0
translation = 0.1625
boundary = 4
[]
[no_y_midsection]
type = DirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply steam pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 101 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[CoolantChannel]
[convective_clad_surface]
boundary = 2
variable = temperature
inlet_temperature = 473.
inlet_pressure = 1.e+05
inlet_massflux = 1.0 # kg/m^2-sec # almost stagnant steam
rod_diameter = 10.75e-03
rod_pitch = 1.26e-02 # default
number_axial_zone = 15
oxide_thickness = scale_thickness
[]
[]
[Materials]
[thermal]
type = ZryThermal
block = cladding
temperature = temperature
[]
[clad_elasticity_tensor]
type = ComputeIsotropicElasticityTensor
block = cladding
youngs_modulus = 1.0e11
poissons_ratio = 0.3
[]
[clad_stress]
type = ComputeMultipleInelasticStress
tangent_operator = elastic
inelastic_models = 'clad_zrycreep'
block = cladding
[]
[clad_zrycreep]
type = ZryCreepLOCAUpdate
block = cladding
temperature = temperature
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
temperature_loca_creep_begin = 501 # see Erbacher et al., 1982
temperature_standard_thermal_creep_end = 500
[]
[thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = cladding
temperature = temperature
stress_free_temperature = 573.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[density]
type = Density
block = cladding
[]
[phase]
type = ZrPhase
block = cladding
temperature = temperature
numerical_method = 2
[]
[oxidation]
type = ZryOxidation
boundary = 2
temperature = temperature
clad_inner_radius = 0.00465
clad_outer_radius = 0.005375
normal_operating_temperature_model = epri_kwu_ce
high_temperature_model = leistikow
use_coolant_channel = true
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = 2
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate_aux
temperature = temperature
fraction_beta_phase = fract_beta_phase
fraction_oxygen_gain = oxywtfgain_total
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0
n_startup_steps = 1
end_time = 700.
dtmax = 1.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average temperature of cladding exterior
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = cladding
[]
[max_clad_temp]
type = NodalExtremeValue
block = cladding
value_type = max
variable = temperature
[]
[max_oxygen_fract]
type = ElementExtremeValue
block = cladding
value_type = max
variable = oxywtfract_total
[]
[max_betaph_fract]
type = ElementExtremeValue
block = cladding
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
block = cladding
value_type = max
variable = creep_rate_aux
[]
[max_creep_strain_mag]
type = ElementExtremeValue
block = cladding
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
block = cladding
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
block = cladding
value_type = max
variable = hoop_stress
[]
[vonmises_stress_clad]
type = ElementAverageValue
block = cladding
variable = vonmises_stress
[]
[min_burst_stress]
type = ElementExtremeValue
block = cladding
value_type = min
variable = burst_stress
[]
[burst]
type = ElementExtremeValue
block = cladding
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = cladding
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = cladding
plenum_boundary_name = 4
external_clad_boundary_name = 2
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = rebeka_2d_04MPa_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
(assessment/LWR/validation/LOCA_Studsvik/analysis/rod_196/Studsvik_196_part1_1p5d_fr_ffrd.i)
[GlobalParams]
density = 10431.0
initial_porosity = 0.05
order = SECOND
family = LAGRANGE
energy_per_fission = 3.2e-11 # J/fission
volumetric_locking_correction = false
displacements = 'disp_x'
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
[]
[Mesh]
coord_type = RZ
[layered1D_mesh]
type = Layered1DMeshGenerator
slices_per_block = 10
clad_gap_width = 80e-6
plenum_height = 0.0393576
pellet_outer_radius = 3.92e-3
clad_thickness = 0.57e-3
fuel_height = 0.2606424
# nx_c = 2
# nx_p = 11
elem_type = EDGE3
[]
patch_update_strategy = auto
patch_size = 10 # For contact algorithm
partitioner = centroid
centroid_partitioner_direction = y
[]
[Variables]
# Define dependent variables and initial conditions
[temperature]
initial_condition = 295.0 # set initial temp to coolant inlet
[]
[]
[AuxVariables]
# Define auxilary variables
[strain_yy_0]
order = CONSTANT
family = MONOMIAL
[]
[tangential_contact_pressure_aux]
block = fuel
[]
[fast_neutron_flux]
block = clad
[]
[fast_neutron_fluence]
block = clad
[]
[grain_radius]
block = fuel
initial_condition = 10e-6
[]
[creep_strain_rate]
order = CONSTANT
family = MONOMIAL
[]
[effective_creep_strain]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[hoop_strain]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[scale_thickness] # ZrO2 scale thickness (m)
order = CONSTANT
family = MONOMIAL
[]
[oxywtfract_total] # Current oxigen weight fraction (oxide+metal) (/)
order = CONSTANT
family = MONOMIAL
[]
[oxywtfgain_total] # Gained oxygen weight fraction (oxide+metal) (/)
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[gap_cond]
order = CONSTANT
family = MONOMIAL
[]
[]
[Functions]
[power_history]
type = PiecewiseLinear
data_file = power_history.csv
format = columns
scale_factor = 1
[]
[axial_peaking_factors]
type = ParsedFunction
expression = 1
[]
[pressure_ramp] # reads and interpolates input data defining amplitude curve for fill gas pressure
type = PiecewiseLinear
x = '-200 0 86400 47386400 47472800 47559200 47645600 94945600 95032000'
y = '0.0065371 1 1 1 1 1 1 1 0.0065371'
scale_factor = 15.5e6
[]
[forced_times]
type = PiecewiseLinear
data_file = timestep_limiting.csv
scale_factor = 1
format = columns
[]
[clad_axial_pressure]
type = CladdingAxialPressureFunction
plenum_pressure = plenum_pressure
coolant_pressure = pressure_ramp
coolant_pressure_scaling_factor = 1.0
fuel_pin_geometry = fuel_pin_geometry
[]
[fuel_axial_pressure]
type = ParsedFunction
expression = plenum_pressure
symbol_names = plenum_pressure
symbol_values = plenum_pressure
[]
[]
[Physics]
[SolidMechanics]
[Layered1D]
[fuel]
block = fuel
add_variables = true
add_scalar_variables = true
strain = FINITE
out_of_plane_strain_name = strain_yy
eigenstrain_names = 'fuel_thermal_eigenstrain fuel_volumetric_eigenstrain axial_relocation_eigenstrain'
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress strain_xx hoop_stress creep_strain_zz strain_zz'
extra_vector_tags = 'ref'
fuel_pin_geometry = fuel_pin_geometry
group_scalar_vars_in_reference_residual = true
mesh_generator = layered1D_mesh
decomposition_method = EigenSolution
temperature = temperature
out_of_plane_pressure_function = fuel_axial_pressure
layer_friction_user_object = 1DFriction_secondary
[]
[clad]
block = clad
add_variables = true
add_scalar_variables = true
strain = FINITE
out_of_plane_strain_name = strain_yy
eigenstrain_names = 'clad_thermal_eigenstrain clad_irradiation_eigenstrain'
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress strain_xx hoop_stress creep_strain_zz strain_zz'
extra_vector_tags = 'ref'
fuel_pin_geometry = fuel_pin_geometry
group_scalar_vars_in_reference_residual = true
mesh_generator = layered1D_mesh
decomposition_method = EigenSolution
temperature = temperature
out_of_plane_pressure_function = clad_axial_pressure
layer_friction_user_object = 1DFriction_primary
[]
[]
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
extra_vector_tags = 'ref'
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
extra_vector_tags = 'ref'
[]
[heat_source]
type = NeutronHeatSource
variable = temperature
extra_vector_tags = 'ref'
block = fuel
burnup_function = burnup
axial_relocation_object = axial_relocation
[]
[]
[Burnup]
[burnup]
block = fuel
rod_ave_lin_pow = power_history # using the power function defined above
axial_power_profile = axial_peaking_factors # using the axial power profile function defined above
num_radial = 80
num_axial = 11
fuel_pin_geometry = fuel_pin_geometry
fuel_volume_ratio = 1.0 # for use with dished fuels (ratio of actual volume to cylinder volume)
order = CONSTANT
family = MONOMIAL
RPF = RPF
isotopes = 'U235 U238 Pu239 Pu240 Pu241 Pu242'
isotope_fractions = '0.05 0.95 0 0 0 0'
[]
[]
[AuxKernels]
# Define auxilliary kernels for each of the aux variables
[fast_neutron_flux]
type = FastNeutronFluxAux
variable = fast_neutron_flux
block = clad
rod_ave_lin_pow = power_history
axial_power_profile = axial_peaking_factors
factor = 3e13
execute_on = timestep_begin
[]
[fast_neutron_fluence]
type = FastNeutronFluenceAux
variable = fast_neutron_fluence
block = clad
fast_neutron_flux = fast_neutron_flux
execute_on = timestep_begin
[]
[grain_radius]
type = GrainRadiusAux
block = fuel
variable = grain_radius
temperature = temperature
execute_on = linear
[]
[creep_strain_rate]
type = MaterialRealAux
property = creep_rate
variable = creep_strain_rate
block = clad
[]
[effective_creep_strain]
type = MaterialRealAux
property = effective_creep_strain
variable = effective_creep_strain
block = clad
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
block = clad
variable = fract_beta_phase
property = fract_beta_phase
[]
[scl_thickness]
type = MaterialRealAux
boundary = 2
variable = scale_thickness
property = oxide_scale_thickness
[]
[ofract_total]
type = MaterialRealAux
boundary = 2
variable = oxywtfract_total
property = current_oxygen_weight_frac_total
[]
[ofgain_total]
type = MaterialRealAux
boundary = 2
variable = oxywtfgain_total
property = oxygen_weight_frac_gained_total
[]
[sigmaburst]
type = MaterialRealAux
boundary = 2
variable = burst_stress
property = burst_stress
[]
[hasburst]
type = MaterialRealAux
boundary = 2
variable = burst
property = failed
execute_on = timestep_end
[]
[conductance]
type = MaterialRealAux
property = gap_conductance
variable = gap_cond
boundary = 10
execute_on = 'linear'
[]
[tangential_contact_pressure_aux]
type = SpatialUserObjectAux
variable = tangential_contact_pressure_aux
user_object = 1DFriction_secondary
block = fuel
execute_on = 'TIMESTEP_END'
[]
[]
[Contact]
[pellet_clad_mechanical]
primary = 5
secondary = 10
formulation = kinematic
model = frictionless
penalty = 1e7
[]
[]
[ThermalContact]
[thermal_contact]
type = GasGapHeatTransfer
variable = temperature
primary = 5
secondary = 10
initial_moles = initial_moles
gas_released = 'fission_gas_released he_prod'
released_gas_types = 'Kr Xe;
He'
released_fractions = '0.153 0.847;
1'
quadrature = true
contact_pressure = contact_pressure
refab_gas_types = He
refab_fractions = 1
refab_time = 95032000
refab_type = 0
[]
[]
[BCs]
[no_x_all]
type = DirichletBC
variable = disp_x
boundary = 12
value = 0.0
[]
[Pressure]
[coolantPressure]
boundary = '2'
function = pressure_ramp
[]
[]
[PlenumPressure]
[plenumPressure]
boundary = 9
initial_pressure = 3.44738e6
startup_time = 0
R = 8.3143
output_initial_moles = initial_moles
temperature = plenum_temp
volume = plenum_volume
material_input = 'fission_gas_released he_prod'
output = plenum_pressure
refab_time = 95032000
refab_pressure = 8.2e6
refab_temperature = 295.0
refab_volume = 1.04e-05
cladding_failure_status = burst
equilibrium_pressure = equilibrium_pressure
additional_volumes = additional_volume
temperature_of_additional_volumes = addition_temperature
[]
[]
[]
[UserObjects]
[layered_average_hoop_strain]
type = LayeredAverage
block = clad
num_layers = 10
direction = y
variable = strain_zz
[]
[cladding_strain_yy]
type = LayeredAverage
block = clad
num_layers = 11
direction = y
variable = strain_yy
execute_on = 'initial timestep_end'
[]
[fuel_strain_yy]
type = LayeredAverage
block = fuel
num_layers = 10
direction = y
variable = strain_yy
execute_on = 'initial timestep_end'
[]
# [fuel_pin_geometry]
# type = Layered1DFuelPinGeometry
# mesh_generator = layered1D_mesh
# []
[terminator]
type = Terminator
expression = 'burst > 0'
[]
# We could have two element UOs to obtain interface stress
[1DContactStressOOP_fuel]
type = Layered1DContactInterfaceStress
direction = y
stress_name = stress
num_layers = 10
# If we do not provide the numbers below, it will look at the mesh, in all blocks to set the layer number. Then, it will
# be wrong because the cladding has more height and won't be able to identify layers in the fuel.
direction_min = 0.01306
direction_max = 0.24761028
block = fuel
execute_on = 'LINEAR NONLINEAR'
[]
[1DContactStressOOP_cladding]
type = Layered1DContactInterfaceStress
direction = y
stress_name = stress
num_layers = 10
# If we do not provide the numbers below, it will look at the mesh, in all blocks to set the layer number. Then, it will
# be wrong because the cladding has more height and won't be able to identify layers in the fuel.
direction_min = 0.01306
direction_max = 0.24761028
block = clad
execute_on = 'LINEAR NONLINEAR'
[]
[1DFriction_secondary]
type = Layered1DFrictionalForce
force_postaux = true
contact_pressure = contact_pressure
direction = y
boundary = pellet_outer_radial_surface
num_layers = 10
interface_oop_stress_provider_fuel = 1DContactStressOOP_fuel
interface_oop_stress_provider_cladding = 1DContactStressOOP_cladding
is_secondary_side = true
tangential_pressure = tangential_contact_pressure_aux
friction_coefficient = 0.2
thickness = 0.02606424
penalty_factor = 1.0e13
# If we do not provide the numbers below, it will look at the mesh, in all blocks to set the layer number. Then, it will
# be wrong because the cladding has more height and won't be able to identify layers in the fuel.
direction_min = 0.01306
direction_max = 0.24761028
scalar_var_name_base_fuel = scalar_strain_yy_fuel
scalar_num_variable_fuel = 10
scalar_var_name_base_cladding = scalar_strain_yy_clad
scalar_num_variable_cladding = 10
execute_on = 'LINEAR NONLINEAR'
[]
[1DFriction_primary]
type = Layered1DFrictionalForce
force_postaux = true
contact_pressure = contact_pressure
direction = y
boundary = clad_inside_right
num_layers = 10
# If we do not provide the numbers below, it will look at the mesh, in all blocks to set the layer number. Then, it will
# be wrong because the cladding has more height and won't be able to identify layers in the fuel.
direction_min = 0.0165094
direction_max = 0.24761028
interface_oop_stress_provider_fuel = 1DContactStressOOP_fuel
interface_oop_stress_provider_cladding = 1DContactStressOOP_cladding
is_secondary_side = false
secondary_side_frictional_user_object = 1DFriction_secondary
friction_coefficient = 0.2
thickness = 0.02606424
penalty_factor = 1.0e13
scalar_var_name_base_fuel = scalar_strain_yy_fuel
scalar_num_variable_fuel = 10
scalar_var_name_base_cladding = scalar_strain_yy_clad
scalar_num_variable_cladding = 10
execute_on = 'LINEAR NONLINEAR'
[]
[]
[PlenumTemperature]
[plenum_temp]
boundary = 5
inner_surfaces = '5'
outer_surfaces = '10'
temperature = temperature
[]
[]
[CoolantChannel]
[convective_clad_surface] # apply convective boundary to clad outer surface
boundary = 2
variable = temperature
inlet_temperature = 580
inlet_pressure = 15.5e6 # Pa
inlet_massflux = 3800 # kg/m^2-sec
rod_diameter = 0.00914 # m
rod_pitch = 1.26e-2 # m
compute_enthalpy = false
linear_heat_rate = power_history
axial_power_profile = axial_peaking_factors
output_properties = 'coolant_channel_htype coolant_channel_hmode'
[]
[]
[Materials]
# [uo2_pulverization]
# type = UO2Pulverization
# block = fuel
# layered_average_contact_pressure = contact_pressure
# temperature = temperature
# burnup_function = burnup
# output_properties = pulverized
# outputs = all
# []
[fuel_dispersal]
type = UO2Dispersal
block = fuel
axial_relocation_object = axial_relocation
layered_average_burnup = layered_average_burnup
layered_average_hoop_strain = layered_average_hoop_strain
dispersal_model = ONE_MM_TWO_PERCENT_STRAIN
[]
# Define material behavior models and input material property data
[fuel_thermal] # temperature and burnup dependent thermal properties of UO2 (BISON kernel)
type = UO2Thermal
block = fuel
thermal_conductivity_model = NFIR
temperature = temperature
burnup_function = burnup
axial_relocation_object = axial_relocation
gap_thermal_conductivity = layered_average_gap_conductivity
[]
[fuel_elasticity_tensor]
type = UO2IsotropicDamageElasticityTensor
block = fuel
fragmentation_model = BARANI
temperature = temperature
rod_ave_lin_pow = power_history
axial_relocation_object = axial_relocation
[]
[fuel_elastic_stress]
type = ComputeMultipleInelasticStress
tangent_operator = elastic
inelastic_models = 'fuel_creep'
block = fuel
[]
[fuel_creep]
type = UO2CreepUpdate
block = fuel
temperature = temperature
fission_rate = fission_rate
initial_grain_radius = 10.0e-6
oxygen_to_metal_ratio = 2.0
[]
# [fuel_relocation]
# type = UO2RelocationEigenstrain
# block = fuel
# burnup_function = burnup
# fuel_pin_geometry = fuel_pin_geometry
# rod_ave_lin_pow = power_history
# axial_power_profile = axial_peaking_factors
# burnup_relocation_stop = 0.024
# relocation_activation1 = 5000
# relocation_model = ESCORE_modified
# eigenstrain_name = fuel_relocation_eigenstrain
# []
[fuel_thermal_expansion]
type = ComputeThermalExpansionEigenstrain
block = fuel
thermal_expansion_coeff = 10.0e-6
temperature = temperature
stress_free_temperature = 295.0
eigenstrain_name = fuel_thermal_eigenstrain
[]
[fuel_volumetric_swelling]
type = UO2VolumetricSwellingEigenstrain
gas_swelling_model_type = SIFGRS
block = fuel
temperature = temperature
burnup_function = burnup
initial_fuel_density = 10431.0
eigenstrain_name = fuel_volumetric_eigenstrain
[]
[fission_gas_release]
type = UO2Sifgrs
block = fuel
temperature = temperature
burnup_function = burnup
grain_radius = grain_radius
gbs_model = true
[]
[clad_density]
type = Density
block = clad
density = 6550.
[]
[clad_thermal]
block = clad
type = ZryThermal
temperature = temperature
[]
[clad_thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = clad
temperature = temperature
stress_free_temperature = 295.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = clad
temperature = temperature
[]
[zry_thermal_creep]
type = ZryCreepLOCAUpdate
block = clad
temperature = temperature
model_irradiation_creep = true
model_primary_creep = true
model_thermal_creep = true
max_inelastic_increment = 5e-4
fast_neutron_flux = fast_neutron_flux
fast_neutron_fluence = fast_neutron_fluence
zircaloy_material_type = zirlo
[]
[clad_stress]
type = ComputeMultipleInelasticStress
tangent_operator = elastic
inelastic_models = 'zry_thermal_creep'
block = clad
[]
[clad_irradiation_growth]
type = ZryIrradiationGrowthEigenstrain
block = clad
fast_neutron_fluence = fast_neutron_fluence
zircaloy_material_type = zirlo
eigenstrain_name = clad_irradiation_eigenstrain
[]
[clad_phase]
type = ZrPhase
block = clad
temperature = temperature
numerical_method = 2
[]
[clad_oxidation]
type = ZryOxidation
boundary = 2
temperature = temperature
clad_inner_radius = 4.18e-03
clad_outer_radius = 4.75e-03
normal_operating_temperature_model = epri_kwu_ce
high_temperature_model = leistikow
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = 2
failure_criterion = overstrain
# effective_strain_rate_creep = creep_strain_rate
# failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
hoop_creep_strain = creep_strain_zz
fraction_beta_phase = fract_beta_phase
fraction_oxygen_gain = oxywtfract_total
temperature = temperature
[]
[fuel_density]
type = Density
block = fuel
[]
[]
[VectorPostprocessors]
[cladding_outer]
type = NodalValueSampler
boundary = 5
variable = disp_x
sort_by = y
[]
[]
[AxialRelocation]
[relocation]
rod_ave_lin_pow = power_history
axial_direction = y
fuel_blocks = fuel
clad_blocks = clad
contact_pressure_variable = contact_pressure
out_of_plane_strain_variable = strain_yy_0
penetration_variable = penetration
clad_inner_volume_addition = 0
burnup_variable = burnup
temperature = temperature
axial_relocation_output_options = MASS_FRACTION
mesh_generator = layered1D_mesh
# CHANGE
gap_thickness_threshold = 0.000050
[]
[]
[Postprocessors]
[volume_fuel_dispersed]
type = LayeredElementIntegralMaterialProperty
block = fuel
mat_prop = dispersed
fuel_pin_geometry = fuel_pin_geometry
execute_on = 'initial timestep_end'
[]
[mass_fuel_dispersed]
type = ParsedPostprocessor
pp_names = volume_fuel_dispersed
expression = '10431 * volume_fuel_dispersed'
execute_on = 'initial timestep_end'
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
l_max_its = 50
l_tol = 8e-3
nl_max_its = 15
nl_rel_tol = 1e-4
nl_abs_tol = 1e-8
start_time = -10
n_startup_steps = 1
end_time = 95032000
dtmax = 1e6
dtmin = 1e-6
[TimeStepper]
type = IterationAdaptiveDT
timestep_limiting_postprocessor = material_timestep
dt = 10
optimal_iterations = 20
iteration_window = 4
linear_iteration_ratio = 100
growth_factor = 2
cutback_factor = .5
timestep_limiting_function = forced_times
force_step_every_function_point = true
[]
[Quadrature]
order = FIFTH
side_order = SEVENTH
[]
[]
[Postprocessors]
[ave_temp_interior]
type = SideAverageValue
boundary = 9
variable = temperature
execute_on = 'initial linear'
[]
[clad_inner_vol]
type = InternalVolume
boundary = 7
#outputs = exodus
execute_on = 'initial timestep_end'
[]
[fission_gas_produced] # fission gas produced (moles)
type = ElementIntegralFisGasGeneratedSifgrs
block = fuel
execute_on = 'linear'
[]
[fission_gas_grain]
type = ElementIntegralFisGasGrainSifgrs
block = fuel
outputs = exodus
execute_on = 'linear'
[]
[fission_gas_boundary]
type = ElementIntegralFisGasBoundarySifgrs
block = fuel
outputs = exodus
execute_on = 'linear'
[]
[flux_from_clad] # area integrated heat flux from the cladding
type = SideDiffusiveFluxIntegral
variable = temperature
boundary = 5
diffusivity = thermal_conductivity
[]
[flux_from_fuel] # area integrated heat flux from the fuel
type = SideDiffusiveFluxIntegral
variable = temperature
boundary = 10
diffusivity = thermal_conductivity
[]
[rod_total_power]
type = ElementIntegralPower
variable = temperature
burnup_function = burnup
block = fuel
[]
[max_fuel_temp]
type = NodalExtremeValue
block = fuel
value_type = max
variable = temperature
[]
[max_clad_temp]
type = NodalExtremeValue
block = clad
value_type = max
variable = temperature
[]
[max_clad_hoop_strain]
type = ElementExtremeValue
block = clad
value_type = max
variable = strain_zz
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = clad
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
block = clad
execute_on = 'initial timestep_end'
[]
[he_prod]
type = IFBAHeProduction
b10_load = 9.27165354e-5
b10_enrich = 0.5
burnup = average_burnup
zrb2_thick = 10e-6
fuel_out_rad = 9.32e-3
ifba_len = 0.3
u235_enrich = 0.05
[]
[volume_pulverized]
type = ElementIntegralMaterialProperty
mat_prop = pulverized
block = fuel
[]
[max_fuel_temp_periphery]
type = NodalExtremeValue
value_type = max
variable = temperature
boundary = 10
[]
[additional_volume]
type = FunctionValuePostprocessor
function = 8.5e-6
execute_on = 'initial linear'
[]
[addition_temperature]
type = FunctionValuePostprocessor
function = 300.0
execute_on = 'initial linear'
[]
[equilibrium_pressure]
type = FunctionValuePostprocessor
function = 101325.0
execute_on = 'initial linear'
[]
[]
[PerformanceMetricOutputs]
[]
[StandardLWRFuelRodOutputs]
layered = true
fuel_pin_geometry = fuel_pin_geometry
fuel_pellet_blocks = 'fuel'
[]
[Outputs]
perf_graph = true
exodus = true
color = false
csv = true
[checkpoint]
type = Checkpoint
num_files = 2
[]
[chkfile]
type = CSV
execute_on = FINAL
show = 'volume_pulverized'
[]
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-01/puzry-01.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-01.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 2000. '
y = '1.e+05 1.e+05 7.4e+05' # Linear increase at 0.0064 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 2000. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = EigenSolution
[]
[]
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = MaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = FunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = DirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = DirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1.e+11
poissons_ratio = 0.3
block = 1
[]
[creep_update]
type = ZryCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 1.e-04
temperature = temperature
temperature_standard_thermal_creep_end = 700.0
temperature_loca_creep_begin = 900.0
[]
[creep]
type = ComputeMultipleInelasticStress
block = 1
tangent_operator = elastic
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.0
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = Density
block = 1
[]
[phase]
type = ZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
active = 'smp'
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0.
n_startup_steps = 1
end_time = 2000.
dtmax = 1.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-01_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/LOCA_Hardy_cladding_test/analysis/2pt8MPa/25C_sec/25C_sec_Hardy_Tube_Test_2pt8MPa.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
volumetric_locking_correction = false
displacements = 'disp_x disp_y'
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
group_variables = 'disp_x disp_y'
[]
[Mesh]
coord_type = RZ
patch_size = 10
patch_update_strategy = iteration
partitioner = centroid
centroid_partitioner_direction = y
[gen]
type = FuelPinMeshGenerator
include_fuel = false
include_clad = true
pellet_outer_radius = 0.0072527
clad_gap_width = 0.0
clad_top_gap_height = 0.0
clad_bot_gap_height = 0.0
clad_thickness = 0.38e-3
pellet_height = 0.5
pellet_quantity = 1
clad_mesh_density = customize
nx_c = 2
ny_c = 50
elem_type = QUAD8
[]
[]
[Variables]
[temperature]
initial_condition = 600.0
[]
[]
[AuxVariables]
[creep_rate_aux]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[total_hoop_strain]
order = CONSTANT
family = MONOMIAL
[]
[burst_stress]
order = CONSTANT
family = MONOMIAL
[]
[burst]
order = CONSTANT
family = MONOMIAL
[]
[]
[Functions]
[pressure_function]
type = PiecewiseLinear
x = '0 40'
y = '1 1'
[]
[temp_function]
type = PiecewiseLinear
y = '600 1600'
[]
[temperature_profile]
type = PiecewiseBilinear
y = '0 40'
x = '0 0.25224 0.50448'
z = '0.995 1.01 0.995 0.995 1.01 0.995'
axis = 1
[]
[inner_temperature]
type = CompositeFunction
functions = 'temp_function temperature_profile'
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[clad]
block = clad
add_variables = true
strain = FINITE
decomposition_method = EigenSolution
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz elastic_strain_xx elastic_strain_yy elastic_strain_zz
creep_strain_xx creep_strain_yy creep_strain_zz hoop_stress'
extra_vector_tags = 'ref'
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
extra_vector_tags = 'ref'
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
extra_vector_tags = 'ref'
[]
[]
[AuxKernels]
[creep_rate_aux]
type = MaterialRealAux
variable = creep_rate_aux
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[creep_rate]
type = MaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[total_hoop_strain]
type = RankTwoAux
rank_two_tensor = total_strain
variable = total_hoop_strain
index_i = 2
index_j = 2
execute_on = timestep_end
block = clad
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = clad_outside_right
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = clad_outside_right
execute_on = timestep_end
[]
[]
[BCs]
[Pressure]
[outer_surface]
boundary = 'clad_outside_bottom clad_outside_right clad_outside_top'
factor = 0.0
function = pressure_function
[]
[inner_surface]
boundary = 'clad_inside_right clad_inside_bottom clad_inside_top'
function = pressure_function
[]
[]
[u_bottom_fix]
type = DirichletBC
variable = disp_y
boundary = 1001
value = 0.0
[]
[x_fix]
type = DirichletBC
variable = disp_x
boundary = centerline
value = 0.0
[]
[temp_bc]
type = FunctionDirichletBC
function = inner_temperature
variable = temperature
boundary = 'clad_inside_bottom clad_inside_right clad_inside_top'
[]
[]
[Materials]
[clad_thermal]
type = ZryThermal
block = clad
zry_thermal_properties_model = MATPRO
temperature = temperature
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = clad
matpro_youngs_modulus = true
matpro_poissons_ratio = true
temperature = temperature
[]
[clad_stress]
type = ComputeMultipleInelasticStress
inelastic_models = 'clad_zrycreep'
block = clad
tangent_operator = nonlinear
[]
[clad_zrycreep]
type = ZryCreepLOCAUpdate
block = clad
temperature = temperature
model_irradiation_creep = false
model_primary_creep = true
model_thermal_creep = true
temperature_loca_creep_begin = 840 # values from the report
temperature_standard_thermal_creep_end = 975
[]
[thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = clad
temperature = temperature
stress_free_temperature = 600.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[clad_density]
type = Density
block = clad
density = 6550.0
[]
[phase]
type = ZrPhase
block = clad
temperature = temperature
numerical_method = 2
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = clad_outside_right
failure_criterion = combined_overstress_and_overstrain
hoop_stress = hoop_stress
hoop_creep_strain = creep_strain_zz
effective_strain_rate_creep = creep_rate_aux
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.0e-5
nl_abs_tol = 1.0e-8
start_time = 0
n_startup_steps = 1
end_time = 40
dtmax = 1
dtmin = 0.0000001
[TimeStepper]
type = IterationAdaptiveDT
timestep_limiting_postprocessor = material_timestep
dt = 1.0
[]
[]
[Postprocessors]
[ave_clad_temp]
type = SideAverageValue
boundary = clad_outside_right
variable = temperature
[]
[gas_volume]
type = InternalVolume
boundary = all_clad_interior
execute_on = 'initial linear'
[]
[max_clad_temp]
type = NodalExtremeValue
block = clad
value_type = max
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = clad
[]
[max_hoop_stress]
type = ElementExtremeValue
block = clad
value_type = max
variable = hoop_stress
[]
[vonmises_stress_clad]
type = ElementAverageValue
block = clad
variable = vonmises_stress
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = total_hoop_strain
[]
[max_disp_x]
type = NodalExtremeValue
block = clad
value_type = max
variable = disp_x
[]
[min_burst_stress]
type = ElementExtremeValue
block = clad
value_type = min
variable = burst_stress
[]
[burst]
type = ElementExtremeValue
block = clad
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = clad
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
[]
[PerformanceMetricOutputs]
[]
[Outputs]
color = false
perf_graph = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[csv]
type = CSV
[]
[chkfile]
type = CSV
show = 'max_disp_x max_hoop_stress vonmises_stress_clad'
execute_on = 'FINAL'
[]
[]
[UserObjects]
[terminator1]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '5'
include_fuel = false
[]
[]
(assessment/LWR/validation/LOCA_Studsvik/analysis/rod_196/Studsvik_196_part2.i)
[GlobalParams]
density = 10431.0
initial_porosity = 0.05
order = SECOND
family = LAGRANGE
energy_per_fission = 3.2e-11 # J/fission
volumetric_locking_correction = false
displacements = 'disp_x disp_y'
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
restart_file_base = 'Studsvik_196_part1_checkpoint_cp/LATEST'
[]
[Mesh]
coord_type = RZ
[smeared_mesh]
type = FuelPinMeshGenerator
clad_top_gap_height = 0.0248576
pellet_height = 0.2606424
pellet_quantity = 1
clad_bot_gap_height = 0.0145
pellet_outer_radius = 3.92e-3
clad_gap_width = 80e-6
clad_thickness = 0.57e-3
clad_mesh_density = customize
pellet_mesh_density = customize
nx_c = 5
ny_c = 50
nx_p = 11
ny_p = 60
elem_type = QUAD8
[]
patch_update_strategy = auto
patch_size = 10 # For contact algorithm
partitioner = centroid
centroid_partitioner_direction = y
[]
[Variables]
[temperature]
[]
[]
[AuxVariables]
# Define auxilary variables
[fast_neutron_flux]
block = clad
[]
[fast_neutron_fluence]
block = clad
[]
[grain_radius]
block = pellet
[]
[creep_strain_rate]
order = CONSTANT
family = MONOMIAL
[]
[effective_creep_strain]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[hoop_strain]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[scale_thickness] # ZrO2 scale thickness (m)
order = CONSTANT
family = MONOMIAL
[]
[oxywtfract_total] # Current oxigen weight fraction (oxide+metal) (/)
order = CONSTANT
family = MONOMIAL
[]
[oxywtfgain_total] # Gained oxygen weight fraction (oxide+metal) (/)
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[gap_cond]
order = CONSTANT
family = MONOMIAL
[]
[]
[Functions]
[power_history]
type = PiecewiseLinear
data_file = power_history.csv
format = columns
scale_factor = 1
[]
[axial_peaking_factors]
type = ParsedFunction
expression = 1
[]
[pressure_ramp] # reads and interpolates input data defining amplitude curve for fill gas pressure
type = PiecewiseLinear
x = '-200 0 86400 47386400 47472800 47559200 47645600 94945600 95032000'
y = '0.0065371 1 1 1 1 1 1 1 0.0065371'
scale_factor = 15.5e6
[]
[clad_surface_temperature]
type = PiecewiseBilinear
axis = 1
data_file = clad_temperature.csv
[]
[forced_times]
type = PiecewiseLinear
data_file = timestep_limiting.csv
scale_factor = 1
format = columns
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[fuel]
block = pellet
add_variables = true
strain = FINITE
eigenstrain_names = 'fuel_thermal_eigenstrain fuel_relocation_eigenstrain fuel_volumetric_eigenstrain'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz'
decomposition_method = EigenSolution
extra_vector_tags = 'ref'
temperature = temperature
[]
[clad]
block = clad
add_variables = true
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain clad_irradiation_eigenstrain'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz creep_strain_zz strain_zz'
extra_vector_tags = 'ref'
decomposition_method = EigenSolution
temperature = temperature
[]
[]
[Kernels]
[gravity]
type = Gravity
variable = disp_y
value = -9.81
[]
[heat]
type = HeatConduction
variable = temperature
extra_vector_tags = 'ref'
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
extra_vector_tags = 'ref'
[]
[heat_source]
type = NeutronHeatSource
variable = temperature
extra_vector_tags = 'ref'
block = pellet
burnup_function = burnup
[]
[]
[Burnup]
[burnup]
block = pellet
rod_ave_lin_pow = power_history # using the power function defined above
axial_power_profile = axial_peaking_factors # using the axial power profile function defined above
num_radial = 80
num_axial = 11
fuel_pin_geometry = fuel_pin_geometry
fuel_volume_ratio = 1.0 # for use with dished pellets (ratio of actual volume to cylinder volume)
order = CONSTANT
family = MONOMIAL
RPF = RPF
isotopes = 'U235 U238 Pu239 Pu240 Pu241 Pu242'
isotope_fractions = '0.05 0.95 0 0 0 0'
[]
[]
[AuxKernels]
# Define auxilliary kernels for each of the aux variables
[fast_neutron_flux]
type = FastNeutronFluxAux
variable = fast_neutron_flux
block = clad
rod_ave_lin_pow = power_history
axial_power_profile = axial_peaking_factors
factor = 3e13
execute_on = timestep_begin
[]
[fast_neutron_fluence]
type = FastNeutronFluenceAux
variable = fast_neutron_fluence
block = clad
fast_neutron_flux = fast_neutron_flux
execute_on = timestep_begin
[]
[grain_radius]
type = GrainRadiusAux
block = pellet
variable = grain_radius
temperature = temperature
execute_on = linear
[]
[creep_strain_rate]
type = MaterialRealAux
property = creep_rate
variable = creep_strain_rate
block = clad
[]
[effective_creep_strain]
type = MaterialRealAux
property = effective_creep_strain
variable = effective_creep_strain
block = clad
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
block = clad
variable = fract_beta_phase
property = fract_beta_phase
[]
[scl_thickness]
type = MaterialRealAux
boundary = 2
variable = scale_thickness
property = oxide_scale_thickness
[]
[ofract_total]
type = MaterialRealAux
boundary = 2
variable = oxywtfract_total
property = current_oxygen_weight_frac_total
[]
[ofgain_total]
type = MaterialRealAux
boundary = 2
variable = oxywtfgain_total
property = oxygen_weight_frac_gained_total
[]
[sigmaburst]
type = MaterialRealAux
boundary = 2
variable = burst_stress
property = burst_stress
[]
[hasburst]
type = MaterialRealAux
boundary = 2
variable = burst
property = failed
execute_on = timestep_end
[]
[conductance]
type = MaterialRealAux
property = gap_conductance
variable = gap_cond
boundary = 10
execute_on = 'linear'
[]
[]
[Contact]
[pellet_clad_mechanical]
primary = 5
secondary = 10
formulation = kinematic
model = frictionless
penalty = 1e7
[]
[]
[ThermalContact]
[thermal_contact]
type = GasGapHeatTransfer
variable = temperature
primary = 5
secondary = 10
initial_moles = initial_moles
gas_released = 'fission_gas_released he_prod'
released_gas_types = 'Kr Xe;
He'
released_fractions = '0.153 0.847;
1'
quadrature = true
contact_pressure = contact_pressure
refab_gas_types = He
refab_fractions = 1
refab_time = 95032000
refab_type = 0
[]
[]
[BCs]
[no_x_all]
type = DirichletBC
variable = disp_x
boundary = 12
value = 0.0
[]
[no_y_clad_bottom]
type = DirichletBC
variable = disp_y
boundary = '1'
value = 0.0
[]
[no_y_fuel_bottom]
type = DirichletBC
variable = disp_y
boundary = '1020'
value = 0.0
[]
[Pressure]
[coolantPressure]
boundary = '1 2 3'
function = pressure_ramp
[]
[]
[PlenumPressure]
[plenumPressure]
boundary = 9
initial_pressure = 3.44738e6
startup_time = 0
R = 8.3143
output_initial_moles = initial_moles
temperature = plenum_temp
volume = plenum_volume
material_input = 'fission_gas_released he_prod'
output = plenum_pressure
refab_time = 95032000
refab_pressure = 8.2e6
refab_temperature = 295.0
refab_volume = 1.04e-05
cladding_failure_status = burst
equilibrium_pressure = equilibrium_pressure
additional_volumes = additional_volume
temperature_of_additional_volumes = addition_temperature
[]
[]
[clad_temp]
type = FunctionDirichletBC
function = clad_surface_temperature
variable = temperature
boundary = 2
[]
[]
[UserObjects]
[fuel_pin_geometry]
type = FuelPinGeometry
[]
# [terminator]
# type = Terminator
# expression = 'burst > 0'
# []
[]
[PlenumTemperature]
[plenum_temp]
boundary = 5
inner_surfaces = '5'
outer_surfaces = '10'
temperature = temperature
[]
[]
[CoolantChannel]
[convective_clad_surface] # apply convective boundary to clad outer surface
boundary = 2
variable = temperature
inlet_temperature = 580
inlet_pressure = 15.5e6 # Pa
inlet_massflux = 3800 # kg/m^2-sec
rod_diameter = 0.00914 # m
rod_pitch = 1.26e-2 # m
compute_enthalpy = false
linear_heat_rate = power_history
axial_power_profile = axial_peaking_factors
output_properties = 'coolant_channel_htype coolant_channel_hmode'
[]
[]
[Materials]
[uo2_pulverization]
type = UO2Pulverization
block = pellet
layered_average_contact_pressure = contact_pressure
temperature = temperature
burnup_function = burnup
output_properties = pulverized
outputs = all
[]
# Define material behavior models and input material property data
[fuel_thermal] # temperature and burnup dependent thermal properties of UO2 (BISON kernel)
type = UO2Thermal
block = pellet
thermal_conductivity_model = NFIR
temperature = temperature
burnup_function = burnup
[]
[fuel_elasticity_tensor]
type = UO2IsotropicDamageElasticityTensor
block = pellet
fragmentation_model = BARANI
rod_ave_lin_pow = power_history
temperature = temperature
[]
[fuel_elastic_stress]
type = ComputeMultipleInelasticStress
tangent_operator = elastic
inelastic_models = 'fuel_creep'
block = pellet
[]
[fuel_creep]
type = UO2CreepUpdate
block = pellet
temperature = temperature
fission_rate = fission_rate
initial_grain_radius = 10.0e-6
oxygen_to_metal_ratio = 2.0
[]
[fuel_relocation]
type = UO2RelocationEigenstrain
block = pellet
burnup_function = burnup
fuel_pin_geometry = fuel_pin_geometry
rod_ave_lin_pow = power_history
axial_power_profile = axial_peaking_factors
burnup_relocation_stop = 0.024
relocation_activation1 = 5000
relocation_model = ESCORE_modified
eigenstrain_name = fuel_relocation_eigenstrain
[]
[fuel_thermal_expansion]
type = ComputeThermalExpansionEigenstrain
block = pellet
thermal_expansion_coeff = 10.0e-6
temperature = temperature
stress_free_temperature = 295.0
eigenstrain_name = fuel_thermal_eigenstrain
[]
[fuel_volumetric_swelling]
type = UO2VolumetricSwellingEigenstrain
gas_swelling_model_type = SIFGRS
block = pellet
temperature = temperature
burnup_function = burnup
initial_fuel_density = 10431.0
eigenstrain_name = fuel_volumetric_eigenstrain
[]
[fission_gas_release]
type = UO2Sifgrs
block = pellet
temperature = temperature
burnup_function = burnup
grain_radius = grain_radius
gbs_model = true
[]
[clad_density]
type = Density
block = clad
density = 6550.
[]
[clad_thermal]
block = clad
type = ZryThermal
temperature = temperature
[]
[clad_thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = clad
temperature = temperature
stress_free_temperature = 295.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = clad
temperature = temperature
[]
[zry_thermal_creep]
type = ZryCreepLOCAUpdate
block = clad
temperature = temperature
model_irradiation_creep = true
model_primary_creep = true
model_thermal_creep = true
max_inelastic_increment = 5e-4
fast_neutron_flux = fast_neutron_flux
fast_neutron_fluence = fast_neutron_fluence
zircaloy_material_type = zirlo
[]
[clad_stress]
type = ComputeMultipleInelasticStress
tangent_operator = elastic
inelastic_models = 'zry_thermal_creep'
block = clad
[]
[clad_irradiation_growth]
type = ZryIrradiationGrowthEigenstrain
block = clad
fast_neutron_fluence = fast_neutron_fluence
zircaloy_material_type = zirlo
eigenstrain_name = clad_irradiation_eigenstrain
[]
[clad_phase]
type = ZrPhase
block = clad
temperature = temperature
numerical_method = 2
[]
[clad_oxidation]
type = ZryOxidation
boundary = 2
temperature = temperature
clad_inner_radius = 4.18e-03
clad_outer_radius = 4.75e-03
normal_operating_temperature_model = epri_kwu_ce
high_temperature_model = leistikow
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = 2
failure_criterion = overstrain
# effective_strain_rate_creep = creep_strain_rate
# failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = stress_zz
hoop_creep_strain = creep_strain_zz
fraction_beta_phase = fract_beta_phase
fraction_oxygen_gain = oxywtfract_total
temperature = temperature
[]
[fuel_density]
type = Density
block = pellet
[]
[]
[Dampers]
[limitT]
type = BoundingValueElementDamper
min_value = 290.0
max_value = 3000.0
variable = temperature
[]
[limitX]
type = MaxIncrement
max_increment = 1e-5
variable = disp_x
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
l_max_its = 50
l_tol = 8e-3
nl_max_its = 15
nl_rel_tol = 1e-4
nl_abs_tol = 1e-8
# n_startup_steps = 1
end_time = 95033429.6
dtmax = 20
dtmin = 1e-6
[TimeStepper]
type = IterationAdaptiveDT
timestep_limiting_postprocessor = material_timestep
dt = 10
optimal_iterations = 20
iteration_window = 4
linear_iteration_ratio = 100
growth_factor = 2
cutback_factor = .5
timestep_limiting_function = forced_times
force_step_every_function_point = true
[]
[Quadrature]
order = FIFTH
side_order = SEVENTH
[]
[]
[Postprocessors]
[ave_temp_interior]
type = SideAverageValue
boundary = 9
variable = temperature
execute_on = 'initial linear'
[]
[clad_inner_vol]
type = InternalVolume
boundary = 7
#outputs = exodus
execute_on = 'initial timestep_end'
[]
[fission_gas_produced] # fission gas produced (moles)
type = ElementIntegralFisGasGeneratedSifgrs
block = pellet
execute_on = 'linear'
[]
[fission_gas_grain]
type = ElementIntegralFisGasGrainSifgrs
block = pellet
outputs = exodus
execute_on = 'linear'
[]
[fission_gas_boundary]
type = ElementIntegralFisGasBoundarySifgrs
block = pellet
outputs = exodus
execute_on = 'linear'
[]
[flux_from_clad] # area integrated heat flux from the cladding
type = SideDiffusiveFluxIntegral
variable = temperature
boundary = 5
diffusivity = thermal_conductivity
[]
[flux_from_fuel] # area integrated heat flux from the fuel
type = SideDiffusiveFluxIntegral
variable = temperature
boundary = 10
diffusivity = thermal_conductivity
[]
[rod_total_power]
type = ElementIntegralPower
variable = temperature
burnup_function = burnup
block = pellet
[]
[rod_input_power]
type = FunctionValuePostprocessor
function = power_history
scale_factor = 0.1186 # rod height
[]
[max_fuel_temp]
type = NodalExtremeValue
block = pellet
value_type = max
variable = temperature
[]
[max_clad_temp]
type = NodalExtremeValue
block = clad
value_type = max
variable = temperature
[]
[max_clad_hoop_strain]
type = ElementExtremeValue
block = clad
value_type = max
variable = strain_zz
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = clad
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
block = clad
execute_on = 'initial timestep_end'
[]
[he_prod]
type = IFBAHeProduction
b10_load = 9.27165354e-5
b10_enrich = 0.5
burnup = average_burnup
zrb2_thick = 10e-6
fuel_out_rad = 9.32e-3
ifba_len = 0.3
u235_enrich = 0.05
[]
[volume_pulverized]
type = ElementIntegralMaterialProperty
mat_prop = pulverized
block = pellet
[]
[max_fuel_temp_periphery]
type = NodalExtremeValue
value_type = max
variable = temperature
boundary = 10
[]
[additional_volume]
type = FunctionValuePostprocessor
function = 8.5e-6
execute_on = 'initial linear'
[]
[addition_temperature]
type = FunctionValuePostprocessor
function = 300.0
execute_on = 'initial linear'
[]
[equilibrium_pressure]
type = FunctionValuePostprocessor
function = 101325.0
execute_on = 'initial linear'
[]
[]
[PerformanceMetricOutputs]
[]
[StandardLWRFuelRodOutputs]
temperature = temperature
fuel_pellet_blocks = 3
[]
[Outputs]
perf_graph = true
exodus = true
color = false
csv = true
[chkfile]
type = CSV
execute_on = FINAL
show = 'volume_pulverized'
[]
[]
(assessment/LWR/validation/LOCA_REBEKA_cladding_burst_tests/analysis/rebeka_3d_10MPa_01Kpers_90deg/rebeka_singlerod_3d_10MPa_90deg.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.0
displacements = 'disp_x disp_y disp_z'
order = SECOND
family = LAGRANGE
[]
[Problem]
[]
[Mesh]
[mesh]
type = FileMeshGenerator
file = 3d_rebeka_singlerod.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[disp_z]
[]
[temperature]
initial_condition = 573.0
[]
[]
[Functions]
[temperature_func]
type = PiecewiseLinear
x = '0. 700. '
y = '573. 1273.' # From 300 to 1000 C at 1 K/s
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 700. '
y = '1.e+07 1.e+07' # 100 bar
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 700. '
y = '1.e+05 1.e+05' # atmospheric pressure
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[clad]
block = cladding
add_variables = false
strain = FINITE
decomposition_method = EigenSolution
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz hoop_stress'
[]
[]
[AuxVariables]
[creep_rate_aux]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[scale_thickness] # ZrO2 scale thickness (m)
order = CONSTANT
family = MONOMIAL
[]
[oxywtfract_total] # Total oxigen weight fraction (oxide+metal) (/)
order = CONSTANT
family = MONOMIAL
[]
[oxywtfgain_total]
order = CONSTANT
family = MONOMIAL
[]
[burst]
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate_aux]
type = MaterialRealAux
variable = creep_rate_aux
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[scl_thickness]
type = MaterialRealAux
variable = scale_thickness
property = oxide_scale_thickness
boundary = 2
[]
[ofract_total]
type = MaterialRealAux
variable = oxywtfract_total
property = current_oxygen_weight_frac_total
boundary = 2
[]
[ofgain_total]
type = MaterialRealAux
boundary = 2
variable = oxywtfgain_total
property = oxygen_weight_frac_gained_total
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = 2
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = 2
execute_on = timestep_end
[]
[]
[BCs]
[inner_temperature]
type = REBEKADirichletBC
variable = temperature
function_tempm = temperature_func
translation = 0.1625
vary_azimuthally = true
azimuthal_variation_pi2 = -30.
minimum_temperature = 573.0
boundary = 4
[]
[no_y_midsection]
type = DirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[no_z_frontside]
type = DirichletBC
variable = disp_z
boundary = 5
value = 0.
[]
[no_x_backside]
type = DirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[Pressure]
[outer_pressure] # apply steam pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[CoolantChannel]
[convective_clad_surface]
boundary = 2
variable = temperature
inlet_temperature = 473.
inlet_pressure = 1.e+05
inlet_massflux = 1.0 # kg/m^2-sec # almost stagnant steam
rod_diameter = 10.75e-03
rod_pitch = 1.26e-02 # default
number_axial_zone = 15
oxide_thickness = scale_thickness
[]
[]
[Materials]
[thermal]
type = ZryThermal
block = cladding
temperature = temperature
[]
[clad_elasticity_tensor]
type = ComputeIsotropicElasticityTensor
block = cladding
youngs_modulus = 1.0e11
poissons_ratio = 0.3
[]
[clad_stress]
type = ComputeMultipleInelasticStress
tangent_operator = elastic
inelastic_models = 'clad_zrycreep'
block = cladding
[]
[clad_zrycreep]
type = ZryCreepLOCAUpdate
block = cladding
temperature = temperature
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
temperature_loca_creep_begin = 501 # see Erbacher et al., 1982
temperature_standard_thermal_creep_end = 500
[]
[thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = cladding
temperature = temperature
stress_free_temperature = 573.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[density]
type = Density
block = cladding
[]
[phase]
type = ZrPhase
block = cladding
temperature = temperature
numerical_method = 2
[]
[oxidation]
type = ZryOxidation
boundary = 2
temperature = temperature
clad_inner_radius = 0.00465
clad_outer_radius = 0.005375
use_coolant_channel = true
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = 2
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate_aux
temperature = temperature
fraction_beta_phase = fract_beta_phase
fraction_oxygen_gain = oxywtfgain_total
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0
n_startup_steps = 1
end_time = 700.
dtmax = 1.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[Postprocessors]
[ave_clad_exterior_temp]
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = cladding
[]
[max_clad_temp]
type = NodalExtremeValue
block = cladding
value_type = max
variable = temperature
[]
[max_oxygen_fract]
type = ElementExtremeValue
block = cladding
value_type = max
variable = oxywtfract_total
[]
[max_betaph_fract]
type = ElementExtremeValue
block = cladding
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
block = cladding
value_type = max
variable = creep_rate_aux
[]
[max_creep_strain_mag]
type = ElementExtremeValue
block = cladding
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
block = cladding
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
block = cladding
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
block = cladding
value_type = min
variable = burst_stress
[]
[burst]
type = ElementExtremeValue
block = cladding
value_type = max
variable = burst
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = cladding
plenum_boundary_name = 4
external_clad_boundary_name = 2
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = rebeka_singlerod_3d_10MPa_90deg_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[]
(test/tests/thermalZry/thermal_test.i)
#--------------------------------------------------------------------------------
#
# This test case is prepared to test thermal material model of zirconium alloy
#
# - Geometry:
# Ri = 0.005 m
# Ro = 0.0055 m
# H = 0.01 m
#
# - Single element
#
# - Clad OD temperature is 573 K
#
# - Inner surface heat flux is 600000 W/m^2
#
# - Result:
#
# |---------------------------+---------+------------|
# | | Bison | Analytical |
# |---------------------------+---------+------------|
# | Clad ID Temperature | 590.573 | 590.54 |
# | (K) | | |
# |---------------------------+---------+------------|
# | Avg. Thermal Conductivity | 16.27 | 16.3 |
# | (W/m-K) | | |
# |---------------------------+---------+------------|
#
#
#--------------------------------------------------------------------------------
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = clad_rz_short_rev3.e
[]
[]
[Variables]
[temp]
order = FIRST
family = LAGRANGE
initial_condition = 573
[]
[]
[Functions]
[heatflux_function]
type = PiecewiseLinear
x = '0 1'
y = '600000 600000'
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temp
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temp
[]
[]
[BCs]
[temp_bc_1]
type = FunctionNeumannBC
variable = temp
boundary = 1
function = heatflux_function
[]
[temp_bc_2]
type = NeumannBC
boundary = 2
value = 0.0
variable = temp
[]
[temp_bc_3]
type = DirichletBC
boundary = 3
value = 573
variable = temp
[]
[temp_bc_4]
type = NeumannBC
boundary = 4
value = 0.0
variable = temp
[]
[]
[Materials]
[clad_density]
type = Density
block = 1
density = 6500
[]
[thermal_clad]
type = ZryThermal
block = 1
temperature = temp
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-ksp_gmres_restart'
petsc_options_value = '101'
line_search = 'none'
l_max_its = 100
nl_max_its = 100
nl_rel_tol = 1e-8
nl_abs_tol = 1e-6
l_tol = 1e-5
start_time = 0.0
end_time = 1
dt = 0.02
[]
[Outputs]
csv = true
[out]
type = Exodus
[]
[]
(examples/accident_tolerant_fuel/u3si2_zircaloy/u3si2_zircaloy.i)
[GlobalParams]
# Set initial fuel density, other global parameters
density = 11590.0
order = SECOND
family = LAGRANGE
energy_per_fission = 3.2e-11 # J/fission
volumetric_locking_correction = false
displacements = 'disp_x disp_y'
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
[]
[Mesh]
coord_type = RZ
# Import mesh file
patch_size = 10 # For contact algorithm
patch_update_strategy = auto
partitioner = centroid
centroid_partitioner_direction = y
[mesh]
type = FileMeshGenerator
file = u3si2_zircaloy_smeared.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temp]
initial_condition = 293.0
[]
[]
[UserObjects]
[pin_geometry]
type = FuelPinGeometry
clad_inner_wall = 5
clad_outer_wall = 2
clad_top = 3
clad_bottom = 1
pellet_exteriors = 8
[]
[]
[AuxVariables]
# Define auxilary variables
[fast_neutron_flux]
block = clad
[]
[fast_neutron_fluence]
block = clad
[]
[gap_cond]
order = CONSTANT
family = MONOMIAL
[]
[hoop_stress]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[oxide_thickness]
order = CONSTANT
family = MONOMIAL
[]
[total_hoop_strain]
order = CONSTANT
family = MONOMIAL
[]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[densification]
order = CONSTANT
family = MONOMIAL
[]
[solid_swell]
order = CONSTANT
family = MONOMIAL
[]
[gaseous_swell]
order = CONSTANT
family = MONOMIAL
[]
[]
[Functions]
[power_history]
type = PiecewiseLinear
x = '0 1e4 1e8'
y = '0 2.5e4 2.5e4'
scale_factor = 1
[]
[axial_peaking_factors]
type = ParsedFunction
expression = 1
[]
[pressure_ramp]
type = PiecewiseLinear
x = '-200 0 1e8'
y = '6.537e-3 1 1'
scale_factor = 15.5e6
[]
[mass_flux_func]
type = PiecewiseLinear
x = '-200 0 1e8'
y = '3800 3800 3800'
[]
[q]
type = CompositeFunction
functions = 'power_history axial_peaking_factors'
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[pellets]
block = pellet_type_1
strain = FINITE
eigenstrain_names = 'fuel_thermal_strain fuel_volumetric_strain'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz'
extra_vector_tags = 'ref'
[]
[clad]
block = clad
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain clad_irradiation_strain'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz'
extra_vector_tags = 'ref'
[]
[]
[Kernels]
[gravity]
type = Gravity
variable = disp_y
value = -9.81
extra_vector_tags = 'ref'
[]
[heat]
type = HeatConduction
variable = temp
extra_vector_tags = 'ref'
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temp
extra_vector_tags = 'ref'
[]
[heat_source]
type = NeutronHeatSource
variable = temp
block = pellet_type_1
burnup_function = burnup
extra_vector_tags = 'ref'
[]
[]
[Burnup]
[burnup]
block = pellet_type_1
rod_ave_lin_pow = power_history
axial_power_profile = axial_peaking_factors
num_radial = 81
num_axial = 11
fuel_pin_geometry = pin_geometry
fuel_volume_ratio = 1.0
RPF = RPF
fuel_type = U3Si2
[]
[]
[AuxKernels]
[fast_neutron_flux]
type = FastNeutronFluxAux
variable = fast_neutron_flux
block = clad
rod_ave_lin_pow = power_history
axial_power_profile = axial_peaking_factors
factor = 3e13
execute_on = timestep_begin
[]
[fast_neutron_fluence]
type = FastNeutronFluenceAux
variable = fast_neutron_fluence
block = clad
fast_neutron_flux = fast_neutron_flux
execute_on = timestep_begin
[]
[hoop_stress]
type = RankTwoScalarAux
rank_two_tensor = stress
variable = hoop_stress
scalar_type = HoopStress
execute_on = timestep_end
[]
[total_hoop_strain]
type = RankTwoScalarAux
rank_two_tensor = total_strain
variable = total_hoop_strain
scalar_type = HoopStress
execute_on = timestep_end
[]
[conductance]
type = MaterialRealAux
property = gap_conductance
variable = gap_cond
boundary = 10
[]
[coolant_htc]
type = MaterialRealAux
property = coolant_channel_htc
variable = coolant_htc
boundary = 2
[]
[oxide]
type = MaterialRealAux
variable = oxide_thickness
property = oxide_scale_thickness
boundary = 2
[]
[creep_rate]
type = MaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
block = clad
[]
[densfication]
type = MaterialRealAux
property = densification
variable = densification
block = pellet_type_1
[]
[solid_swell]
type = MaterialRealAux
property = solid_swelling
variable = solid_swell
block = pellet_type_1
[]
[gaseous_swell]
type = MaterialRealAux
property = gaseous_swelling
variable = gaseous_swell
block = pellet_type_1
[]
[]
[Contact]
[pellet_clad_mechanical]
primary = 5
secondary = 10
normal_smoothing_distance = 0.1
penalty = 1e7
[]
[]
[ThermalContact]
[thermal_contact]
type = GasGapHeatTransfer
variable = temp
primary = 5
secondary = 10
initial_moles = initial_moles
gas_released = fis_gas_released
contact_pressure = contact_pressure
quadrature = true
[]
[]
[BCs]
[no_x_all] # pin pellets and clad along axis of symmetry (y)
type = DirichletBC
variable = disp_x
boundary = 12
value = 0.0
[]
[no_y_clad_bottom] # pin clad bottom in the axial direction (y)
type = DirichletBC
variable = disp_y
boundary = '1'
value = 0.0
[]
[no_y_fuel_bottom] # pin fuel bottom in the axial direction (y)
type = DirichletBC
variable = disp_y
boundary = '1020'
value = 0.0
[]
[Pressure]
[coolantPressure]
boundary = '1 2 3'
function = pressure_ramp
[]
[]
[PlenumPressure]
[plenumPressure]
boundary = 9
initial_pressure = 2.0e6
startup_time = 0
R = 8.3143
output_initial_moles = initial_moles
temperature = ave_temp_interior
volume = gas_volume
material_input = fis_gas_released
output = plenum_pressure
[]
[]
[]
[CoolantChannel]
[convective_clad_surface]
boundary = '1 2 3'
variable = temp
inlet_temperature = 580 # K
inlet_pressure = pressure_ramp # Pa
inlet_massflux = mass_flux_func # kg/m^2-sec
rod_diameter = 9.4996e-3 # m
rod_pitch = 1.26e-2 # m
linear_heat_rate = power_history
axial_power_profile = axial_peaking_factors
[]
[]
[Materials]
[fuel_thermal]
type = SilicideFuelThermal
block = pellet_type_1
thermal_conductivity_model = WHITE
silicon_mole_fraction = 0.4
temperature = temp
[]
[fuel_elasticity_tensor]
type = U3Si2ElasticityTensor
block = pellet_type_1
[]
[fuel_stress]
type = ComputeMultipleInelasticStress
block = pellet_type_1
tangent_operator = elastic
inelastic_models = 'fuel_creep'
[]
[fuel_creep]
type = U3Si2CreepUpdate
block = pellet_type_1
temperature = temp
[]
[fuel_thermal_expansion]
type = U3Si2ThermalExpansionEigenstrain
block = pellet_type_1
temperature = temp
stress_free_temperature = 295.0
eigenstrain_name = fuel_thermal_strain
[]
[fuel_volumetric_swelling]
type = U3Si2VolumetricSwellingEigenstrain
block = pellet_type_1
gaseous_swelling_type = U3SI2FG
temperature = temp
burnup_function = burnup
eigenstrain_name = fuel_volumetric_strain
[]
[clad_thermal]
type = ZryThermal
temperature = temp
block = clad
[]
[clad_elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 7.5e10
poissons_ratio = 0.3
block = clad
[]
[clad_stress]
type = ComputeMultipleInelasticStress
tangent_operator = elastic
inelastic_models = 'clad_zrycreep clad_plasticity'
relative_tolerance = 1e-5
block = clad
[]
[clad_zrycreep]
type = ZryCreepLimbackHoppeUpdate
block = clad
temperature = temp
fast_neutron_flux = fast_neutron_flux
fast_neutron_fluence = fast_neutron_fluence
model_irradiation_creep = true
model_primary_creep = true
model_thermal_creep = true
relative_tolerance = 1e-5
max_inelastic_increment = 1e-4
zircaloy_material_type = stress_relief_annealed
[]
[thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = clad
temperature = temp
stress_free_temperature = 295.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[irradiation_swelling]
type = ZryIrradiationGrowthEigenstrain
block = clad
fast_neutron_fluence = fast_neutron_fluence
zircaloy_material_type = stress_relief_annealed
eigenstrain_name = clad_irradiation_strain
[]
[clad_plasticity]
type = ZryPlasticityUpdate
block = clad
temperature = temp
fast_neutron_flux = fast_neutron_flux
fast_neutron_fluence = fast_neutron_fluence
relative_tolerance = 1e-5
cold_work_factor = 0.5
plasticity_model_type = MATPRO
zircaloy_alloy_type = 4
[]
[fission_gas_behavior]
type = U3Si2Sifgrs
block = pellet_type_1
temperature = temp
burnup_function = burnup
saturation_coverage = 0.5
[]
[clad_density]
type = Density
block = clad
density = 6511.0
[]
[fuel_density]
type = Density
block = pellet_type_1
[]
[ZryOxidation]
type = ZryOxidation
boundary = 2
clad_inner_radius = 4.1783e-3
clad_outer_radius = 4.7498e-3
normal_operating_temperature_model = epri_kwu_ce
temperature = temp
fast_neutron_flux = fast_neutron_flux
use_coolant_channel = true
oxygen_weight_fraction_initial = 0.0012
[]
[]
[Dampers]
[limitT]
type = MaxIncrement
max_increment = 100.0
variable = temp
[]
[limitX]
type = MaxIncrement
max_increment = 1e-5
variable = disp_x
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package -ksp_gmres_restart'
petsc_options_value = 'lu superlu_dist 51'
line_search = 'none'
l_max_its = 100
l_tol = 8e-3
nl_max_its = 25
nl_rel_tol = 1e-5
nl_abs_tol = 1e-10
start_time = -200
n_startup_steps = 1
end_time = 1e8
dtmax = 1e6
dtmin = 1e-3
[TimeStepper]
type = IterationAdaptiveDT
dt = 2.0e2
force_step_every_function_point = true
timestep_limiting_function = power_history
max_function_change = 3e20
optimal_iterations = 10
iteration_window = 2
linear_iteration_ratio = 100
timestep_limiting_postprocessor = material_timestep
[]
[Quadrature]
order = FIFTH
side_order = SEVENTH
[]
[]
[Postprocessors]
[avg_fuel_surface]
type = SideAverageValue
boundary = 10
variable = temp
[]
[ave_temp_interior]
type = SideAverageValue
boundary = 9
variable = temp
execute_on = 'initial linear'
[]
[clad_inner_vol]
type = InternalVolume
boundary = 7
[]
[pellet_volume]
type = InternalVolume
boundary = 8
[]
[avg_clad_temp]
type = SideAverageValue
boundary = 7
variable = temp
[]
[fis_gas_produced]
type = ElementIntegralFisGasGeneratedSifgrs
block = pellet_type_1
[]
[fis_gas_released]
type = ElementIntegralFisGasReleasedSifgrs
block = pellet_type_1
[]
[fis_gas_grain]
type = ElementIntegralFisGasGrainSifgrs
block = pellet_type_1
[]
[fis_gas_boundary]
type = ElementIntegralFisGasBoundarySifgrs
block = pellet_type_1
[]
[gas_volume]
type = InternalVolume
boundary = 9
execute_on = 'initial linear'
[]
[flux_from_clad]
type = SideDiffusiveFluxIntegral
variable = temp
boundary = 5
diffusivity = thermal_conductivity
[]
[flux_from_fuel]
type = SideDiffusiveFluxIntegral
variable = temp
boundary = 10
diffusivity = thermal_conductivity
[]
[_dt]
type = TimestepSize
[]
[num_lin_it]
type = NumLinearIterations
[]
[num_nonlin_it]
type = NumNonlinearIterations
[]
[tot_lin_it]
type = CumulativeValuePostprocessor
postprocessor = num_lin_it
[]
[tot_nonlin_it]
type = CumulativeValuePostprocessor
postprocessor = num_nonlin_it
[]
[alive_time]
type = PerfGraphData
section_name = Root
data_type = TOTAL
[]
[rod_total_power]
type = ElementIntegralPower
variable = temp
burnup_function = burnup
block = pellet_type_1
[]
[rod_input_power]
type = FunctionValuePostprocessor
function = power_history
scale_factor = 0.1186
[]
[average_burnup]
type = ElementAverageValue
block = pellet_type_1
variable = burnup
[]
[oxide_thickness]
type = ElementExtremeValue
block = clad
variable = oxide_thickness
[]
[fis_gas_percent]
type = FGRPercent
fission_gas_released = fis_gas_released
fission_gas_generated = fis_gas_produced
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = clad
[]
[]
[Outputs]
perf_graph = true
time_step_interval = 1
exodus = true
color = false
csv = true
print_linear_residuals = true
[console]
type = Console
max_rows = 25
[]
[]
(assessment/LWR/validation/RIA_NSRR_FK/analysis/FK3/FK03.i)
# This file was created using BIF with the following inputs:
# FK03/FK03.var - md5sum: 63fb064f9380e246b80d3fb7762c0b71
# pulse.tpl - md5sum: 37e5a6b8a0c63ad020906dada3472585
[GlobalParams]
density = 10020.6066633
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
energy_per_fission = 3.2e-11
a_lower = 0.01822
a_upper = 0.12422
temperature = temp
volumetric_locking_correction = false
[]
[Mesh]
coord_type = RZ
[smeared_pellet_mesh]
type = FuelPinMeshGenerator
clad_mesh_density = customize
pellet_mesh_density = customize
elem_type = QUAD8
ny_p = 100
nx_c = 4
ny_c = 100
nx_p = 12
ny_cu = 3
ny_cl = 3
bx_p = 0.75
clad_bot_gap_height = 0.00152
bottom_clad_height = 0.0167
top_clad_height = 0.0167
clad_thickness = 0.00086
pellet_outer_radius = 0.00527
clad_top_gap_height = 0.05265
pellet_height = 0.106
clad_gap_width = 1e-05
pellet_quantity = 1
[]
patch_size = 5
patch_update_strategy = auto
partitioner = centroid
centroid_partitioner_direction = y
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
converge_on = 'disp_x disp_y temp'
[]
[Variables]
[temp]
block = '1 3'
initial_condition = 293
[]
[]
[AuxVariables]
[BuTC]
[]
[gap]
order = CONSTANT
family = MONOMIAL
[]
[fast_neutron_flux]
block = 1
[]
[fast_neutron_fluence]
block = 1
[]
[buavg]
order = CONSTANT
family = MONOMIAL
[]
[fission_rate]
initial_condition = 0
[]
[grain_radius]
block = 3
initial_condition = 5.96e-6
[]
[integral_burnup]
order = CONSTANT
family = MONOMIAL
[]
[pellet_id]
order = CONSTANT
family = MONOMIAL
block = 3
[]
[porosity]
order = CONSTANT
family = MONOMIAL
initial_condition = 0.085711070864
[]
[SED]
order = CONSTANT
family = MONOMIAL
[]
[]
[Functions]
[linear_heat_rate_profile]
type = PiecewiseLinear
data_file = pulse.csv
format = columns
[]
[flux]
type = ConstantFunction
value = 0.0
[]
[axial_peaking_factors]
type = ConstantFunction
value = 1
[]
[coolant_pressure_ramp]
type = ConstantFunction
value = 101325
[]
[linear_heat_generation_rate]
type = CompositeFunction
functions = 'linear_heat_rate_profile axial_peaking_factors'
[]
[axial_flux]
type = CompositeFunction
functions = 'flux axial_peaking_factors'
[]
[burnup_thermal_conductivity]
type = ConstantFunction
value = 1 # should be burnup / 950
[]
[radial_power_profile]
type = PiecewiseLinear
data_file = RadialPowerProfile.csv
format = columns
axis = X
[]
[radial_burnup_profile]
type = PiecewiseLinear
data_file = RadialBurnupProfile.csv
format = columns
axis = X
[]
[initial_burnup]
type = CompositeFunction
functions = 'burnup_thermal_conductivity radial_burnup_profile'
[]
[]
[Burnup]
[burnup]
block = 3
rod_ave_lin_pow = linear_heat_rate_profile
axial_power_profile = axial_peaking_factors
rpf_input = radial_power_profile
num_radial = 80
num_axial = 49
fuel_inner_radius = 0.0
fuel_outer_radius = 0.00527
fuel_volume_ratio = 1.0
isotopes = 'U235 U238 Pu239 Pu240 Pu241 Pu242'
isotope_fractions = '0.039 0.961 0.0 0.0 0.0 0.0'
[]
[]
[Physics/SolidMechanics/QuasiStatic]
add_variables = true
[fuel]
block = 3
strain = FINITE
incremental = true
eigenstrain_names = 'fuel_thermal_eigenstrain
fuel_volumetric_swelling_eigenstrain'
extra_vector_tags = 'ref'
generate_output = 'vonmises_stress hydrostatic_stress elastic_strain_xx
elastic_strain_yy elastic_strain_zz stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz'
decomposition_method = EigenSolution
[]
[clad]
block = 1
strain = FINITE
incremental = true
eigenstrain_names = 'clad_thermal_eigenstrain'
extra_vector_tags = 'ref'
generate_output = 'vonmises_stress elastic_strain_xx
elastic_strain_yy elastic_strain_zz stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz creep_strain_xx creep_strain_yy creep_strain_zz'
decomposition_method = EigenSolution
[]
[]
[Kernels]
[gravity]
type = Gravity
variable = disp_y
value = -9.81
extra_vector_tags = 'ref'
block = '1 3'
[]
[heat]
type = HeatConduction
variable = temp
extra_vector_tags = 'ref'
block = '1 3'
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temp
extra_vector_tags = 'ref'
block = '1 3'
[]
[heat_source]
type = NeutronHeatSource
fission_rate = fission_rate
variable = temp
block = 3
extra_vector_tags = 'ref'
[]
[]
[AuxKernels]
[BuTC]
type = FunctionAux
block = 3
variable = BuTC
function = initial_burnup
[]
[pelletid]
type = PelletIdAux
block = 3
variable = pellet_id
number_pellets = 1
execute_on = initial
[]
[gap]
type = SpatialUserObjectAux
block = 3
variable = gap
execute_on = timestep_end
user_object = avg_gap
[]
[buavg]
type = SpatialUserObjectAux
block = 3
variable = buavg
execute_on = timestep_end
user_object = integral_burnup
[]
[fast_neutron_flux]
type = FastNeutronFluxAux
variable = fast_neutron_flux
function = axial_flux
block = 1
execute_on = timestep_begin
[]
[fast_neutron_fluence]
type = FastNeutronFluenceAux
variable = fast_neutron_fluence
block = 1
fast_neutron_flux = fast_neutron_flux
execute_on = timestep_begin
[]
[fuel_porosity]
type = PorosityAuxUO2
block = 3
variable = porosity
execute_on = timestep_begin
[]
[grain_radius]
type = GrainRadiusAux
block = 3
variable = grain_radius
temperature = temp
execute_on = timestep_begin
[]
[SED]
type = MaterialRealAux
variable = SED
property = strain_energy_density
execute_on = timestep_end
block = 1
[]
[]
[Contact]
[mechanical]
model = coulomb
formulation = mortar
primary = 5
secondary = 10
friction_coefficient = 0.4
c_normal = 1e+12
c_tangential = 1e+24
tangential_lm_scaling = 1.0e-16
normal_lm_scaling = 1.0e-10
[]
[]
[ThermalContactMortar]
[thermal_contact]
secondary_variable = temp
primary_boundary = '5'
secondary_boundary = '10'
layer_thickness = layer_thickness_action
roughness_coef = 3.2
roughness_primary = 1.5e-6
roughness_secondary = 1.75e-6
jump_distance_model = LANNING
plenum_pressure = plenum_pressure
contact_pressure = mechanical_normal_lm
initial_moles = initial_moles
gas_released = fission_gas_released
thermal_lm_scaling = 1.0e-2
[]
[]
[BCs]
[no_x_all]
type = DirichletBC
variable = disp_x
boundary = 12
value = 0.0
[]
[no_y_fuel_bottom]
type = DirichletBC
variable = disp_y
boundary = 20
value = 0.0
[]
[no_y_clad_bottom]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[]
[coolant_temp]
type = DirichletBC
boundary = '1 2 3'
variable = temp
value = 293
[]
[Pressure]
[coolantPressure]
boundary = '1 2 3'
factor = 1
function = coolant_pressure_ramp
[]
[]
[PlenumPressure]
[plenumPressure]
boundary = '10 5'
initial_pressure = 0.3e6
startup_time = 0
R = 8.314462
output_initial_moles = initial_moles
temperature = plenum_temperature
volume = plenum_volume
material_input = fission_gas_released
output = plenum_pressure
initial_temperature = 293
[]
[]
[]
[Materials]
[fuel_swelling]
type = UO2VolumetricSwellingEigenstrain
block = 3
burnup = burnup
initial_fuel_density = 10020.6066633
total_densification = 0.006
gas_swelling_model_type = SIFGRS
eigenstrain_name = 'fuel_volumetric_swelling_eigenstrain'
[]
[fuel_thermal]
type = UO2Thermal
thermal_conductivity_model = NFIR
block = 3
temperature = temp
burnup = BuTC
initial_porosity = 0.085711070864
[]
[fuel_elasticity_tensor]
type = UO2ElasticityTensor
block = 3
[]
[fuel_thermal_expansion]
type = UO2ThermalExpansionMartinEigenstrain
block = 3
stress_free_temperature = 293
eigenstrain_name = 'fuel_thermal_eigenstrain'
[]
[fuel_elastic_stress]
type = ComputeFiniteStrainElasticStress
block = '3'
[]
[clad_thermal]
type = ZryThermal
block = 1
temperature = temp
[]
[clad_inelastic_stress]
type = ComputeMultipleInelasticStress
block = 1
tangent_operator = elastic
inelastic_models ='plasticity'
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = 1
fast_neutron_fluence = fast_neutron_fluence
initial_fast_fluence = 8.40e25
cold_work_factor = 0.01
matpro_youngs_modulus = true
matpro_poissons_ratio = true
[]
## TODO: Creep is not active, but is transfered from the SM version.
## Adding creep causes the Peak Hoop strain to best match the FALCON
## results given by R. Montgomery and D. Sunderland. Only retaining
## plasticity matches the results from Wenfeng Liu, John Alvis, Robert Montgomery, and Ken Yueh
[clad_creep_stress]
type = ZryCreepLimbackHoppeUpdate
block = 1
fast_neutron_flux = fast_neutron_flux
fast_neutron_fluence = fast_neutron_fluence
initial_fast_fluence = 8.40e25
[]
[clad_thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 293.0
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[plasticity]
type = ZryPlasticityUpdate
block = 1
initial_fast_fluence = 8.40e25
fast_neutron_flux = fast_neutron_flux
fast_neutron_fluence = fast_neutron_fluence
cold_work_factor = .01
plasticity_model_type = MATPRO
output_properties = yield_stress
outputs = all
zircaloy_alloy_type = 4
[]
[fission_gas_release]
type = UO2Sifgrs
block = 3
temperature = temp
fission_rate = fission_rate
grain_radius = grain_radius
gbs_model = true
burnup = BuTC
transient_option = MICROCRACKING
[]
[clad_density]
type = Density
block = 1
density = 6551
[]
[fuel_density]
type = Density
block = 3
[]
[strain_energy_density]
type = StrainEnergyDensity
incremental = true
block = '1 3'
[]
[]
[UserObjects]
[avg_gap]
type = LayeredAverage
block = 3
variable = penetration
direction = y
num_layers = 48
[]
[pbz]
type = PelletBrittleZone
block = 3
pellet_id = pellet_id
temperature = temp
pellet_radius = 0.00527
number_pellets = 1
execute_on = timestep_begin
[]
[integral_burnup]
type = LayeredAverage
block = 3
variable = burnup
direction = y
num_layers = 1
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_converged_reason -ksp_converged_reason -snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package -mat_mffd_err -pc_factor_shift_type '
'-pc_factor_shift_amount'
petsc_options_value = 'lu superlu_dist 1e-5 NONZERO 1e-12'
line_search = 'none'
l_max_its = 40
l_tol = 8e-3
nl_max_its = 40
nl_rel_tol = 1e-3
nl_abs_tol = 1e-10
dtmin = 0.00001
dtmax = 1.0
start_time = 0
end_time = 100
[TimeStepper]
type = IterationAdaptiveDT
dt = 0.0001
optimal_iterations = 200
linear_iteration_ratio = 100
timestep_limiting_function = linear_heat_rate_profile
max_function_change = 550000
force_step_every_function_point = true
[]
[]
[Dampers]
[limitT]
type = MaxIncrement
max_increment = 200.0
variable = temp
[]
[limitX]
type = MaxIncrement
max_increment = 1e-4
variable = disp_x
[]
[]
[Postprocessors]
[max_hoop_strain]
type = ElementExtremeValue
variable = strain_zz
block = 1
[]
[max_SED]
type = ElementExtremeValue
variable = SED
block = 1
[]
[average_grain_radius]
type = ElementAverageValue
block = 3
outputs = 'exodus'
variable = grain_radius
[]
[clad_inner_vol]
type = InternalVolume
boundary = 7
outputs = 'exodus'
execute_on = 'timestep_begin initial'
[]
[flux_from_clad]
type = SideDiffusiveFluxIntegral
variable = temp
boundary = 5
diffusivity = thermal_conductivity
outputs = 'exodus'
[]
[flux_from_fuel]
type = SideDiffusiveFluxIntegral
variable = temp
boundary = 10
diffusivity = thermal_conductivity
outputs = 'exodus'
[]
[rod_total_power]
type = ElementIntegralPower
variable = temp
fission_rate = fission_rate
block = 3
[]
[rod_input_power]
type = FunctionValuePostprocessor
function = linear_heat_rate_profile
scale_factor = 0.106
[]
[average_fission_rate]
type = ElementAverageValue
variable = fission_rate
block = '3'
[]
[RAE]
type = RadialAverageEnthalpy
vector_postprocessor = rad_temp
radial_direction = x
axial_direction = y
axial_position = 0.0503
temperature_name = temp
[]
[peak_RAE]
type = TimeExtremeValue
postprocessor = RAE
[]
[]
[VectorPostprocessors]
[rad_temp]
type = NodalValueSampler
block = 3
sort_by = y
variable = temp
execute_on = timestep_end
outputs = dummy
[]
[]
[StandardLWRFuelRodOutputs]
fuel_pellet_blocks = 3
cladding_blocks = 1
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[chkfile]
type = CSV
show = 'average_centerline_fuel_temperature average_fission_rate fission_gas_released_percentage peak_RAE rod_total_power'
execute_on = 'FINAL'
[]
[console]
type = Console
max_rows = 25
output_linear = true
[]
[dummy]
type = CSV
enable = false
[]
[]
(test/tests/zry_oxidation_cladding/oxidation_cladding_zry.i)
# This test demonstrates the usage of the model for cladding oxidation from
# normal operating to high temperature (accident) conditions, through the
# epri_kwu_ce, Leistikow, and Prater relations.
#
# The mesh is a 1x1x1 cube, with temperature boundary conditions ramping from
# 600K to 1950K, no displacement boundary conditions.
#
# The final oxidation thickness expected is 4.059e-4 m and the final total gained
# oxygen concentration is 7.228e-1 kg/m^3, from hand calculations performed alongside
# the BISON simulation.
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
[mesh]
type = FileMeshGenerator
file = cube_111.e
[]
[]
[Functions]
[Temp_func]
type = PiecewiseLinear
x = '0. 100000000. 100000010. 100000100. 100000110. 100000200. 100000210. 100000300.'
y = '600. 600. 1100. 1100. 1850. 1850. 1950. 1950. '
[]
[FNFlux_func]
type = PiecewiseLinear
x = '0. 100000300.'
y = '1.e+17 1.e+17 '
[]
[]
[Variables]
[temp]
order = FIRST
family = LAGRANGE
initial_condition = 600.
[]
[disp_x]
order = FIRST
family = LAGRANGE
[]
[disp_y]
order = FIRST
family = LAGRANGE
[]
[disp_z]
order = FIRST
family = LAGRANGE
[]
[]
[AuxVariables]
[fast_neutron_flux]
order = FIRST
family = LAGRANGE
initial_condition = 1.0e+17
[]
[scale_thickness] # ZrO2 scale thickness (m)
order = CONSTANT
family = MONOMIAL
[]
[oxyconc2_scale] # Oxygen concentration in ZrO2 scale (kg/m**2)
order = CONSTANT
family = MONOMIAL
[]
[oxyconc2_metal] # Oxygen concentration in metal (kg/m**2)
order = CONSTANT
family = MONOMIAL
[]
[oxyconc2_total] # Total oxygen concentration (oxide + metal) (kg/m**2)
order = CONSTANT
family = MONOMIAL
[]
[oxywtfract_metal] # Oxygen weight fraction in metal (/)
order = CONSTANT
family = MONOMIAL
[]
[oxywtfract_total] # Total oxygen weight fraction (oxide+metal) (/)
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[all]
strain = finite
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temp
[]
[]
[AuxKernels]
[fnflux]
type = FastNeutronFluxAux
variable = fast_neutron_flux
block = 1
function = FNFlux_func
execute_on = timestep_begin
[]
[scl_thickness]
type = MaterialRealAux
variable = scale_thickness
property = oxide_scale_thickness
boundary = 1
[]
[oconc_scale]
type = MaterialRealAux
variable = oxyconc2_scale
property = gained_oxygen_concentration_scale
boundary = 1
[]
[oconc_metal]
type = MaterialRealAux
variable = oxyconc2_metal
property = gained_oxygen_concentration_metal_wall
boundary = 1
[]
[oconc_total]
type = MaterialRealAux
variable = oxyconc2_total
property = gained_oxygen_concentration_total
boundary = 1
[]
[ofract_metal]
type = MaterialRealAux
variable = oxywtfract_metal
property = current_oxygen_weight_frac_metal_wall
boundary = 1
[]
[ofract_total]
type = MaterialRealAux
variable = oxywtfract_total
property = current_oxygen_weight_frac_total
boundary = 1
[]
[]
[BCs]
[bottom_T]
type = FunctionDirichletBC
variable = temp
function = Temp_func
boundary = 1
[]
[x_disp]
type = DirichletBC
variable = disp_x
value = 0
boundary = 1
[]
[y_disp]
type = DirichletBC
variable = disp_y
value = 0
boundary = 2
[]
[z_disp]
type = DirichletBC
variable = disp_z
value = 0
boundary = 3
[]
[]
[Materials]
[elasticity_tensor]
type = ZryElasticityTensor
block = 1
[]
[stress]
type = ComputeFiniteStrainElasticStress
block = 1
[]
[thermal]
type = ZryThermal
block = 1
temperature = temp
[]
[oxidation_zry]
type = ZryOxidation
boundary = 1
clad_inner_radius = 0.004650
clad_outer_radius = 0.005375
normal_operating_temperature_model = epri_kwu_ce
high_temperature_model = leistikow
temperature = temp
fast_neutron_flux = fast_neutron_flux
show_debug_output = true
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = 'lu superlu_dist'
l_tol = 1.e-08
nl_abs_tol = 1.e-08
nl_rel_tol = 1.e-08
start_time = 0.
num_steps = 5000 #5000
end_time = 100000300 #*100
[TimeStepper]
type = IterationAdaptiveDT
dt = 1.e+06
optimal_iterations = 6
iteration_window = 2
linear_iteration_ratio = 100
time_t = '0. 100000000.'
time_dt = '1.e+06 10. '
growth_factor = 1.
[]
[]
[Postprocessors]
[_dt]
type = TimestepSize
[]
[temp]
type = NodalVariableValue
variable = temp
nodeid = 0
execute_on = 'initial timestep_end'
[]
[scale_thickness]
type = ElementalVariableValue
elementid = 0
variable = scale_thickness
[]
[oxyconc2_scale]
type = ElementalVariableValue
elementid = 0
variable = oxyconc2_scale
[]
[oxyconc2_metal]
type = ElementalVariableValue
elementid = 0
variable = oxyconc2_metal
[]
[oxyconc2_total]
type = ElementalVariableValue
elementid = 0
variable = oxyconc2_total
[]
[oxywtfract_metal]
type = ElementalVariableValue
elementid = 0
variable = oxywtfract_metal
[]
[oxywtfract_total]
type = ElementalVariableValue
elementid = 0
variable = oxywtfract_total
[]
[]
[Outputs]
file_base = oxidation_cladding_zry_out
[exodus]
type = Exodus
[]
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-11/puzry-11.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-11.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 1200. '
y = '1.e+05 1.e+05 1.534e+06' # Linear increase at 0.0717 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 1200. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = EigenSolution
[]
[]
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = MaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = FunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = DirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = DirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1.e+11
poissons_ratio = 0.3
block = 1
[]
[creep_update]
type = ZryCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 1.e-04
temperature = temperature
temperature_standard_thermal_creep_end = 700
temperature_loca_creep_begin = 900.
[]
[creep]
type = ComputeMultipleInelasticStress
block = 1
tangent_operator = elastic
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = Density
block = 1
[]
[phase]
type = ZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
active = 'smp'
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0.
n_startup_steps = 1
end_time = 1200.
dtmax = 1.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-11_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/LOCA_Hardy_cladding_test/analysis/5pt5MPa/100C_sec/100C_sec_Hardy_Tube_Test_5pt5MPa.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
volumetric_locking_correction = false
displacements = 'disp_x disp_y'
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
group_variables = 'disp_x disp_y'
[]
[Mesh]
coord_type = RZ
patch_size = 10
patch_update_strategy = iteration
partitioner = centroid
centroid_partitioner_direction = y
[gen]
type = FuelPinMeshGenerator
include_fuel = false
include_clad = true
pellet_outer_radius = 0.0072527
clad_gap_width = 0.0
clad_top_gap_height = 0.0
clad_bot_gap_height = 0.0
clad_thickness = 0.38e-3
pellet_height = 0.5
pellet_quantity = 1
clad_mesh_density = customize
nx_c = 2
ny_c = 50
elem_type = QUAD8
[]
[]
[Variables]
[temperature]
initial_condition = 600.0
[]
[]
[AuxVariables]
[creep_rate_aux]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[total_hoop_strain]
order = CONSTANT
family = MONOMIAL
[]
[burst_stress]
order = CONSTANT
family = MONOMIAL
[]
[burst]
order = CONSTANT
family = MONOMIAL
[]
[]
[Functions]
[pressure_function]
type = PiecewiseLinear
x = '0 40'
y = '1 1'
[]
[temp_function]
type = PiecewiseLinear
y = '600 1600'
[]
[temperature_profile]
type = PiecewiseBilinear
y = '0 40'
x = '0 0.25224 0.50448'
z = '0.995 1.01 0.995 0.995 1.01 0.995'
axis = 1
[]
[inner_temperature]
type = CompositeFunction
functions = 'temp_function temperature_profile'
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[clad]
block = clad
add_variables = true
strain = FINITE
decomposition_method = EigenSolution
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz elastic_strain_xx elastic_strain_yy elastic_strain_zz
creep_strain_xx creep_strain_yy creep_strain_zz hoop_stress'
extra_vector_tags = 'ref'
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
extra_vector_tags = 'ref'
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
extra_vector_tags = 'ref'
[]
[]
[AuxKernels]
[creep_rate_aux]
type = MaterialRealAux
variable = creep_rate_aux
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[creep_rate]
type = MaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[total_hoop_strain]
type = RankTwoAux
rank_two_tensor = total_strain
variable = total_hoop_strain
index_i = 2
index_j = 2
execute_on = timestep_end
block = clad
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = clad_outside_right
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = clad_outside_right
execute_on = timestep_end
[]
[]
[BCs]
[Pressure]
[outer_surface]
boundary = 'clad_outside_bottom clad_outside_right clad_outside_top'
factor = 0.0
function = pressure_function
[]
[inner_surface]
boundary = 'clad_inside_right clad_inside_bottom clad_inside_top'
function = pressure_function
[]
[]
[u_bottom_fix]
type = DirichletBC
variable = disp_y
boundary = 1001
value = 0.0
[]
[x_fix]
type = DirichletBC
variable = disp_x
boundary = centerline
value = 0.0
[]
[temp_bc]
type = FunctionDirichletBC
function = inner_temperature
variable = temperature
boundary = 'clad_inside_bottom clad_inside_right clad_inside_top'
[]
[]
[Materials]
[clad_thermal]
type = ZryThermal
block = clad
zry_thermal_properties_model = MATPRO
temperature = temperature
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = clad
matpro_youngs_modulus = true
matpro_poissons_ratio = true
temperature = temperature
[]
[clad_stress]
type = ComputeMultipleInelasticStress
inelastic_models = 'clad_zrycreep'
block = clad
tangent_operator = nonlinear
[]
[clad_zrycreep]
type = ZryCreepLOCAUpdate
block = clad
temperature = temperature
model_irradiation_creep = false
model_primary_creep = true
model_thermal_creep = true
temperature_loca_creep_begin = 840 # values from the report
temperature_standard_thermal_creep_end = 975
[]
[thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = clad
temperature = temperature
stress_free_temperature = 600.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[clad_density]
type = Density
block = clad
density = 6550.0
[]
[phase]
type = ZrPhase
block = clad
temperature = temperature
numerical_method = 2
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = clad_outside_right
failure_criterion = combined_overstress_and_overstrain
hoop_stress = hoop_stress
hoop_creep_strain = creep_strain_zz
effective_strain_rate_creep = creep_rate_aux
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.0e-5
nl_abs_tol = 1.0e-8
start_time = 0
n_startup_steps = 1
end_time = 40
dtmax = 1
dtmin = 0.0000001
[TimeStepper]
type = IterationAdaptiveDT
timestep_limiting_postprocessor = material_timestep
dt = 1.0
[]
[]
[Postprocessors]
[ave_clad_temp]
type = SideAverageValue
boundary = clad_outside_right
variable = temperature
[]
[gas_volume]
type = InternalVolume
boundary = all_clad_interior
execute_on = 'initial linear'
[]
[max_clad_temp]
type = NodalExtremeValue
block = clad
value_type = max
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = clad
[]
[max_hoop_stress]
type = ElementExtremeValue
block = clad
value_type = max
variable = hoop_stress
[]
[vonmises_stress_clad]
type = ElementAverageValue
block = clad
variable = vonmises_stress
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = total_hoop_strain
[]
[max_disp_x]
type = NodalExtremeValue
block = clad
value_type = max
variable = disp_x
[]
[min_burst_stress]
type = ElementExtremeValue
block = clad
value_type = min
variable = burst_stress
[]
[burst]
type = ElementExtremeValue
block = clad
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = clad
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
[]
[PerformanceMetricOutputs]
[]
[Outputs]
color = false
perf_graph = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[csv]
type = CSV
[]
[chkfile]
type = CSV
show = 'max_disp_x max_hoop_stress vonmises_stress_clad'
execute_on = 'FINAL'
[]
[]
[UserObjects]
[terminator1]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '5'
include_fuel = false
[]
[]
(assessment/LWR/validation/LOCA_REBEKA_cladding_burst_tests/analysis/rebeka_2d_12MPa/rebeka_singlerod_2d_12MPa.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.0
order = SECOND
family = LAGRANGE
displacements = 'disp_x disp_y'
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = rebeka_singlerod.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 573.0
[]
[]
[Functions]
[temperature_func]
type = PiecewiseLinear
x = '0. 700. '
y = '573. 1273.' # From 300 to 1000 C at 1 K/s
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 700. '
y = '1.2e+07 1.2e+07' # 120 bar
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 700. '
y = '1.e+05 1.e+05' # atmospheric pressure
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[clad]
block = cladding
add_variables = false
strain = FINITE
decomposition_method = EigenSolution
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz hoop_stress'
[]
[]
[AuxVariables]
[creep_rate_aux]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[scale_thickness]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfract_total]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfgain_total]
order = CONSTANT
family = MONOMIAL
[]
[burst_stress]
order = CONSTANT
family = MONOMIAL
[]
[burst]
order = CONSTANT
family = MONOMIAL
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate_aux]
type = MaterialRealAux
variable = creep_rate_aux
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[scl_thickness]
type = MaterialRealAux
variable = scale_thickness
property = oxide_scale_thickness
boundary = 2
[]
[ofract_total]
type = MaterialRealAux
variable = oxywtfract_total
property = current_oxygen_weight_frac_total
boundary = 2
[]
[ofgain_total]
type = MaterialRealAux
boundary = 2
variable = oxywtfgain_total
property = oxygen_weight_frac_gained_total
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = 2
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = 2
execute_on = timestep_end
[]
[]
[BCs]
[inner_temperature]
type = REBEKADirichletBC
variable = temperature
function_tempm = temperature_func
minimum_temperature = 573.0
translation = 0.1625
boundary = 4
[]
[no_y_midsection]
type = DirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply steam pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 101 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[CoolantChannel]
[convective_clad_surface]
boundary = 2
variable = temperature
inlet_temperature = 473.
inlet_pressure = 1.e+05
inlet_massflux = 1.0 # kg/m^2-sec # almost stagnant steam
rod_diameter = 10.75e-03
rod_pitch = 1.26e-02 # default
number_axial_zone = 15
oxide_thickness = scale_thickness
[]
[]
[Materials]
[thermal]
type = ZryThermal
block = cladding
temperature = temperature
[]
[clad_elasticity_tensor]
type = ComputeIsotropicElasticityTensor
block = cladding
youngs_modulus = 1.0e11
poissons_ratio = 0.3
[]
[clad_stress]
type = ComputeMultipleInelasticStress
tangent_operator = elastic
inelastic_models = 'clad_zrycreep'
block = cladding
[]
[clad_zrycreep]
type = ZryCreepLOCAUpdate
block = cladding
temperature = temperature
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
temperature_loca_creep_begin = 501 # see Erbacher et al., 1982
temperature_standard_thermal_creep_end = 500
[]
[thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = cladding
temperature = temperature
stress_free_temperature = 573.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[density]
type = Density
block = cladding
[]
[phase]
type = ZrPhase
block = cladding
temperature = temperature
numerical_method = 2
[]
[oxidation]
type = ZryOxidation
boundary = 2
temperature = temperature
clad_inner_radius = 0.00465
clad_outer_radius = 0.005375
normal_operating_temperature_model = epri_kwu_ce
high_temperature_model = leistikow
use_coolant_channel = true
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = 2
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate_aux
temperature = temperature
fraction_beta_phase = fract_beta_phase
fraction_oxygen_gain = oxywtfgain_total
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0
n_startup_steps = 1
end_time = 700.
dtmax = 1.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average temperature of cladding exterior
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = cladding
[]
[max_clad_temp]
type = NodalExtremeValue
block = cladding
value_type = max
variable = temperature
[]
[max_oxygen_fract]
type = ElementExtremeValue
block = cladding
value_type = max
variable = oxywtfract_total
[]
[max_betaph_fract]
type = ElementExtremeValue
block = cladding
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
block = cladding
value_type = max
variable = creep_rate_aux
[]
[max_creep_strain_mag]
type = ElementExtremeValue
block = cladding
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
block = cladding
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
block = cladding
value_type = max
variable = hoop_stress
[]
[vonmises_stress_clad]
type = ElementAverageValue
block = cladding
variable = vonmises_stress
[]
[min_burst_stress]
type = ElementExtremeValue
block = cladding
value_type = min
variable = burst_stress
[]
[burst]
type = ElementExtremeValue
block = cladding
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = cladding
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = cladding
plenum_boundary_name = 4
external_clad_boundary_name = 2
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = rebeka_2d_12MPa_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
(assessment/LWR/validation/RIA_NSRR_FK/analysis/FK6/FK06.i)
# This file was created using BIF with the following inputs:
# FK06/FK06.var - md5sum: 5a60c05af67ba840a89caacf70b852e2
# pulse.tpl - md5sum: 37e5a6b8a0c63ad020906dada3472585
[GlobalParams]
density = 10310.8809782
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
energy_per_fission = 3.2e-11
a_lower = 0.01822
a_upper = 0.12422
temperature = temp
volumetric_locking_correction = false
[]
[Mesh]
coord_type = RZ
[smeared_pellet_mesh]
type = FuelPinMeshGenerator
clad_mesh_density = customize
pellet_mesh_density = customize
elem_type = QUAD8
ny_p = 100
nx_c = 4
ny_c = 100
nx_p = 12
ny_cu = 3
ny_cl = 3
bx_p = 0.75
clad_bot_gap_height = 0.00152
bottom_clad_height = 0.0167
top_clad_height = 0.0167
clad_thickness = 0.00086
pellet_outer_radius = 0.00527
clad_top_gap_height = 0.05265
pellet_height = 0.106
clad_gap_width = 1e-05
pellet_quantity = 1
[]
patch_size = 5
patch_update_strategy = auto
partitioner = centroid
centroid_partitioner_direction = y
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
converge_on = 'disp_x disp_y temp'
[]
[Variables]
[temp]
initial_condition = 293
block = '1 3'
[]
[]
[AuxVariables]
[BuTC]
[]
[gap]
order = CONSTANT
family = MONOMIAL
[]
[fast_neutron_flux]
block = 1
[]
[fast_neutron_fluence]
block = 1
[]
[buavg]
order = CONSTANT
family = MONOMIAL
[]
[fission_rate]
initial_condition = 0
[]
[grain_radius]
block = 3
initial_condition = 5.96e-6
[]
[integral_burnup]
order = CONSTANT
family = MONOMIAL
[]
[pellet_id]
order = CONSTANT
family = MONOMIAL
block = 3
[]
[porosity]
order = CONSTANT
family = MONOMIAL
initial_condition = 0.0592261881186
[]
[SED]
order = CONSTANT
family = MONOMIAL
[]
[]
[Functions]
[linear_heat_rate_profile]
type = PiecewiseLinear
data_file = pulse.csv
format = columns
[]
[flux]
type = ConstantFunction
value = 0.0
[]
[axial_peaking_factors]
type = ConstantFunction
value = 1
[]
[coolant_pressure_ramp]
type = ConstantFunction
value = 101325
[]
[linear_heat_generation_rate]
type = CompositeFunction
functions = 'linear_heat_rate_profile axial_peaking_factors'
[]
[axial_flux]
type = CompositeFunction
functions = 'flux axial_peaking_factors'
[]
[burnup_thermal_conductivity]
type = ConstantFunction
value = 1 # should be burnup / 950
[]
[radial_power_profile]
type = PiecewiseLinear
data_file = RadialPowerProfile.csv
format = columns
axis = X
[]
[radial_burnup_profile]
type = PiecewiseLinear
data_file = RadialBurnupProfile.csv
format = columns
axis = X
[]
[initial_burnup]
type = CompositeFunction
functions = 'burnup_thermal_conductivity radial_burnup_profile'
[]
[]
[Burnup]
[burnup]
block = 3
rod_ave_lin_pow = linear_heat_rate_profile
axial_power_profile = axial_peaking_factors
rpf_input = radial_power_profile
num_radial = 80
num_axial = 49
fuel_inner_radius = 0.0
fuel_outer_radius = 0.00527
fuel_volume_ratio = 1.0
isotopes = 'U235 U238 Pu239 Pu240 Pu241 Pu242'
isotope_fractions = '0.045 0.955 0.0 0.0 0.0 0.0'
[]
[]
[Physics/SolidMechanics/QuasiStatic]
add_variables = true
[fuel]
block = 3
strain = FINITE
incremental = true
eigenstrain_names = 'fuel_thermal_eigenstrain
fuel_volumetric_swelling_eigenstrain'
extra_vector_tags = 'ref'
generate_output = 'vonmises_stress hydrostatic_stress elastic_strain_xx
elastic_strain_yy '
'elastic_strain_zz stress_xx stress_yy stress_zz strain_xx
strain_yy '
'strain_zz'
decomposition_method = EigenSolution
[]
[clad]
block = 1
strain = FINITE
incremental = true
eigenstrain_names = 'clad_thermal_eigenstrain'
extra_vector_tags = 'ref'
generate_output = 'vonmises_stress elastic_strain_xx
elastic_strain_yy elastic_strain_zz '
'stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz '
'creep_strain_xx creep_strain_yy creep_strain_zz'
decomposition_method = EigenSolution
[]
[]
[Kernels]
[gravity]
type = Gravity
variable = disp_y
value = -9.81
block = '1 3'
extra_vector_tags = 'ref'
[]
[heat]
type = HeatConduction
variable = temp
block = '1 3'
extra_vector_tags = 'ref'
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temp
block = '1 3'
extra_vector_tags = 'ref'
[]
[heat_source]
type = NeutronHeatSource
fission_rate = fission_rate
variable = temp
block = 3
extra_vector_tags = 'ref'
[]
[]
[AuxKernels]
[BuTC]
type = FunctionAux
block = 3
variable = BuTC
function = initial_burnup
[]
[pelletid]
type = PelletIdAux
block = 3
variable = pellet_id
number_pellets = 1
execute_on = initial
[]
[gap]
type = SpatialUserObjectAux
block = 3
variable = gap
execute_on = timestep_end
user_object = avg_gap
[]
[buavg]
type = SpatialUserObjectAux
block = 3
variable = buavg
execute_on = timestep_end
user_object = integral_burnup
[]
[fast_neutron_flux]
type = FastNeutronFluxAux
variable = fast_neutron_flux
function = axial_flux
block = 1
execute_on = timestep_begin
[]
[fast_neutron_fluence]
type = FastNeutronFluenceAux
variable = fast_neutron_fluence
block = 1
fast_neutron_flux = fast_neutron_flux
execute_on = timestep_begin
[]
[fuel_porosity]
type = PorosityAuxUO2
block = 3
variable = porosity
execute_on = timestep_begin
[]
[grain_radius]
type = GrainRadiusAux
block = 3
variable = grain_radius
temperature = temp
execute_on = timestep_begin
[]
[SED]
type = MaterialRealAux
variable = SED
property = strain_energy_density
execute_on = timestep_end
block = 1
[]
[]
[Contact]
[mechanical]
model = coulomb
formulation = mortar
primary = 5
secondary = 10
friction_coefficient = 0.4
c_normal = 1e+12
c_tangential = 1e+24
tangential_lm_scaling = 1.0e-16
normal_lm_scaling = 1.0e-10
[]
[]
[ThermalContactMortar]
[thermal_contact]
secondary_variable = temp
primary_boundary = '5'
secondary_boundary = '10'
layer_thickness = layer_thickness_action
roughness_coef = 3.2
roughness_primary = 1.5e-6
roughness_secondary = 1.75e-6
jump_distance_model = LANNING
plenum_pressure = plenum_pressure
initial_moles = initial_moles
initial_gas_types = 'He Ar'
initial_fractions = '0.25 0.75'
gas_released = fission_gas_released
contact_pressure = mechanical_normal_lm
thermal_lm_scaling = 1.0e-2
[]
[]
[BCs]
[no_x_all]
type = DirichletBC
variable = disp_x
boundary = 12
value = 0.0
[]
[no_y_fuel_bottom]
type = DirichletBC
variable = disp_y
boundary = 20
value = 0.0
[]
[no_y_clad_bottom]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[]
[coolant_temp]
type = DirichletBC
boundary = '1 2 3'
variable = temp
value = 293
[]
[Pressure]
[coolantPressure]
boundary = '1 2 3'
factor = 1
function = coolant_pressure_ramp
[]
[]
[PlenumPressure]
[plenumPressure]
boundary = '10 5'
initial_pressure = 0.1e6
startup_time = 0
R = 8.314462
output_initial_moles = initial_moles
temperature = plenum_temperature
volume = plenum_volume
material_input = fission_gas_released
output = plenum_pressure
initial_temperature = 293
[]
[]
[]
[Materials]
[fuel_swelling]
type = UO2VolumetricSwellingEigenstrain
block = 3
burnup = burnup
initial_fuel_density = 10310.8809782
total_densification = 0.006
gas_swelling_model_type = SIFGRS
eigenstrain_name = 'fuel_volumetric_swelling_eigenstrain'
[]
[fuel_thermal]
type = UO2Thermal
thermal_conductivity_model = NFIR
block = 3
temperature = temp
burnup = BuTC
initial_porosity = 0.0592261881186
[]
[fuel_elasticity_tensor]
type = UO2ElasticityTensor
block = 3
[]
[fuel_thermal_expansion]
type = UO2ThermalExpansionMartinEigenstrain
block = 3
stress_free_temperature = 293
eigenstrain_name = 'fuel_thermal_eigenstrain'
[]
[fuel_elastic_stress]
type = ComputeFiniteStrainElasticStress
block = '3'
[]
[clad_thermal]
type = ZryThermal
block = 1
temperature = temp
[]
[clad_inelastic_stress]
type = ComputeMultipleInelasticStress
block = 1
tangent_operator = elastic
inelastic_models = 'plasticity'
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = 1
fast_neutron_fluence = fast_neutron_fluence
initial_fast_fluence = 1.30e26
cold_work_factor = 0.01
matpro_youngs_modulus = true
matpro_poissons_ratio = true
[]
## TODO: Creep is not active, but is transfered from the SM version.
## Adding creep causes the Peak Hoop strain to best match the FALCON
## results given by R. Montgomery and D. Sunderland. Only retaining
## plasticity matches the results from Wenfeng Liu, John Alvis, Robert Montgomery, and Ken Yueh
[clad_creep_stress]
type = ZryCreepLimbackHoppeUpdate
block = 1
fast_neutron_flux = fast_neutron_flux
fast_neutron_fluence = fast_neutron_fluence
initial_fast_fluence = 1.30e26
[]
[clad_thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 293.0
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[plasticity]
type = ZryPlasticityUpdate
block = 1
initial_fast_fluence = 1.30e26
fast_neutron_flux = fast_neutron_flux
fast_neutron_fluence = fast_neutron_fluence
cold_work_factor = .01
plasticity_model_type = MATPRO
output_properties = yield_stress
outputs = all
zircaloy_alloy_type = 4
[]
[fission_gas_release]
type = UO2Sifgrs
block = 3
temperature = temp
fission_rate = fission_rate
grain_radius = grain_radius
gbs_model = true
burnup = BuTC
transient_option = MICROCRACKING
[]
[clad_density]
type = Density
block = 1
density = 6551
[]
[fuel_density]
type = Density
block = 3
[]
[strain_energy_density]
type = StrainEnergyDensity
block = '1 3'
incremental = true
[]
[]
[UserObjects]
[avg_gap]
type = LayeredAverage
block = 3
variable = penetration
direction = y
num_layers = 48
[]
[pbz]
type = PelletBrittleZone
block = 3
pellet_id = pellet_id
temperature = temp
pellet_radius = 0.00527
number_pellets = 1
execute_on = timestep_begin
[]
[integral_burnup]
type = LayeredAverage
block = 3
variable = burnup
direction = y
num_layers = 1
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_converged_reason -ksp_converged_reason -snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package -mat_mffd_err -pc_factor_shift_type '
'-pc_factor_shift_amount'
petsc_options_value = 'lu superlu_dist 1e-5 NONZERO 1e-12'
line_search = 'none'
l_max_its = 40
l_tol = 8e-3
nl_max_its = 40
nl_rel_tol = 1e-3
nl_abs_tol = 1e-10
dtmin = 0.00001
dtmax = 1.0
start_time = 0
end_time = 100
[TimeStepper]
type = IterationAdaptiveDT
dt = 0.0001
optimal_iterations = 200
linear_iteration_ratio = 100
timestep_limiting_function = linear_heat_rate_profile
max_function_change = 500000
force_step_every_function_point = true
[]
[]
[Dampers]
[limitT]
type = MaxIncrement
max_increment = 200.0
variable = temp
[]
[limitX]
type = MaxIncrement
max_increment = 1e-4
variable = disp_x
[]
[]
[Postprocessors]
[max_hoop_strain]
type = ElementExtremeValue
variable = strain_zz
block = 1
[]
[max_SED]
type = ElementExtremeValue
variable = SED
block = 1
[]
[average_grain_radius]
type = ElementAverageValue
block = 3
outputs = 'exodus'
variable = grain_radius
[]
[clad_inner_vol]
type = InternalVolume
boundary = 7
outputs = 'exodus'
execute_on = 'timestep_begin initial'
[]
[flux_from_clad]
type = SideDiffusiveFluxIntegral
variable = temp
boundary = 5
diffusivity = thermal_conductivity
outputs = 'exodus'
[]
[flux_from_fuel]
type = SideDiffusiveFluxIntegral
variable = temp
boundary = 10
diffusivity = thermal_conductivity
outputs = 'exodus'
[]
[rod_total_power]
type = ElementIntegralPower
variable = temp
fission_rate = fission_rate
block = 3
[]
[rod_input_power]
type = FunctionValuePostprocessor
function = linear_heat_rate_profile
scale_factor = 0.106
[]
[average_fission_rate]
type = ElementAverageValue
variable = fission_rate
block = '3'
[]
[RAE]
type = RadialAverageEnthalpy
vector_postprocessor = rad_temp
radial_direction = x
axial_direction = y
axial_position = 0.0503
temperature_name = temp
[]
[peak_RAE]
type = TimeExtremeValue
postprocessor = RAE
[]
[]
[VectorPostprocessors]
[rad_temp]
type = NodalValueSampler
block = 3
sort_by = y
variable = temp
execute_on = timestep_end
outputs = dummy
[]
[]
[StandardLWRFuelRodOutputs]
fuel_pellet_blocks = 3
cladding_blocks = 1
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[chkfile]
type = CSV
show = 'average_centerline_fuel_temperature average_fission_rate fission_gas_released_percentage '
'peak_RAE rod_total_power'
execute_on = 'FINAL'
[]
[console]
type = Console
max_rows = 25
output_linear = true
[]
[dummy]
type = CSV
enable = false
[]
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-09/puzry-09_aniso.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-09.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 1200. '
y = '1.e+05 1.e+05 1.524e+06' # Linear increase at 0.0712 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 1200. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
# Circumferential steady-state creep test and analysis of Zircaloy-4 fuel cladding
# Nuclear Engineering and Design, 53, 2312-2322 (2021)
[F]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.738 0.738 0.57'
[]
[G]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.174 0.174 0.45'
[]
[H]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.588 0.588 0.48'
[]
[L]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[M]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[N]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = TaylorExpansion
use_automatic_differentiation = true
[]
[]
[]
[]
[Kernels]
[heat]
type = ADHeatConduction
variable = temperature
[]
[heat_ie]
type = ADHeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = ADMaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = ADMaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = ADMaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = ADMaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = ADMaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = ADFunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = ADDirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = ADDirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ADZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1.e+11
poissons_ratio = 0.3
block = 1
[]
[hill_constants]
type = ADHillConstants
hill_constants = "0.738 0.174 0.588 1.0 1.0 1.0"
function_names = "F G H L M N"
temperature = temperature
[]
[creep_update]
type = ADZryAnisoCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 2.5e-05
temperature = temperature
temperature_standard_thermal_creep_end = 700
temperature_loca_creep_begin = 900.
fract_beta_phase_name = 'fract_beta_phase'
max_integration_error = 1000000.0
absolute_tolerance = 1e-07
relative_tolerance = 1e-07
[]
[creep]
type = ADComputeMultipleInelasticStress
block = 1
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ADZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = ADDensity
block = 1
[]
[phase]
type = ADZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ADZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = NEWTON
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0.
n_startup_steps = 1
end_time = 2500.
dtmax = 1.
dtmin = 1.0e-9
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-09_aniso_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-07/puzry-07_aniso.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-07.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 1300. '
y = '1.e+05 1.e+05 2.377e+06' # Linear increase at 0.0759 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 1300. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
# Circumferential steady-state creep test and analysis of Zircaloy-4 fuel cladding
# Nuclear Engineering and Design, 53, 2312-2322 (2021)
[F]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.738 0.738 0.57'
[]
[G]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.174 0.174 0.45'
[]
[H]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.588 0.588 0.48'
[]
[L]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[M]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[N]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = TaylorExpansion
use_automatic_differentiation = true
[]
[]
[]
[]
[Kernels]
[heat]
type = ADHeatConduction
variable = temperature
[]
[heat_ie]
type = ADHeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = ADMaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = ADMaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = ADMaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = ADMaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = ADMaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = ADFunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = ADDirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = ADDirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ADZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1.e+11
poissons_ratio = 0.3
block = 1
[]
[hill_constants]
type = ADHillConstants
hill_constants = "0.738 0.174 0.588 1.0 1.0 1.0"
function_names = "F G H L M N"
temperature = temperature
[]
[creep_update]
type = ADZryAnisoCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 2.0e-05
temperature = temperature
temperature_standard_thermal_creep_end = 700
temperature_loca_creep_begin = 900.
fract_beta_phase_name = 'fract_beta_phase'
max_integration_error = 1000000.0
absolute_tolerance = 1e-07
relative_tolerance = 1e-07
[]
[creep]
type = ADComputeMultipleInelasticStress
block = 1
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ADZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = ADDensity
block = 1
[]
[phase]
type = ADZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ADZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = NEWTON
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0.
n_startup_steps = 1
end_time = 2500.
dtmax = 1.
dtmin = 1.0e-9
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-07_aniso_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-17/puzry-17_aniso.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-17.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 1500. '
y = '1.e+05 1.e+05 5.91e+06' # Linear increase at 0.1162 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 1500. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
# Circumferential steady-state creep test and analysis of Zircaloy-4 fuel cladding
# Nuclear Engineering and Design, 53, 2312-2322 (2021)
[F]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.738 0.738 0.57'
[]
[G]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.174 0.174 0.45'
[]
[H]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.588 0.588 0.48'
[]
[L]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[M]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[N]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = TaylorExpansion
use_automatic_differentiation = true
[]
[]
[]
[]
[Kernels]
[heat]
type = ADHeatConduction
variable = temperature
[]
[heat_ie]
type = ADHeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = ADMaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = ADMaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = ADMaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = ADMaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = ADMaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = ADFunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = ADDirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = ADDirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ADZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1.e+11
poissons_ratio = 0.3
block = 1
[]
[hill_constants]
type = ADHillConstants
hill_constants = "0.738 0.174 0.588 1.0 1.0 1.0"
function_names = "F G H L M N"
temperature = temperature
[]
[creep_update]
type = ADZryAnisoCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 1.5e-05
temperature = temperature
temperature_standard_thermal_creep_end = 700
temperature_loca_creep_begin = 900.
fract_beta_phase_name = 'fract_beta_phase'
max_integration_error = 1000000.0
absolute_tolerance = 1e-13
relative_tolerance = 1e-11
[]
[creep]
type = ADComputeMultipleInelasticStress
block = 1
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ADZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = ADDensity
block = 1
[]
[phase]
type = ADZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ADZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = NEWTON
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-07
start_time = 0.
n_startup_steps = 1
end_time = 2500.
dtmax = 1.
dtmin = 1.0e-9
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-17_aniso_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/LOCA_Studsvik/analysis/rod_191/Studsvik_191_part2.i)
[GlobalParams]
density = 10431.0
initial_porosity = 0.05
order = SECOND
family = LAGRANGE
energy_per_fission = 3.2e-11 # J/fission
volumetric_locking_correction = false
displacements = 'disp_x disp_y'
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
restart_file_base = 'Studsvik_191_part1_checkpoint_cp/LATEST'
[]
[Mesh]
coord_type = RZ
[smeared_mesh]
type = FuelPinMeshGenerator
clad_top_gap_height = 0.021861442
pellet_height = 0.265388558
pellet_quantity = 1
clad_bot_gap_height = 0.01275
pellet_outer_radius = 4.1e-3
clad_gap_width = 80e-6
clad_thickness = 0.57e-3
clad_mesh_density = customize
pellet_mesh_density = customize
nx_c = 5
ny_c = 50
nx_p = 11
ny_p = 60
elem_type = QUAD8
[]
patch_update_strategy = auto
patch_size = 10 # For contact algorithm
partitioner = centroid
centroid_partitioner_direction = y
[]
[Variables]
[temperature]
[]
[]
[AuxVariables]
# Define auxilary variables
[fast_neutron_flux]
block = clad
[]
[fast_neutron_fluence]
block = clad
[]
[grain_radius]
block = pellet
[]
[creep_strain_rate]
order = CONSTANT
family = MONOMIAL
[]
[effective_creep_strain]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[hoop_strain]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[scale_thickness] # ZrO2 scale thickness (m)
order = CONSTANT
family = MONOMIAL
[]
[oxywtfract_total] # Current oxigen weight fraction (oxide+metal) (/)
order = CONSTANT
family = MONOMIAL
[]
[oxywtfgain_total] # Gained oxygen weight fraction (oxide+metal) (/)
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[gap_cond]
order = CONSTANT
family = MONOMIAL
[]
[]
[Functions]
[power_history]
type = PiecewiseLinear
data_file = power_history.csv
format = columns
scale_factor = 1
[]
[axial_peaking_factors]
type = ParsedFunction
expression = 1
[]
[pressure_ramp] # reads and interpolates input data defining amplitude curve for fill gas pressure
type = PiecewiseLinear
x = '-200 0 166755600 166842000'
y = '0.006537 1 1 0.006537'
scale_factor = 15.5e6
[]
[clad_surface_temperature]
type = PiecewiseBilinear
axis = 1
data_file = clad_temperature.csv
[]
[forced_times]
type = PiecewiseLinear
data_file = timestep_limiting.csv
scale_factor = 1
format = columns
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[fuel]
block = pellet
add_variables = true
strain = FINITE
eigenstrain_names = 'fuel_thermal_eigenstrain fuel_relocation_eigenstrain fuel_volumetric_eigenstrain'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz'
decomposition_method = EigenSolution
extra_vector_tags = 'ref'
temperature = temperature
[]
[clad]
block = clad
add_variables = true
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain clad_irradiation_eigenstrain'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz creep_strain_zz strain_zz'
extra_vector_tags = 'ref'
decomposition_method = EigenSolution
temperature = temperature
[]
[]
[Kernels]
[gravity]
type = Gravity
variable = disp_y
value = -9.81
[]
[heat]
type = HeatConduction
variable = temperature
extra_vector_tags = 'ref'
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
extra_vector_tags = 'ref'
[]
[heat_source]
type = NeutronHeatSource
variable = temperature
extra_vector_tags = 'ref'
block = pellet
burnup_function = burnup
[]
[]
[Burnup]
[burnup]
block = pellet
rod_ave_lin_pow = power_history # using the power function defined above
axial_power_profile = axial_peaking_factors # using the axial power profile function defined above
num_radial = 80
num_axial = 11
fuel_pin_geometry = fuel_pin_geometry
fuel_volume_ratio = 1.0 # for use with dished pellets (ratio of actual volume to cylinder volume)
order = CONSTANT
family = MONOMIAL
RPF = RPF
isotopes = 'U235 U238 Pu239 Pu240 Pu241 Pu242'
isotope_fractions = '0.05 0.95 0 0 0 0'
[]
[]
[AuxKernels]
# Define auxilliary kernels for each of the aux variables
[fast_neutron_flux]
type = FastNeutronFluxAux
variable = fast_neutron_flux
block = clad
rod_ave_lin_pow = power_history
axial_power_profile = axial_peaking_factors
factor = 3e13
execute_on = timestep_begin
[]
[fast_neutron_fluence]
type = FastNeutronFluenceAux
variable = fast_neutron_fluence
block = clad
fast_neutron_flux = fast_neutron_flux
execute_on = timestep_begin
[]
[grain_radius]
type = GrainRadiusAux
block = pellet
variable = grain_radius
temperature = temperature
execute_on = linear
[]
[creep_strain_rate]
type = MaterialRealAux
property = creep_rate
variable = creep_strain_rate
block = clad
[]
[effective_creep_strain]
type = MaterialRealAux
property = effective_creep_strain
variable = effective_creep_strain
block = clad
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
block = clad
variable = fract_beta_phase
property = fract_beta_phase
[]
[scl_thickness]
type = MaterialRealAux
boundary = 2
variable = scale_thickness
property = oxide_scale_thickness
[]
[ofract_total]
type = MaterialRealAux
boundary = 2
variable = oxywtfract_total
property = current_oxygen_weight_frac_total
[]
[ofgain_total]
type = MaterialRealAux
boundary = 2
variable = oxywtfgain_total
property = oxygen_weight_frac_gained_total
[]
[sigmaburst]
type = MaterialRealAux
boundary = 2
variable = burst_stress
property = burst_stress
[]
[hasburst]
type = MaterialRealAux
boundary = 2
variable = burst
property = failed
execute_on = timestep_end
[]
[conductance]
type = MaterialRealAux
property = gap_conductance
variable = gap_cond
boundary = 10
execute_on = 'linear'
[]
[]
[Contact]
[pellet_clad_mechanical]
primary = 5
secondary = 10
formulation = kinematic
model = frictionless
penalty = 1e7
[]
[]
[ThermalContact]
[thermal_contact]
type = GasGapHeatTransfer
variable = temperature
primary = 5
secondary = 10
initial_moles = initial_moles
gas_released = fission_gas_released
quadrature = true
contact_pressure = contact_pressure
refab_gas_types = He
refab_fractions = 1
refab_time = 166842000
refab_type = 0
[]
[]
[BCs]
[no_x_all]
type = DirichletBC
variable = disp_x
boundary = 12
value = 0.0
[]
[no_y_clad_bottom]
type = DirichletBC
variable = disp_y
boundary = '1'
value = 0.0
[]
[no_y_fuel_bottom]
type = DirichletBC
variable = disp_y
boundary = '1020'
value = 0.0
[]
[Pressure]
[coolantPressure]
boundary = '1 2 3'
function = pressure_ramp
[]
[]
[PlenumPressure]
[plenumPressure]
boundary = 9
initial_pressure = 3.44738e6
startup_time = 0
R = 8.3143
output_initial_moles = initial_moles
temperature = plenum_temp
volume = plenum_volume
material_input = fission_gas_released
output = plenum_pressure
refab_time = 166842000
refab_pressure = 11e6
refab_temperature = 295.0
refab_volume = 1.04e-05
cladding_failure_status = burst
equilibrium_pressure = equilibrium_pressure
additional_volumes = additional_volume
temperature_of_additional_volumes = addition_temperature
[]
[]
[clad_temp]
type = FunctionDirichletBC
function = clad_surface_temperature
variable = temperature
boundary = 2
[]
[]
[UserObjects]
[fuel_pin_geometry]
type = FuelPinGeometry
[]
# [terminator]
# type = Terminator
# expression = 'burst > 0'
# []
[]
[PlenumTemperature]
[plenum_temp]
boundary = 5
inner_surfaces = '5'
outer_surfaces = '10'
temperature = temperature
[]
[]
[CoolantChannel]
[convective_clad_surface] # apply convective boundary to clad outer surface
boundary = 2
variable = temperature
inlet_temperature = 580
inlet_pressure = 15.5e6 # Pa
inlet_massflux = 3800 # kg/m^2-sec
rod_diameter = 0.0095 # m
rod_pitch = 1.26e-2 # m
compute_enthalpy = false
linear_heat_rate = power_history
axial_power_profile = axial_peaking_factors
output_properties = 'coolant_channel_htype coolant_channel_hmode'
[]
[]
[Materials]
[uo2_pulverization]
type = UO2Pulverization
block = pellet
layered_average_contact_pressure = contact_pressure
temperature = temperature
burnup_function = burnup
output_properties = pulverized
outputs = all
[]
# Define material behavior models and input material property data
[fuel_thermal] # temperature and burnup dependent thermal properties of UO2 (BISON kernel)
type = UO2Thermal
block = pellet
thermal_conductivity_model = NFIR
temperature = temperature
burnup_function = burnup
[]
[fuel_elasticity_tensor]
type = UO2IsotropicDamageElasticityTensor
block = pellet
fragmentation_model = BARANI
rod_ave_lin_pow = power_history
temperature = temperature
[]
[fuel_elastic_stress]
type = ComputeMultipleInelasticStress
tangent_operator = elastic
inelastic_models = 'fuel_creep'
block = pellet
[]
[fuel_creep]
type = UO2CreepUpdate
block = pellet
temperature = temperature
fission_rate = fission_rate
initial_grain_radius = 10.0e-6
oxygen_to_metal_ratio = 2.0
[]
[fuel_relocation]
type = UO2RelocationEigenstrain
block = pellet
burnup_function = burnup
rod_ave_lin_pow = power_history
axial_power_profile = axial_peaking_factors
fuel_pin_geometry = fuel_pin_geometry
burnup_relocation_stop = 0.024
relocation_activation1 = 5000
relocation_model = ESCORE_modified
eigenstrain_name = fuel_relocation_eigenstrain
[]
[fuel_thermal_expansion]
type = ComputeThermalExpansionEigenstrain
block = pellet
thermal_expansion_coeff = 10.0e-6
temperature = temperature
stress_free_temperature = 295.0
eigenstrain_name = fuel_thermal_eigenstrain
[]
[fuel_volumetric_swelling]
type = UO2VolumetricSwellingEigenstrain
gas_swelling_model_type = SIFGRS
block = pellet
temperature = temperature
burnup_function = burnup
initial_fuel_density = 10431.0
eigenstrain_name = fuel_volumetric_eigenstrain
[]
[fission_gas_release]
type = UO2Sifgrs
block = pellet
temperature = temperature
burnup_function = burnup
grain_radius = grain_radius
gbs_model = true
[]
[clad_density]
type = Density
block = clad
density = 6550.
[]
[clad_thermal]
block = clad
type = ZryThermal
temperature = temperature
[]
[clad_thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = clad
temperature = temperature
stress_free_temperature = 295.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = clad
temperature = temperature
[]
[zry_thermal_creep]
type = ZryCreepLOCAUpdate
block = clad
temperature = temperature
model_irradiation_creep = true
model_primary_creep = true
model_thermal_creep = true
max_inelastic_increment = 5e-4
fast_neutron_flux = fast_neutron_flux
fast_neutron_fluence = fast_neutron_fluence
zircaloy_material_type = zirlo
[]
[clad_stress]
type = ComputeMultipleInelasticStress
tangent_operator = elastic
inelastic_models = 'zry_thermal_creep'
block = clad
[]
[clad_irradiation_growth]
type = ZryIrradiationGrowthEigenstrain
block = clad
fast_neutron_fluence = fast_neutron_fluence
zircaloy_material_type = zirlo
eigenstrain_name = clad_irradiation_eigenstrain
[]
[clad_phase]
type = ZrPhase
block = clad
temperature = temperature
numerical_method = 2
[]
[clad_oxidation]
type = ZryOxidation
boundary = 2
temperature = temperature
clad_inner_radius = 4.18e-03
clad_outer_radius = 4.75e-03
normal_operating_temperature_model = epri_kwu_ce
high_temperature_model = leistikow
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = 2
failure_criterion = overstrain
# effective_strain_rate_creep = creep_strain_rate
# failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = stress_zz
hoop_creep_strain = creep_strain_zz
fraction_beta_phase = fract_beta_phase
fraction_oxygen_gain = oxywtfract_total
temperature = temperature
[]
[fuel_density]
type = Density
block = pellet
[]
[]
[Dampers]
[limitT]
type = MaxIncrement
max_increment = 100
variable = temperature
[]
[limitX]
type = MaxIncrement
max_increment = 1e-5
variable = disp_x
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
l_max_its = 50
l_tol = 8e-3
nl_max_its = 15
nl_rel_tol = 1e-4
nl_abs_tol = 1e-8
# n_startup_steps = 1
end_time = 166843509.6
dtmax = 20
dtmin = 1e-6
[TimeStepper]
type = IterationAdaptiveDT
timestep_limiting_postprocessor = material_timestep
dt = 10
optimal_iterations = 20
iteration_window = 4
linear_iteration_ratio = 100
growth_factor = 2
cutback_factor = .5
timestep_limiting_function = forced_times
force_step_every_function_point = true
[]
[Quadrature]
order = FIFTH
side_order = SEVENTH
[]
[]
[Postprocessors]
[ave_temp_interior]
type = SideAverageValue
boundary = 9
variable = temperature
execute_on = 'initial linear'
[]
[clad_inner_vol]
type = InternalVolume
boundary = 7
#outputs = exodus
execute_on = 'initial timestep_end'
[]
[fission_gas_produced] # fission gas produced (moles)
type = ElementIntegralFisGasGeneratedSifgrs
block = pellet
execute_on = 'linear'
[]
[fission_gas_grain]
type = ElementIntegralFisGasGrainSifgrs
block = pellet
outputs = exodus
execute_on = 'linear'
[]
[fission_gas_boundary]
type = ElementIntegralFisGasBoundarySifgrs
block = pellet
outputs = exodus
execute_on = 'linear'
[]
[flux_from_clad] # area integrated heat flux from the cladding
type = SideDiffusiveFluxIntegral
variable = temperature
boundary = 5
diffusivity = thermal_conductivity
[]
[flux_from_fuel] # area integrated heat flux from the fuel
type = SideDiffusiveFluxIntegral
variable = temperature
boundary = 10
diffusivity = thermal_conductivity
[]
[rod_total_power]
type = ElementIntegralPower
variable = temperature
burnup_function = burnup
block = pellet
[]
[rod_input_power]
type = FunctionValuePostprocessor
function = power_history
scale_factor = 0.1186 # rod height
[]
[max_fuel_temp]
type = NodalExtremeValue
block = pellet
value_type = max
variable = temperature
[]
[max_clad_temp]
type = NodalExtremeValue
block = clad
value_type = max
variable = temperature
[]
[max_clad_hoop_strain]
type = ElementExtremeValue
block = clad
value_type = max
variable = strain_zz
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = clad
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
block = clad
execute_on = 'initial timestep_end'
[]
[volume_pulverized]
type = ElementIntegralMaterialProperty
mat_prop = pulverized
block = pellet
[]
[max_fuel_temp_periphery]
type = NodalExtremeValue
value_type = max
variable = temperature
boundary = 10
[]
[additional_volume]
type = FunctionValuePostprocessor
function = 8.5e-6
execute_on = 'initial linear'
[]
[addition_temperature]
type = FunctionValuePostprocessor
function = 300.0
execute_on = 'initial linear'
[]
[equilibrium_pressure]
type = FunctionValuePostprocessor
function = 101325.0
execute_on = 'initial linear'
[]
[]
[PerformanceMetricOutputs]
[]
[StandardLWRFuelRodOutputs]
temperature = temperature
fuel_pellet_blocks = 3
[]
[Outputs]
perf_graph = true
exodus = true
color = false
csv = true
[chkfile]
type = CSV
execute_on = FINAL
show = 'volume_pulverized'
[]
[]
(assessment/LWR/validation/LOCA_IFA_650/analysis/IFA_650_2/IFA_650_2.i)
[GlobalParams]
density = 10412 # 0.95TD UO2, TD=10960
temperature = temp
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
energy_per_fission = 3.2e-11 # J/fission
volumetric_locking_correction = false
[]
[Mesh]
coord_type = RZ
patch_size = 10 # For contact algorithm
patch_update_strategy = auto
partitioner = centroid
centroid_partitioner_direction = y
[mesh]
type = FileMeshGenerator
file = mesh_ife6502_medium2.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temp]
initial_condition = 300.
[]
[]
[AuxVariables]
[fast_neutron_flux]
[]
[fast_neutron_fluence]
[]
[grain_radius]
initial_condition = 5.e-06 # !! assumption
[]
[max_fission_rate]
[]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[scale_thickness] # ZrO2 scale thickness (m)
order = CONSTANT
family = MONOMIAL
[]
[oxywtfract_total] # Current oxigen weight fraction (oxide+metal) (/)
order = CONSTANT
family = MONOMIAL
[]
[oxywtfgain_total] # Gained oxigen weight fraction (oxide+metal) (/)
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[gap_cond]
order = CONSTANT
family = MONOMIAL
[]
[bbl_bdr_2]
order = CONSTANT
family = MONOMIAL
[]
[rad_bbl_bdr]
order = CONSTANT
family = MONOMIAL
[]
[sat_coverage]
order = CONSTANT
family = MONOMIAL
[]
[GBCoverage]
order = CONSTANT
family = MONOMIAL
[]
[deltav_v0_bd]
order = CONSTANT
family = MONOMIAL
[]
[]
[Functions]
[average_linear_heat_rate]
type = PiecewiseLinear
data_file = linear_heat_rate_av.csv
format = columns
scale_factor = 1
[]
[axial_power_peaking_factors]
type = PiecewiseBilinear
data_file = axial_peaking_factors_lhr.csv
scale_factor = 1
axis = 1 # (0,1,2) => (x,y,z)
[]
[average_clad_outer_temperature]
type = PiecewiseLinear
data_file = temperature_clad_outer_av.csv
format = columns
scale_factor = 1
[]
[axial_temperature_peaking_factors]
type = PiecewiseBilinear
data_file = axial_peaking_factors_ctemp.csv
scale_factor = 1
axis = 1 # (0,1,2) => (x,y,z)
[]
[clad_outer_temperature]
type = CompositeFunction
functions = 'average_clad_outer_temperature axial_temperature_peaking_factors'
[]
[coolant_pressure]
type = PiecewiseLinear
data_file = pressure_rig.csv
format = columns
scale_factor = 1
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[uo2nat]
block = 'pellet_type_1 pellet_type_3'
strain = FINITE
incremental = true
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
eigenstrain_names = 'uo2nat_thermal_strain'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz hoop_stress
hoop_strain'
decomposition_method = EigenSolution
[]
[fuel]
block = pellet_type_2
strain = FINITE
incremental = true
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
eigenstrain_names = 'fuel_thermal_strain fuel_relocation_eigenstrain
fuel_volumetric_swelling_eigenstrain'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz hoop_stress
hoop_strain'
[]
[clad]
block = clad
strain = FINITE
incremental = true
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
eigenstrain_names = 'clad_thermal_strain clad_irradiation_growth'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz hoop_stress
hoop_strain'
decomposition_method = EigenSolution
[]
[]
[Kernels]
[gravity] # body force term in stress equilibrium equation
type = Gravity
variable = disp_y
value = -9.81
[]
[heat]
type = HeatConduction
variable = temp
#extra_vector_tags = 'ref'
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temp
#extra_vector_tags = 'ref'
[]
[heat_source]
type = NeutronHeatSource
variable = temp
#extra_vector_tags = 'ref'
block = pellet_type_2
fission_rate = fission_rate
decay_heat_function = decay_heat_function # Couple to postprocessor which defines the decay heat function
max_fission_rate = max_fission_rate # Couple to auxvariable which defines maximum fission rate over irradiation
[]
[]
[Burnup]
[burnup]
block = pellet_type_2
rod_ave_lin_pow = average_linear_heat_rate
axial_power_profile = axial_power_peaking_factors
num_radial = 80
num_axial = 11
a_lower = 28.5e-03 # mesh dependent
a_upper = 528.5e-03 # mesh dependent
fuel_inner_radius = 0.
fuel_outer_radius = 4.145e-03
fuel_volume_ratio = 1. # for use with dished pellets (ratio of actual volume to cylinder volume)
RPF = RPF
[]
[]
[AuxKernels]
[fast_neutron_flux]
type = FastNeutronFluxAux
variable = fast_neutron_flux
block = clad
rod_ave_lin_pow = average_linear_heat_rate
axial_power_profile = axial_power_peaking_factors
factor = 3.e+13
execute_on = timestep_begin
[]
[fast_neutron_fluence]
type = FastNeutronFluenceAux
variable = fast_neutron_fluence
block = clad
fast_neutron_flux = fast_neutron_flux
execute_on = timestep_begin
[]
[grain_radius]
type = GrainRadiusAux
block = pellet_type_2
variable = grain_radius
temperature = temp
execute_on = linear
[]
[max_fission_rate]
type = MaxFissionRateAux
variable = max_fission_rate
block = pellet_type_2
fission_rate = fission_rate
execute_on = timestep_begin
[]
[creep_rate]
type = MaterialRealAux
block = clad
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
block = clad
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
block = clad
variable = fract_beta_phase
property = fract_beta_phase
[]
[scl_thickness]
type = MaterialRealAux
boundary = 2
variable = scale_thickness
property = oxide_scale_thickness
[]
[ofract_total]
type = MaterialRealAux
boundary = 2
variable = oxywtfract_total
property = current_oxygen_weight_frac_total
[]
[ofgain_total]
type = MaterialRealAux
boundary = 2
variable = oxywtfgain_total
property = oxygen_weight_frac_gained_total
[]
[sigmaburst]
type = MaterialRealAux
boundary = 2
variable = burst_stress
property = burst_stress
[]
[hasburst]
type = MaterialRealAux
boundary = 2
variable = burst
property = failed
execute_on = timestep_end
[]
[conductance]
type = MaterialRealAux
boundary = 10
property = gap_conductance
variable = gap_cond
[]
[nbbl2]
type = MaterialRealAux
block = pellet_type_2
variable = bbl_bdr_2
property = bubble_GB_surface_density
[]
[radbbl]
type = MaterialRealAux
block = pellet_type_2
variable = rad_bbl_bdr
property = bubble_radius_GB
[]
[stcvrg]
type = MaterialRealAux
block = pellet_type_2
variable = sat_coverage
property = sat_coverage
[]
[frcvrg]
type = MaterialRealAux
block = pellet_type_2
variable = GBCoverage
property = GBCoverage
[]
[dvv0bd]
type = MaterialRealAux
block = pellet_type_2
variable = deltav_v0_bd
property = deltav_v0_bubble_GB
[]
[]
[Contact]
# Define mechanical contact between the fuel (sideset=10) and the clad (sideset=5)
[pellet_clad_mechanical]
primary = 5
secondary = 10
penalty = 1.e+07
[]
[]
#TODO: Add option in StandardLWRFuelRodOutputs to compute plenum temperature this way.
# We are using 'plenum_temp' rather than 'plenum_temperature', which is generated
# automatically by StandardLWRFuelRodOutputs, but computed in a different way.
[PlenumTemperature]
[plenum_temp]
boundary = 5
inner_surfaces = '5'
outer_surfaces = '10'
temperature = temp
[]
[]
[ThermalContact]
# Define thermal contact between the fuel (sideset=10) and the clad (sideset=5)
[thermal_contact]
type = GasGapHeatTransfer
variable = temp
primary = 5
secondary = 10
initial_moles = initial_moles
gas_released = fission_gas_released
plenum_pressure = plenum_pressure
contact_pressure = contact_pressure
jump_distance_model = LANNING
quadrature = true
normal_smoothing_distance = 0.1
[]
[]
[BCs]
[no_x_all] # pin pellets and clad along axis of symmetry (y)
type = DirichletBC
variable = disp_x
boundary = 12
value = 0.
[]
[no_y_clad_bottom] # pin clad bottom in the axial direction (y)
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.
[]
[no_y_fuel_bottom] # pin fuel bottom in the axial direction (y)
type = DirichletBC
variable = disp_y
boundary = '1020'
value = 0.
[]
[clad_outer_temperature]
type = FunctionDirichletBC
boundary = '1 2 3'
variable = temp
function = clad_outer_temperature
[]
[Pressure] # apply coolant pressure on clad outer walls
[coolantPressure]
boundary = '1 2 3'
function = coolant_pressure # use the pressure_ramp function defined above
[]
[]
[PlenumPressure] # apply plenum pressure on clad inner walls and pellet surfaces
[plenumPressure]
boundary = 9
initial_pressure = 4.e+06
startup_time = -200
R = 8.3143
output_initial_moles = initial_moles
temperature = plenum_temp
volume = plenum_volume
material_input = fission_gas_released
output = plenum_pressure
[]
[]
[]
[Materials]
[fuel_density]
type = Density
block = pellet_type_2
[]
[fuel_thermal]
type = UO2Thermal
block = pellet_type_2
thermal_conductivity_model = FINK_LUCUTA
temperature = temp
burnup_function = burnup
[]
[fuel_thermal_expansion]
type = ComputeThermalExpansionEigenstrain
block = pellet_type_2
thermal_expansion_coeff = 10.0e-6
temperature = temp
stress_free_temperature = 295.0
eigenstrain_name = fuel_thermal_strain
[]
[fuel_elasticity_tensor]
type = UO2ElasticityTensor
block = pellet_type_2
[]
[fuel_stress]
type = ComputeFiniteStrainElasticStress
block = pellet_type_2
[]
[fuel_swelling]
type = UO2VolumetricSwellingEigenstrain
gas_swelling_model_type = SIFGRS
block = pellet_type_2
temperature = temp
burnup_function = burnup
initial_porosity = 0.0468
initial_fuel_density = 10447.
eigenstrain_name = fuel_volumetric_swelling_eigenstrain
[]
[fuel_relocation]
type = UO2RelocationEigenstrain
block = pellet_type_2
burnup_function = burnup
diameter = 0.00829
rod_ave_lin_pow = average_linear_heat_rate
axial_power_profile = axial_power_peaking_factors
diametral_gap =70.e-06
burnup_relocation_stop = 1.e+20
eigenstrain_name = fuel_relocation_eigenstrain
relocation_activation1 = 19685.039
[]
[fission_gas]
type = UO2Sifgrs
block = pellet_type_2
temperature = temp
fission_rate = fission_rate
grain_radius = grain_radius
gbs_model = true
transient_option = MICROCRACKING_BURNUP
[]
[clad_density]
type = Density
block = clad
density = 6550.
[]
[clad_thermal]
block = clad
type = ZryThermal
temperature = temp
[]
[clad_thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = clad
temperature = temp
stress_free_temperature = 300.0 #TODO: It is odd to have different values for fuel and clad, but keeping this way to match SM
eigenstrain_name = clad_thermal_strain
[]
[clad_elasticity_tensor]
type = ComputeIsotropicElasticityTensor
block = clad
youngs_modulus = 1.e+11
poissons_ratio = 0.3
[]
[zry_thermal_creep]
type = ZryCreepLOCAUpdate
block = clad
temperature = temp
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 3.e-03
#TODO: The parameters below really should be provided, but they weren't specified in the SM model.
# They may have not been included because irradiation creep wasn't modeled. However, they are used in the thermal
# creep model as well.
# fast_neutron_flux = fast_neutron_flux
# fast_neutron_fluence = fast_neutron_fluence
[]
[clad_stress]
type = ComputeMultipleInelasticStress
tangent_operator = elastic
inelastic_models = 'zry_thermal_creep'
block = clad
[]
[clad_irradiation_growth]
type = ZryIrradiationGrowthEigenstrain
block = clad
fast_neutron_fluence = fast_neutron_fluence
zircaloy_material_type = ESCORE_IrradiationGrowthZr4
eigenstrain_name = clad_irradiation_growth
[]
[clad_phase]
type = ZrPhase
block = clad
temperature = temp
numerical_method = 2
[]
[clad_oxidation]
type = ZryOxidation
boundary = 2
temperature = temp
clad_inner_radius = 4.18e-03
clad_outer_radius = 4.75e-03
normal_operating_temperature_model = epri_kwu_ce
high_temperature_model = leistikow
#use_coolant_channel = true
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = 2
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
#eff_strain_rate_plast =
fraction_beta_phase = fract_beta_phase
fraction_oxygen_gain = oxywtfract_total
temperature = temp
[]
[uo2nat_thermal]
type = HeatConductionMaterial
block = 'pellet_type_1 pellet_type_3'
thermal_conductivity = 3. # !! assumption
specific_heat = 300. # !! assumption
[]
[uo2nat_density]
type = Density
block = 'pellet_type_1 pellet_type_3'
[]
[uo2nat_thermal_expansion]
type = ComputeThermalExpansionEigenstrain
block = 'pellet_type_1 pellet_type_3'
thermal_expansion_coeff = 10.0e-6
temperature = temp
stress_free_temperature = 295.0
eigenstrain_name = uo2nat_thermal_strain
[]
[uo2nat_elasticity_tensor]
type = UO2ElasticityTensor
block = 'pellet_type_1 pellet_type_3'
[]
[uo2nat_stress]
type = ComputeFiniteStrainElasticStress
block = 'pellet_type_1 pellet_type_3'
[]
[]
[Dampers]
[limitT]
type = MaxIncrement
max_increment = 100.
variable = temp
[]
[limitX]
type = MaxIncrement
max_increment = 1.e-05
variable = disp_x
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1.e-02
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-10
start_time = -200
n_startup_steps = 1
end_time = 229440
dtmax = 2700. #1000.
dtmin = 0.00000001
[TimeStepper]
type = IterationAdaptiveDT
dt = 200.
#optimal_iterations = 4
#iteration_window = 2
#linear_iteration_ratio = 100
timestep_limiting_function = average_clad_outer_temperature
max_function_change = 10
timestep_limiting_postprocessor = material_timestep
time_t = '-200. 0. 3.5e+04 216000. 218700. 219180. 219240. 219799. 219819. 219821. 219999.'
time_dt = ' 200. 900. 2700. 2700. 60. 60. 20. 20.
10. 10. 2.'
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '5'
include_fuel = true
[]
[]
[Postprocessors]
[decay_heat_function]
type = DecayHeatFunction
time_at_shutdown = 100000001.
[]
[clad_inner_vol] # volume inside of cladding
type = InternalVolume
boundary = 7
execute_on = 'initial linear'
[]
[avg_clad_temp] # average temperature of cladding interior
type = SideAverageValue
boundary = 7
variable = temp
execute_on = 'initial timestep_end'
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temp
block = clad
execute_on = 'initial timestep_end'
[]
[max_fuel_temp]
type = NodalExtremeValue
value_type = max
variable = temp
block = pellet_type_2
execute_on = 'initial timestep_end'
[]
[central_fuel_temp]
type = NodalVariableValue
variable = temp
nodeid = 54 # Global node ID = 55 !! Mesh dependent
execute_on = 'initial timestep_end'
[]
[flux_from_clad] # area integrated heat flux from the cladding
type = SideDiffusiveFluxIntegral
variable = temp
boundary = 5
diffusivity = thermal_conductivity
execute_on = 'initial linear'
[]
[flux_from_fuel] # area integrated heat flux from the fuel
type = SideDiffusiveFluxIntegral
variable = temp
boundary = 10
diffusivity = thermal_conductivity
execute_on = 'initial linear'
[]
[alhr_input]
type = FunctionValuePostprocessor
function = average_linear_heat_rate
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = clad
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
block = clad
execute_on = 'initial timestep_end'
[]
[max_oxygen_fract]
type = ElementExtremeValue
block = clad
value_type = max
variable = oxywtfract_total
execute_on = 'initial timestep_end'
[]
[max_oxygen_fgain]
type = ElementExtremeValue
block = clad
value_type = max
variable = oxywtfgain_total
execute_on = 'initial timestep_end'
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
block = clad
execute_on = 'initial timestep_end'
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
block = clad
execute_on = 'initial timestep_end'
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = hoop_strain
block = clad
execute_on = 'initial timestep_end'
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
block = clad
execute_on = 'initial timestep_end'
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
block = clad
execute_on = 'initial timestep_end'
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = hoop_strain
block = clad
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
fuel_pellet_blocks = pellet_type_2
temperature = temp
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
print_linear_residuals = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[out_vector_pp]
execute_vector_postprocessors_on = 'timestep_end'
type = CSV
[]
[]
(assessment/LWR/validation/LOCA_REBEKA_cladding_burst_tests/analysis/rebeka_2d_10MPa/rebeka_singlerod_2d_10MPa_1pt5.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
order = SECOND
family = LAGRANGE
volumetric_locking_correction = false
displacements = 'disp_x'
[]
[Mesh]
coord_type = RZ
[layered1D_mesh]
type = Layered1DMeshGenerator
clad_mesh_density = customize
include_fuel = false
include_clad = true
include_plenum = false
pellet_outer_radius = 0.00465
clad_gap_width = 0
clad_thickness = 0.000725
fuel_height = 0.1625
slices_per_block = 10
pellet_bottom_coor = 0.0
nx_c = 1
[]
patch_update_strategy = auto
partitioner = centroid
centroid_partitioner_direction = y
[]
[UserObjects]
[pin_geometry]
type = Layered1DFuelPinGeometry
include_fuel = false
mesh_generator = layered1D_mesh
[]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[]
[Variables]
[temperature]
initial_condition = 573.0
[]
[]
[Functions]
[temperature_func]
type = PiecewiseLinear
x = '0. 700. '
y = '573. 1273.' # From 300 to 1000 C at 1 K/s
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 700. '
y = '1.e+07 1.e+07' # 100 bar
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 700. '
y = '1.e+05 1.e+05' # atmospheric pressure
[]
[clad_axial_pressure]
type = CladdingAxialPressureFunction
plenum_pressure = inner_pressure_func
coolant_pressure = outer_pressure_func
coolant_pressure_scaling_factor = 1
fuel_pin_geometry = pin_geometry
[]
[]
[Physics/SolidMechanics/Layered1D]
[clad]
block = clad
add_variables = true
strain = FINITE
add_scalar_variables = true
out_of_plane_strain_name = strain_yy
fuel_pin_geometry = pin_geometry
out_of_plane_pressure_function = clad_axial_pressure
decomposition_method = EigenSolution
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
eigenstrain_names = 'clad_thermal_eigenstrain'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz
creep_strain_xx creep_strain_yy creep_strain_xy creep_strain_zz strain_xx
strain_yy strain_zz hoop_stress'
group_scalar_vars_in_reference_residual = false
mesh_generator = layered1D_mesh
[]
[]
[AuxVariables]
[disp_y] ## Required for easier visualization in Paraview
[]
[disp_z] ## Required for easier visualization in Paraview
[]
[creep_rate_aux]
order = CONSTANT
family = MONOMIAL
[]
[effective_creep_strain]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[scale_thickness]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfract_total]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfgain_total]
order = CONSTANT
family = MONOMIAL
[]
[burst_stress]
order = CONSTANT
family = MONOMIAL
[]
[burst]
order = CONSTANT
family = MONOMIAL
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate_aux]
type = MaterialRealAux
variable = creep_rate_aux
property = creep_rate
execute_on = timestep_end
[]
[effective_creep_strain]
type = MaterialRealAux
property = effective_creep_strain
variable = effective_creep_strain
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[scl_thickness]
type = MaterialRealAux
variable = scale_thickness
property = oxide_scale_thickness
boundary = 2
[]
[ofract_total]
type = MaterialRealAux
variable = oxywtfract_total
property = current_oxygen_weight_frac_total
boundary = 2
[]
[ofgain_total]
type = MaterialRealAux
boundary = 2
variable = oxywtfgain_total
property = oxygen_weight_frac_gained_total
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = 2
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = 2
execute_on = timestep_end
[]
[]
[BCs]
[inner_temperature]
type = REBEKADirichletBC
variable = temperature
function_tempm = temperature_func
minimum_temperature = 573.0
translation = 0.1625
boundary = 5
[]
[Pressure]
[outer_pressure] # apply steam pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 5
function = inner_pressure_func
[]
[]
[]
[CoolantChannel]
[convective_clad_surface]
boundary = 2
variable = temperature
inlet_temperature = 473.
inlet_pressure = 1.e+05
inlet_massflux = 1. # kg/m^2-sec # almost stagnant steam
rod_diameter = 10.75e-03
rod_pitch = 1.26e-02 # default
oxide_thickness = scale_thickness
[]
[]
[Materials]
[thermal]
type = ZryThermal
block = clad
temperature = temperature
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = clad
matpro_youngs_modulus = false
matpro_poissons_ratio = false
[]
[clad_stress]
type = ComputeMultipleInelasticStress
tangent_operator = elastic
inelastic_models = 'clad_zrycreep'
block = clad
[]
[clad_zrycreep]
type = ZryCreepLOCAUpdate
block = clad
temperature = temperature
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
temperature_loca_creep_begin = 501
temperature_standard_thermal_creep_end = 500
[]
[thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = clad
temperature = temperature
stress_free_temperature = 573.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[density]
type = Density
block = clad
[]
[phase]
type = ZrPhase
block = clad
temperature = temperature
numerical_method = 2
[]
[oxidation]
type = ZryOxidation
boundary = 2
temperature = temperature
clad_inner_radius = 0.00465
clad_outer_radius = 0.005375
normal_operating_temperature_model = epri_kwu_ce
high_temperature_model = leistikow
use_coolant_channel = true
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = 2
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate_aux
temperature = temperature
fraction_beta_phase = fract_beta_phase
fraction_oxygen_gain = oxywtfgain_total
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-06
nl_abs_tol = 1.e-08
start_time = 0
n_startup_steps = 1
end_time = 700.
dtmax = 1.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[Postprocessors]
[ave_clad_exterior_temp]
type = LayeredSideAverageValuePostprocessor
boundary = 2
variable = temperature
fuel_pin_geometry = pin_geometry
[]
[max_clad_temp]
type = NodalExtremeValue
block = clad
value_type = max
variable = temperature
[]
[min_clad_temp]
type = NodalExtremeValue
block = clad
value_type = min
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = clad
[]
[max_oxygen_fract]
type = ElementExtremeValue
block = clad
value_type = max
variable = oxywtfract_total
[]
[max_betaph_fract]
type = ElementExtremeValue
block = clad
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
block = clad
value_type = max
variable = creep_rate_aux
[]
[max_eff_creep_strain]
type = ElementExtremeValue
block = clad
value_type = max
variable = effective_creep_strain
[]
[max_hoop_strain]
type = ElementExtremeValue
block = clad
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
block = clad
value_type = max
variable = hoop_stress
[]
[vonmises_stress_clad]
type = ElementAverageValue
block = clad
variable = vonmises_stress
[]
[min_burst_stress]
type = ElementExtremeValue
block = clad
value_type = min
variable = burst_stress
[]
[burst]
type = ElementExtremeValue
block = clad
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = clad
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = pin_geometry
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[top_disp_r_clad_slice] # this is mid height
type = NodalVariableValue
variable = disp_x
nodeid = 28 # 1 line element
[]
[inner_pressure_func]
type = FunctionValuePostprocessor
function = inner_pressure_func
execute_on = 'initial linear'
[]
[stress_xx] # stess in the top Element
type = ElementalVariableValue
variable = stress_xx
elementid = 9 #single line element
[]
[stress_yy] # stess in the top Element
type = ElementalVariableValue
variable = stress_yy
elementid = 9 #single line element
[]
[stress_zz] # stess in the top Element
type = ElementalVariableValue
variable = stress_zz
elementid = 9 #single line element
[]
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = rebeka_2d_10MPa_1pt5_out_chkfile
show = 'ave_clad_exterior_temp max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/LOCA_ORNL_cladding_burst_tests/analysis/Zr2_2/ornl_zr2_2_aniso.i)
# Simulation ORNL burst tests Zr2_2
[GlobalParams]
density = 6550.
order = SECOND
family = LAGRANGE
displacements = 'disp_x disp_y'
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = zr2_ornl_burst_test_mesh.e
[]
[]
[Variables]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func] # only 10 inches of the rod are within the heated zone (cf. Terrani email)
type = PiecewiseBilinear
data_file = temperature_ornl_zr2_2.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
data_file = pressure_inner_ornl_zr2_2.csv
scale_factor = 1.e+06
format = columns
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 700. '
y = '0.1 0.1 ' # atmospheric pressure
scale_factor = 1.e+06
[]
# Circumferential steady-state creep test and analysis of Zircaloy-4 fuelcladding
# Nuclear Engineering and Design, 53, 2312-2322 (2021)
[F]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.738 0.57 0.57'
[]
[G]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.174 0.45 0.45'
[]
[H]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.588 0.48 0.48'
[]
[L]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[M]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[N]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[clad]
use_automatic_differentiation = true
block = cladding
add_variables = true
strain = FINITE
decomposition_method = TaylorExpansion
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
eigenstrain_names = 'clad_thermal_eigenstrain'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz hoop_stress'
[]
[]
[AuxVariables]
[creep_rate_aux]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[scale_thickness]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfract_total]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfgain_total]
order = CONSTANT
family = MONOMIAL
[]
[burst_stress]
order = CONSTANT
family = MONOMIAL
[]
[burst]
order = CONSTANT
family = MONOMIAL
[]
[]
[Kernels]
[heat]
type = ADHeatConduction
variable = temperature
[]
[heat_ie]
type = ADHeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate_aux]
type = ADMaterialRealAux
variable = creep_rate_aux
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = ADMaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[scl_thickness]
type = ADMaterialRealAux
variable = scale_thickness
property = oxide_scale_thickness
boundary = 2
[]
[ofract_total]
type = ADMaterialRealAux
variable = oxywtfract_total
property = current_oxygen_weight_frac_total
boundary = 2
[]
[ofgain_total]
type = ADMaterialRealAux
boundary = 2
variable = oxywtfgain_total
property = oxygen_weight_frac_gained_total
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = 2
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = 2
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = ADFunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 4'
preset = false
[]
[no_y_top]
type = ADDirichletBC
variable = disp_y
boundary = 3
value = 0.
preset = false
[]
[Pressure]
[outer_pressure] # apply steam pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[mid_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 2 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
type = ADZryThermal
block = cladding
temperature = temperature
[]
[clad_elasticity_tensor]
type = ADZryElasticityTensor
block = cladding
matpro_youngs_modulus = false
matpro_poissons_ratio = false
[]
[clad_stress]
type = ADComputeMultipleInelasticStress
inelastic_models = 'clad_zrycreep'
block = cladding
[]
[hill_constants]
type = ADHillConstants
# hill_constants = "0.5 0.5 0.5 1.0 1.0 1.0"
hill_constants = "0.738 0.174 0.588 1.0 1.0 1.0"
function_names = "F G H L M N"
[]
[clad_zrycreep]
type = ADZryAnisoCreepLOCAUpdate
block = cladding
temperature = temperature
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
temperature_loca_creep_begin = 301
temperature_standard_thermal_creep_end = 300
fract_beta_phase_name = 'ad_fract_beta_phase'
[]
[thermal_expansion]
type = ADZryThermalExpansionMATPROEigenstrain
block = cladding
temperature = temperature
stress_free_temperature = 300.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[density]
type = ADDensity
block = cladding
[]
[phase]
type = ZrPhase
block = cladding
temperature = temperature
numerical_method = 2
[]
[phase_converter]
type = MaterialADConverter
reg_props_in = 'fract_beta_phase'
ad_props_out = 'ad_fract_beta_phase'
[]
[oxidation]
type = ADZryOxidation
boundary = 2
temperature = temperature
clad_inner_radius = 0.004875
clad_outer_radius = 0.005580
normal_operating_temperature_model = epri_kwu_ce
high_temperature_model = leistikow
#use_coolant_channel = true
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = 2
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate_aux
temperature = temperature
fraction_beta_phase = fract_beta_phase
fraction_oxygen_gain = oxywtfgain_total
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = PJFNK
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0
n_startup_steps = 1
end_time = 700.
dtmax = 2.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 2.
[]
[]
[Postprocessors]
[pressure_inner]
type = FunctionValuePostprocessor
function = inner_pressure_func
execute_on = 'initial timestep_end'
[]
[pressure_outer]
type = FunctionValuePostprocessor
function = outer_pressure_func
execute_on = 'initial timestep_end'
[]
[ave_clad_temp]
type = SideAverageValue
boundary = 2
variable = temperature
execute_on = 'initial timestep_end'
[]
[max_clad_temp]
type = NodalExtremeValue
block = cladding
value_type = max
variable = temperature
execute_on = 'initial timestep_end'
[]
[min_clad_temp]
type = NodalExtremeValue
block = cladding
value_type = min
variable = temperature
execute_on = 'initial timestep_end'
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = cladding
[]
[max_oxygen_fract]
type = ElementExtremeValue
block = cladding
value_type = max
variable = oxywtfract_total
execute_on = 'initial timestep_end'
[]
[max_betaph_fract]
type = ElementExtremeValue
block = cladding
value_type = max
variable = fract_beta_phase
execute_on = 'initial timestep_end'
[]
[max_creep_rate]
type = ElementExtremeValue
block = cladding
value_type = max
variable = creep_rate_aux
execute_on = 'initial timestep_end'
[]
[max_creep_strain_mag]
type = ElementExtremeValue
block = cladding
value_type = max
variable = creep_strain_mag
execute_on = 'initial timestep_end'
[]
[max_hoop_strain]
type = ElementExtremeValue
block = cladding
value_type = max
variable = strain_zz
execute_on = 'initial timestep_end'
[]
[max_hoop_stress]
type = ElementExtremeValue
block = cladding
value_type = max
variable = hoop_stress
[]
[vonmises_stress_clad]
type = ElementAverageValue
block = cladding
variable = vonmises_stress
execute_on = 'initial timestep_end'
[]
[min_burst_stress]
type = ElementExtremeValue
block = cladding
value_type = min
variable = burst_stress
execute_on = 'initial timestep_end'
[]
[burst]
type = ElementExtremeValue
block = cladding
value_type = max
variable = burst
execute_on = 'initial timestep_end'
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = cladding
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[mid_disp_r_clad]
type = NodalVariableValue
variable = disp_x
nodeid = 22
[]
[stress_xx_midplane] # stress in the mid Element
type = ElementalVariableValue
variable = stress_xx
elementid = 19
[]
[stress_yy_midplane] # stress in the mid Element
type = ElementalVariableValue
variable = stress_yy
elementid = 19
[]
[stress_zz_midplane] # stress in the mid Element
type = ElementalVariableValue
variable = stress_zz
elementid = 19
[]
[strain_zz_midplane] # strain in the mid Element
type = ElementalVariableValue
variable = strain_zz
elementid = 19
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
plenum_boundary_name = 4
cladding_blocks = cladding
[]
[PerformanceMetricOutputs]
[]
[Outputs]
exodus = true
perf_graph = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 20
[]
[chkfile]
type = CSV
file_base = ornl_zr2_2_aniso_chkfile
show = 'pressure_inner max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-15/puzry-15_aniso.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-15.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 2000. '
y = '1.e+05 1.e+05 1.183e+07' # Linear increase at 0.1173 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 2000. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
# Circumferential steady-state creep test and analysis of Zircaloy-4 fuel cladding
# Nuclear Engineering and Design, 53, 2312-2322 (2021)
[F]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.738 0.738 0.57'
[]
[G]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.174 0.174 0.45'
[]
[H]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.588 0.588 0.48'
[]
[L]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[M]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[N]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = TaylorExpansion
use_automatic_differentiation = true
[]
[]
[]
[]
[Kernels]
[heat]
type = ADHeatConduction
variable = temperature
[]
[heat_ie]
type = ADHeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = ADMaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = ADMaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = ADMaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = ADMaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = ADMaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = ADFunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = ADDirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = ADDirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ADZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1.e+11
poissons_ratio = 0.3
block = 1
[]
[hill_constants]
type = ADHillConstants
hill_constants = "0.738 0.174 0.588 1.0 1.0 1.0"
function_names = "F G H L M N"
temperature = temperature
[]
[creep_update]
type = ADZryAnisoCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 1.5e-05
temperature = temperature
temperature_standard_thermal_creep_end = 700
temperature_loca_creep_begin = 900.
fract_beta_phase_name = 'fract_beta_phase'
max_integration_error = 1000000.0
absolute_tolerance = 1e-13
relative_tolerance = 1e-11
[]
[creep]
type = ADComputeMultipleInelasticStress
block = 1
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ADZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = ADDensity
block = 1
[]
[phase]
type = ADZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ADZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = NEWTON
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-07
start_time = 0.
n_startup_steps = 1
end_time = 2500.
dtmax = 1.
dtmin = 1.0e-9
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-15_aniso_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-09/puzry-09.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[temperature]
initial_condition = 300.
[]
[disp_x]
[]
[disp_y]
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-09.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 1200. '
y = '1.e+05 1.e+05 1.524e+06' # Linear increase at 0.0712 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 1200. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = EigenSolution
[]
[]
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = MaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = FunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = DirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = DirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1.e+11
poissons_ratio = 0.3
block = 1
[]
[creep_update]
type = ZryCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 1.e-04
temperature = temperature
temperature_standard_thermal_creep_end = 700
temperature_loca_creep_begin = 900.
[]
[creep]
type = ComputeMultipleInelasticStress
block = 1
tangent_operator = elastic
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = Density
block = 1
[]
[phase]
type = ZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
active = 'smp'
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0.
n_startup_steps = 1
end_time = 1200.
dtmax = 1.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-09_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/LOCA_ORNL_cladding_burst_tests/analysis/Zr2_1/ornl_zr2_1_ad.i)
# Simulation ORNL burst tests Zr2_1
[GlobalParams]
density = 6550.
order = SECOND
family = LAGRANGE
displacements = 'disp_x disp_y'
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = zr2_ornl_burst_test_mesh.e
[]
[]
[Variables]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func] # only 10 inches of the rod are within the heated zone (cf. Terrani email)
type = PiecewiseBilinear
data_file = temperature_ornl_zr2_1.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
data_file = pressure_inner_ornl_zr2_1.csv
scale_factor = 1.e+06
format = columns
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 400. '
y = '0.1 0.1 ' # atmospheric pressure
scale_factor = 1.e+06
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[clad]
use_automatic_differentiation = true
block = cladding
add_variables = true
strain = FINITE
decomposition_method = TaylorExpansion
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
eigenstrain_names = 'clad_thermal_eigenstrain'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz hoop_stress'
[]
[]
[AuxVariables]
[creep_rate_aux]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[scale_thickness]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfract_total]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfgain_total]
order = CONSTANT
family = MONOMIAL
[]
[burst_stress]
order = CONSTANT
family = MONOMIAL
[]
[burst]
order = CONSTANT
family = MONOMIAL
[]
[]
[Kernels]
[heat]
type = ADHeatConduction
variable = temperature
[]
[heat_ie]
type = ADHeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate_aux]
type = ADMaterialRealAux
variable = creep_rate_aux
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = ADMaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[scl_thickness]
type = ADMaterialRealAux
variable = scale_thickness
property = oxide_scale_thickness
boundary = 2
[]
[ofract_total]
type = ADMaterialRealAux
variable = oxywtfract_total
property = current_oxygen_weight_frac_total
boundary = 2
[]
[ofgain_total]
type = ADMaterialRealAux
boundary = 2
variable = oxywtfgain_total
property = oxygen_weight_frac_gained_total
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = 2
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = 2
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = ADFunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 4'
preset = false
[]
[no_y_top]
type = ADDirichletBC
variable = disp_y
boundary = 3
value = 0.
preset = false
[]
[Pressure]
[outer_pressure] # apply steam pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[mid_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 2 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
type = ADZryThermal
block = cladding
temperature = temperature
[]
[clad_elasticity_tensor]
type = ADZryElasticityTensor
block = cladding
matpro_youngs_modulus = false
matpro_poissons_ratio = false
[]
[clad_stress]
type = ADComputeMultipleInelasticStress
inelastic_models = 'clad_zrycreep'
block = cladding
[]
[hill_constants]
type = ADHillConstants
hill_constants = "0.5 0.5 0.5 1.0 1.0 1.0"
#hill_constants = "0.738 0.174 0.588 1.0 1.0 1.0"
#function_names = "F G H L M N"
[]
[clad_zrycreep]
type = ADZryAnisoCreepLOCAUpdate
block = cladding
temperature = temperature
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
temperature_loca_creep_begin = 301
temperature_standard_thermal_creep_end = 300
fract_beta_phase_name = 'ad_fract_beta_phase'
[]
[thermal_expansion]
type = ADZryThermalExpansionMATPROEigenstrain
block = cladding
temperature = temperature
stress_free_temperature = 300.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[density]
type = ADDensity
block = cladding
[]
[phase]
type = ZrPhase
block = cladding
temperature = temperature
numerical_method = 2
[]
[phase_converter]
type = MaterialADConverter
reg_props_in = 'fract_beta_phase'
ad_props_out = 'ad_fract_beta_phase'
[]
[oxidation]
type = ADZryOxidation
boundary = 2
temperature = temperature
clad_inner_radius = 0.004875
clad_outer_radius = 0.005580
normal_operating_temperature_model = epri_kwu_ce
high_temperature_model = leistikow
#use_coolant_channel = true
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = 2
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate_aux
temperature = temperature
fraction_beta_phase = fract_beta_phase
fraction_oxygen_gain = oxywtfgain_total
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = PJFNK
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0
n_startup_steps = 1
end_time = 400.
dtmax = 1.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[Postprocessors]
[pressure_inner]
type = FunctionValuePostprocessor
function = inner_pressure_func
execute_on = 'initial timestep_end'
[]
[pressure_outer]
type = FunctionValuePostprocessor
function = outer_pressure_func
execute_on = 'initial timestep_end'
[]
[ave_clad_temp]
type = SideAverageValue
boundary = 2
variable = temperature
execute_on = 'initial timestep_end'
[]
[max_clad_temp]
type = NodalExtremeValue
block = cladding
value_type = max
variable = temperature
execute_on = 'initial timestep_end'
[]
[min_clad_temp]
type = NodalExtremeValue
block = cladding
value_type = min
variable = temperature
execute_on = 'initial timestep_end'
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = cladding
[]
[max_oxygen_fract]
type = ElementExtremeValue
block = cladding
value_type = max
variable = oxywtfract_total
execute_on = 'initial timestep_end'
[]
[max_betaph_fract]
type = ElementExtremeValue
block = cladding
value_type = max
variable = fract_beta_phase
execute_on = 'initial timestep_end'
[]
[max_creep_rate]
type = ElementExtremeValue
block = cladding
value_type = max
variable = creep_rate_aux
execute_on = 'initial timestep_end'
[]
[max_creep_strain_mag]
type = ElementExtremeValue
block = cladding
value_type = max
variable = creep_strain_mag
execute_on = 'initial timestep_end'
[]
[max_hoop_strain]
type = ElementExtremeValue
block = cladding
value_type = max
variable = strain_zz
execute_on = 'initial timestep_end'
[]
[max_hoop_stress]
type = ElementExtremeValue
block = cladding
value_type = max
variable = hoop_stress
[]
[vonmises_stress_clad]
type = ElementAverageValue
block = cladding
variable = vonmises_stress
execute_on = 'initial timestep_end'
[]
[min_burst_stress]
type = ElementExtremeValue
block = cladding
value_type = min
variable = burst_stress
execute_on = 'initial timestep_end'
[]
[burst]
type = ElementExtremeValue
block = cladding
value_type = max
variable = burst
execute_on = 'initial timestep_end'
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = cladding
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[mid_disp_r_clad]
type = NodalVariableValue
variable = disp_x
nodeid = 22
[]
[stress_xx_midplane] # stress in the mid Element
type = ElementalVariableValue
variable = stress_xx
elementid = 19
[]
[stress_yy_midplane] # stress in the mid Element
type = ElementalVariableValue
variable = stress_yy
elementid = 19
[]
[stress_zz_midplane] # stress in the mid Element
type = ElementalVariableValue
variable = stress_zz
elementid = 19
[]
[strain_zz_midplane] # strain in the mid Element
type = ElementalVariableValue
variable = strain_zz
elementid = 19
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
plenum_boundary_name = 4
cladding_blocks = cladding
[]
[PerformanceMetricOutputs]
[]
[Outputs]
exodus = true
perf_graph = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 20
[]
[chkfile]
type = CSV
file_base = ornl_zr2_1_ad_chkfile
show = 'pressure_inner max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(test/tests/standard_lwr_outputs_action/clad_nonstandard_names.i)
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
[]
[Mesh]
coord_type = RZ
[mesh]
type = GeneratedMeshGenerator
dim = 2
nx = 2
ny = 10
xmin = 1
xmax = 2
ymax = 5
[]
[]
[Variables]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
x = '0.0 0.025'
y = '0.0 300.0 300.0'
z = '1000.0 1400.0 1400.0 2000.0 1400.0 1400.0'
axis = 1 # (0,1,2) => (x,y,z)
[]
[power_history]
type = PiecewiseLinear
x = '0.000000 10800'
y = '0.000000 16404.200000' #LHR5
scale_factor = 1
[]
[axial_peaking_factors]
type = PiecewiseBilinear
x = '0.00324 3.77797'
y = '0.000000 10800'
z = '1.0 1.0 1.0 1.0'
axis = 1
scale_factor = 1
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 2000. '
y = '1.e+05 1.e+05 7.4e+05'
[]
[pressure_ramp]
type = PiecewiseLinear
scale_factor = 1
x = '0 10800.0'
y = '0.00651 1.0'
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[clad]
add_variables = true
strain = FINITE
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
[]
[]
[BCs]
[no_x_all]
type = DirichletBC
variable = disp_x
boundary = 'left'
value = 0.0
[]
[no_y_clad_bottom]
type = DirichletBC
variable = disp_y
boundary = 'bottom'
value = 0.0
[]
[Pressure]
[coolantPressure]
boundary = 'right'
factor = 15.5e6
function = pressure_ramp
[]
[]
[]
[CoolantChannel]
[convective_clad_surface]
boundary = 'right'
variable = temperature
inlet_temperature = 580
inlet_pressure = 15.5e6
inlet_massflux = 3800
rod_diameter = 0.948e-2
rod_pitch = 1.26e-2
linear_heat_rate = power_history
axial_power_profile = axial_peaking_factors
[]
[]
[Materials]
[thermal]
type = ZryThermal
temperature = temperature
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
[]
[clad_stress]
type = ComputeFiniteStrainElasticStress
[]
[density]
type = Density
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -sub_pc_type'
petsc_options_value = 'asm lu'
line_search = 'none'
l_max_its = 100
l_tol = 1e-8
nl_max_its = 15
nl_rel_tol = 1.e-8
nl_abs_tol = 1.e-10
start_time = 0.
end_time = 50.
dtmax = 10.0
dtmin = 10
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 0
plenum_boundary_name = 'left'
external_clad_boundary_name = 'right'
[]
[Outputs]
perf_graph = true
csv = true
[]
(test/tests/solid_mechanics/zry_mechanics/elastic_modulus_zry.i)
#--------------------------------------------------------------------------------
#
# This test case is prepared to test elastic moduli of zirconium alloy calculation
# using the matpro functions celmod.f and cshear.f for temperatures under the
# phase transistion temperature.
#
# - Geometry:
# Ri = 0.005 m
# Ro = 0.0055 m
# H = 0.01 m
#
# - Single element
# - Temperature = 300 - 1000 K
# - Boundary conditions:
# axial stress = -100 MPa at the top. The BC option has been changed from the
# original test's use of the Pressure action to a simplified Pressure BC that
# applies pressure to only the top surface in the axial (y-axis) direction
#
# Results:
# The strain in the radial direction can be calculated using the Young's modulus
# and the Poisson's ratio from the applied 100.0 MPa pressure.
# \f$ \epsilon_{rr} = v * \frac{\sigma_{axial}{E}} $/f
#
# The expected results for an increase in temperature under constant pressure:
# Temperature (K) strain_rr (m/m)
# 370 4.1484e-4
# 440 4.3968e-4
# 510 4.6753e-4
# 580 4.9896e-4
# 650 5.3468e-4
# 720 5.7557e-4
# 790 6.2282e-4
# 860 6.7795e-4
# 930 7.4301e-4
# 1000 8.2080e-4
#
# The final two timesteps maintain a constant temperature to demonstrate that
# the elastic properties are constant under constant temperature
#
#--------------------------------------------------------------------------------
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = clad_rz_short_rev3.e
[]
[]
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Variables]
[temp]
order = FIRST
family = LAGRANGE
initial_condition = 300
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[all]
strain = FINITE
block = 1
incremental = true
add_variables = true
generate_output = 'elastic_strain_xx'
[]
[]
[]
[]
[Functions]
[temperature_function]
type = PiecewiseLinear
x = '0 10'
y = '300 1000'
[]
[pressure_function]
type = PiecewiseLinear
x = '0 10'
y = '1 1'
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temp
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temp
[]
[]
[BCs]
[top_pressure] #Simplified BC to apply pressure in only disp_y
type = Pressure
boundary = 2
variable = disp_y
function = pressure_function
factor = 100e6
[]
[u_bottom_fix]
type = DirichletBC
variable = disp_y
boundary = 4
value = 0.0
[]
[temp_bc_1]
type = FunctionDirichletBC
variable = temp
boundary = '1 2 3 4'
function = temperature_function
[]
[]
[Materials]
[elasticity_tensor]
type = ZryElasticityTensor
temperature = temp
matpro_poissons_ratio = true
matpro_youngs_modulus = true
[]
[stress]
type = ComputeFiniteStrainElasticStress
[]
[clad_density]
type = Density
density = 7874
[]
[thermal]
type = ZryThermal
temperature = temp
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-ksp_gmres_restart'
petsc_options_value = '101'
line_search = 'none'
l_max_its = 100
nl_max_its = 100
nl_rel_tol = 1e-8
nl_abs_tol = 1e-8
l_tol = 1e-8
start_time = 0.0
end_time = 12
dt = 1
[]
[Postprocessors]
[elastic_strain_rr]
type = ElementAverageValue
variable = elastic_strain_xx
[]
[temp]
type = AverageNodalVariableValue
variable = temp
execute_on = 'initial timestep_end'
[]
[]
[Outputs]
exodus = true
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-22/puzry-22.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-22.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 6000. '
y = '1.e+05 1.e+05 7.5e+06' # Linear increase at 0.0148 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 6000. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = EigenSolution
[]
[]
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = MaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = FunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = DirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = DirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1.e+11
poissons_ratio = 0.3
block = 1
[]
[creep_update]
type = ZryCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 1.e-04
temperature = temperature
temperature_standard_thermal_creep_end = 700
temperature_loca_creep_begin = 900.
[]
[creep]
type = ComputeMultipleInelasticStress
block = 1
tangent_operator = elastic
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = Density
block = 1
[]
[phase]
type = ZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
active = 'smp'
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0.
n_startup_steps = 1
end_time = 6000.
dtmax = 1.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-22_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/IFA_677/analysis/IFA_677_Base.i)
# This is a partial input file that contains characteristics common to the entire assessment case
# NOTE: This file is not meant to be run on its own as it requires information contained in the .params files
# Fuel material properties
total_densification = 0.09e-2 # (-)
oxygen_to_metal_ratio = 2.002 # (-)
# Cladding material properties
cladding_density = 6550.0 # kg/m^3
# Cladding geometry
clad_inner_radius = 4.65e-3 # m
clad_outer_radius = 5.375e-3 # m
# Rod geometry
a_lower = 0.001025 # m
fuel_inner_radius = 0.0 # m
fuel_outer_radius = 0.4565e-02 # m
fuel_volume_ratio = 0.9940 # (-)
fuel_diameter = 9.13e-3 # m
diametral_gap = 170.e-6 # m
# Neutronics, power, and isotope fractions
energy_per_fission = 3.28451e-11 # J/fission
isotope_fraction_Pu239 = 0.0
isotope_fraction_Pu240 = 0.0
isotope_fraction_Pu241 = 0.0
isotope_fraction_Pu242 = 0.0
# Temperature conditions
initial_temperature = 293.0 # K
stress_free_temperature = 293.0 # K
# Coolant pressure ramp parameters
pressure_ramp_x = '-200 0'
pressure_ramp_y = '0.0298 1'
pressure_ramp_factor = 3.4e6 # (-)
# Coolant Channel parameters
inlet_pressure = 3.4e+06 # Pa
inlet_massflux = 450. # kg/m^2-s
rod_diameter = 10.75e-03 # m
rod_pitch = 46.e-03 # m
htc_correlation_type = 2
# Contact
contact_penalty = 1e14 # (-)
roughness_primary = 5.0e-6
roughness_secondary = 0.32e-6
roughness_coef = 3.2
normal_smoothing_distance = 0.1 # m
# Relocation
relocation_activation1 = 5000 # W/m
# Plenum parameters
initial_plenum_pressure = 1.35e6 # Pa
startup_time = 0 # s
# Physical constants
gravitational_acceleration_constant = -9.81 # m/s^2
ideal_gas_constant = 8.3143 # J/mol-K
# Numerical options
l_max_its = 50
l_tol = 8e-3
nl_max_its = 20
nl_rel_tol = 1e-4
start_time = -200 # s
n_startup_steps = 1
dtmax = 5e5 # s
dtmin = 0.1 # s
TimeStepper_dt = 2e2 # s
TimeStepper_max_function_change = 1e20
# Postprocessor parameters
burnup_scaling_factor = 950.0 # (-)
time_days_scale_factor = 1.157407407e-5 # (-)
midplane_oxide_thickness_elementid = 629
outer_midplane_clad_temperature_nodeid = 763
fuel_central_temperature_nodeid = 337
clad_elongation_nodeid = 826
fuel_elongation_nodeid = 504
upper_TC_temperature_nodeid = 633
lower_TC_temperature_nodeid = 31
[GlobalParams]
displacements = 'disp_x disp_y'
temperature = temperature
order = FIRST
family = LAGRANGE
density = ${initial_fuel_density}
initial_porosity = ${initial_fuel_porosity}
energy_per_fission = ${energy_per_fission}
volumetric_locking_correction = false
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
acceptable_multiplier = 10
[]
[Mesh]
coord_type = RZ
patch_update_strategy = auto
patch_size = 10
partitioner = centroid
centroid_partitioner_direction = y
[mesh]
type = FileMeshGenerator
file = ${rod_mesh_file}
[]
[]
[Variables]
[temperature]
initial_condition = ${initial_temperature}
[]
[]
[AuxVariables]
[fast_neutron_flux]
[]
[fast_neutron_fluence]
[]
[grain_radius]
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
initial_condition = ${initial_grain_radius}
[]
[gap_cond]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[effective_creep_strain]
block = clad
order = CONSTANT
family = MONOMIAL
[]
[oxide_thickness]
order = CONSTANT
family = MONOMIAL
[]
[]
[Functions]
[power_history]
type = PiecewiseLinear
data_file = ${power_history_data_file}
scale_factor = 1e3
format = columns
[]
[corrected_power_history]
type = ParsedFunction
symbol_names = 'rod_average_burnup power_history'
symbol_values = 'burnup_MWdkgU power_history'
expression = 'if(rod_average_burnup < 14.5, power_history, 0.98 * power_history)'
[]
[axial_peaking_factors]
type = PiecewiseBilinear
data_file = ${axial_peaking_data_file}
scale_factor = 1
axis = 1
[]
[power_correction]
type = PiecewiseBilinear
data_file = ${power_correction_data_file}
scale_factor = 1
axis = 1
[]
[corrected_axial_peaking_factors]
type = CompositeFunction
functions = 'axial_peaking_factors power_correction'
[]
[pressure_ramp]
type = PiecewiseLinear
x = ${pressure_ramp_x}
y = ${pressure_ramp_y}
[]
[coolant_inlet_temperature]
type = PiecewiseLinear
data_file = ${coolant_inlet_temperature_data_file}
scale_factor = 1
format = columns
[]
[fast_flux]
type = PiecewiseLinear
data_file = ${fast_neutron_flux_data_file}
scale_factor = 1e4
format = columns
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[pellets]
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
add_variables = true
strain = FINITE
eigenstrain_names = 'fuel_relocation_strain fuel_thermal_eigenstrain fuel_volumetric_strain'
generate_output = 'vonmises_stress hydrostatic_stress stress_xx stress_yy stress_zz'
extra_vector_tags = 'ref'
[]
[clad]
block = clad
add_variables = true
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain clad_irradiation_strain'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx strain_yy strain_zz'
extra_vector_tags = 'ref'
[]
[]
[]
[]
[Kernels]
[gravity]
type = Gravity
variable = disp_y
value = ${gravitational_acceleration_constant}
[]
[heat]
type = HeatConduction
variable = temperature
extra_vector_tags = 'ref'
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
extra_vector_tags = 'ref'
[]
[heat_source]
type = NeutronHeatSource
variable = temperature
extra_vector_tags = 'ref'
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
burnup_function = burnup
[]
[]
[Burnup]
[burnup]
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
rod_ave_lin_pow = corrected_power_history
axial_power_profile = corrected_axial_peaking_factors
num_radial = 80
num_axial = 11
a_lower = ${a_lower}
a_upper = ${a_upper}
fuel_inner_radius = ${fuel_inner_radius}
fuel_outer_radius = ${fuel_outer_radius}
fuel_volume_ratio = ${fuel_volume_ratio}
order = CONSTANT
family = MONOMIAL
RPF = RPF
isotopes = 'U235 U238 Pu239 Pu240 Pu241 Pu242'
isotope_fractions = '${isotope_fraction_U235} ${isotope_fraction_U238} ${isotope_fraction_Pu239} ${isotope_fraction_Pu240} ${isotope_fraction_Pu241} ${isotope_fraction_Pu242}'
[]
[]
[AuxKernels]
[fast_neutron_flux]
type = FastNeutronFluxAux
variable = fast_neutron_flux
block = clad
function = fast_flux
execute_on = timestep_begin
[]
[fast_neutron_fluence]
type = FastNeutronFluenceAux
variable = fast_neutron_fluence
block = clad
fast_neutron_flux = fast_neutron_flux
execute_on = timestep_begin
[]
[grain_radius]
type = GrainRadiusAux
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
variable = grain_radius
temperature = temperature
execute_on = linear
[]
[conductance]
type = MaterialRealAux
property = gap_conductance
variable = gap_cond
boundary = 10
execute_on = linear
[]
[effective_creep_strain]
type = MaterialRealAux
block = 1
property = effective_creep_strain
variable = effective_creep_strain
execute_on = 'timestep_end'
[]
[oxide]
type = MaterialRealAux
property = oxide_scale_thickness
variable = oxide_thickness
boundary = 2
[]
[]
[Contact]
[pellet_clad_mechanical]
primary = 5
secondary = 10
formulation = penalty
model = frictionless
normalize_penalty = true
penalty = ${contact_penalty}
normal_smoothing_distance = ${normal_smoothing_distance}
[]
[]
[ThermalContact]
[thermal_contact]
type = GasGapHeatTransfer
variable = temperature
primary = 5
secondary = 10
initial_moles = initial_moles
gas_released = fission_gas_released
contact_pressure = contact_pressure
quadrature = true
roughness_primary = ${roughness_primary}
roughness_secondary = ${roughness_secondary}
roughness_coef = ${roughness_coef}
[]
[]
[PlenumTemperature]
[plenum_temp]
boundary = 5
inner_surfaces = '5'
outer_surfaces = '10'
temperature = temperature
[]
[]
[BCs]
[no_x_all]
type = DirichletBC
variable = disp_x
boundary = 12
value = 0.0
[]
[no_y_clad_bottom]
type = DirichletBC
variable = disp_y
boundary = '1'
value = 0.0
[]
[no_y_fuel_bottom]
type = DirichletBC
variable = disp_y
boundary = '20'
value = 0.0
[]
[Pressure]
[coolantPressure]
boundary = '1 2 3'
factor = ${pressure_ramp_factor}
function = pressure_ramp
[]
[]
[PlenumPressure]
[plenumPressure]
boundary = '9'
initial_pressure = ${initial_plenum_pressure}
startup_time = ${startup_time}
R = ${ideal_gas_constant}
output_initial_moles = initial_moles
temperature = plenum_temp
volume = gas_volume
material_input = fission_gas_released
output = plenum_pressure
[]
[]
[]
[CoolantChannel]
[convective_clad_surface]
boundary = '1 2 3'
variable = temperature
inlet_temperature = coolant_inlet_temperature
inlet_pressure = ${inlet_pressure}
inlet_massflux = ${inlet_massflux}
rod_diameter = ${rod_diameter}
rod_pitch = ${rod_pitch}
htc_correlation_type = ${htc_correlation_type}
compute_enthalpy = true
linear_heat_rate = corrected_power_history
axial_power_profile = corrected_axial_peaking_factors
oxide_thickness = oxide_thickness
[]
[]
[Materials]
[fuel_thermal]
type = UO2Thermal
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
thermal_conductivity_model = HALDEN #NFIR
temperature = temperature
burnup_function = burnup
[]
[fuel_volumetric_swelling]
type = UO2VolumetricSwellingEigenstrain
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
burnup_function = burnup
total_densification = ${total_densification}
initial_fuel_density = ${initial_fuel_density}
gas_swelling_model_type = SIFGRS
eigenstrain_name = fuel_volumetric_strain
[]
[fuel_relocation]
type = UO2RelocationEigenstrain
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
relocation_model = ESCORE_modified
burnup_function = burnup
diameter = ${fuel_diameter}
diametral_gap = ${diametral_gap}
rod_ave_lin_pow = corrected_power_history
axial_power_profile = corrected_axial_peaking_factors
relocation_activation1 = ${relocation_activation1}
eigenstrain_name = fuel_relocation_strain
[]
[fuel_thermal_expansion]
type = UO2ThermalExpansionMATPROEigenstrain
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
stress_free_temperature = ${stress_free_temperature}
eigenstrain_name = fuel_thermal_eigenstrain
[]
[fuel_elasticity_tensor]
type = UO2IsotropicDamageElasticityTensor
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
rod_ave_lin_pow = corrected_power_history
fragmentation_model = BARANI
[]
[fuel_stress]
type = ComputeMultipleInelasticStress
inelastic_models = 'fuel_creep'
tangent_operator = elastic
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
[]
[fuel_creep]
type = UO2CreepUpdate
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
temperature = temperature
fission_rate = fission_rate
initial_grain_radius = ${initial_grain_radius}
oxygen_to_metal_ratio = ${oxygen_to_metal_ratio}
[]
[fuel_density]
type = Density
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
[]
[clad_thermal]
type = ZryThermal
block = clad
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = clad
fast_neutron_fluence = fast_neutron_fluence
[]
[clad_stress]
type = ComputeMultipleInelasticStress
tangent_operator = elastic
inelastic_models = 'clad_zrycreep'
block = clad
[]
[clad_zrycreep]
type = ZryCreepLimbackHoppeUpdate
block = clad
fast_neutron_flux = fast_neutron_flux
fast_neutron_fluence = fast_neutron_fluence
model_primary_creep = true
model_thermal_creep = true
model_irradiation_creep = true
[]
[clad_thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = clad
stress_free_temperature = ${stress_free_temperature}
eigenstrain_name = clad_thermal_eigenstrain
[]
[clad_irradiation_growth]
type = ZryIrradiationGrowthEigenstrain
block = clad
fast_neutron_fluence = fast_neutron_fluence
eigenstrain_name = clad_irradiation_strain
[]
[clad_density]
type = Density
block = clad
density = ${cladding_density}
[]
[clad_oxidation]
type = ZryOxidation
boundary = 2
clad_inner_radius = ${clad_inner_radius}
clad_outer_radius = ${clad_outer_radius}
use_coolant_channel = true
fast_neutron_flux = fast_neutron_flux
[]
[fission_gas_release]
type = UO2Sifgrs
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
temperature = temperature
burnup_function = burnup
grain_radius = grain_radius
gbs_model = true
transient_option = MICROCRACKING_BURNUP
ig_bubble_model = NUCLEATION_RESOLUTION
diff_coeff_option = TURNBULL_D1_4D2_4D3
doping_type = CR2O3_DOPED
cr_doped_option = BEST_ESTIMATE_1773
[]
[]
[Preconditioning]
[SMP]
type = SMP
full = true
[]
[]
[Dampers]
[BoundingValueNodalDamper]
type = MaxIncrement
max_increment = 20
variable = temperature
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
l_max_its = ${l_max_its}
l_tol = ${l_tol}
nl_max_its = ${nl_max_its}
nl_rel_tol = ${nl_rel_tol}
nl_abs_tol = ${nl_abs_tol}
start_time = ${start_time}
n_startup_steps = ${n_startup_steps}
end_time = ${end_time}
dtmax = ${dtmax}
dtmin = ${dtmin}
[TimeStepper]
type = IterationAdaptiveDT
dt = ${TimeStepper_dt}
timestep_limiting_function = power_history
max_function_change = ${TimeStepper_max_function_change}
force_step_every_function_point = true
[]
[Quadrature]
order = FIFTH
side_order = SEVENTH
[]
[]
[Postprocessors]
[alhr_input]
type = FunctionValuePostprocessor
function = corrected_power_history
execute_on = 'initial timestep_end'
[]
[temperature_fuel_max]
type = NodalExtremeValue
variable = temperature
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
execute_on = 'initial timestep_end'
[]
[burnup]
type = RodAverageBurnup
burnup_function = burnup
[]
[burnup_MWdkgU]
type = ScalePostprocessor
value = burnup
scaling_factor = ${burnup_scaling_factor}
[]
[time_days]
type = FunctionValuePostprocessor
function = t
scale_factor = ${time_days_scale_factor}
[]
[temperature_clad_max]
type = NodalExtremeValue
block = clad
value_type = max
variable = temperature
execute_on = 'initial timestep_end'
[]
[oxide_thickness_midplane]
type = ElementalVariableValue
elementid = ${midplane_oxide_thickness_elementid}
variable = oxide_thickness
execute_on = 'initial timestep_end'
[]
[strain_clad_hoop_max]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = clad
[]
[temperature_clad_outer_midplane]
type = NodalVariableValue
nodeid = ${outer_midplane_clad_temperature_nodeid}
variable = temperature
execute_on = 'initial timestep_end'
[]
[temperature_fuel_central]
type = NodalVariableValue
variable = temperature
nodeid = ${fuel_central_temperature_nodeid}
execute_on = 'initial timestep_end'
[]
[gas_volume]
type = InternalVolume
boundary = '9'
execute_on = 'initial linear'
[]
[fission_gas_produced]
type = ElementIntegralFisGasGeneratedSifgrs
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
execute_on = linear
[]
[fission_gas_released]
type = ElementIntegralFisGasReleasedSifgrs
block = 'pellet_type_1 pellet_type_2 pellet_type_3'
execute_on = linear
[]
[fgr_percent]
type = FGRPercent
fission_gas_released = fission_gas_released
fission_gas_generated = fission_gas_produced
execute_on = linear
[]
[clad_elongation]
type = NodalVariableValue
variable = disp_y
nodeid = ${clad_elongation_nodeid}
[]
[fuel_elongation]
type = NodalVariableValue
variable = disp_y
nodeid = ${fuel_elongation_nodeid}
[]
[upper_TC_temperature]
type = NodalVariableValue
variable = temperature
nodeid = ${upper_TC_temperature_nodeid}
[]
[lower_TC_temperature]
type = NodalVariableValue
variable = temperature
nodeid = ${lower_TC_temperature_nodeid}
[]
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
color = false
[console]
type = Console
max_rows = 15
[]
[chkfile]
type = CSV
file_base = '${id}_chkfile'
show = 'lower_TC_temperature upper_TC_temperature fgr_percent plenum_pressure strain_clad_hoop_max'
execute_on = 'FINAL'
[]
[csv]
type = CSV
file_base = '${id}_csv'
[]
[exodus]
type = Exodus
file_base = '${id}_exodus'
[]
[]
(assessment/LWR/validation/LOCA_Hardy_cladding_test/analysis/2pt1MPa/25C_sec/25C_sec_Hardy_Tube_Test_2pt1MPa.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
volumetric_locking_correction = false
displacements = 'disp_x disp_y'
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
group_variables = 'disp_x disp_y'
[]
[Mesh]
coord_type = RZ
patch_size = 10
patch_update_strategy = iteration
partitioner = centroid
centroid_partitioner_direction = y
[gen]
type = FuelPinMeshGenerator
include_fuel = false
include_clad = true
pellet_outer_radius = 0.0072527
clad_gap_width = 0.0
clad_top_gap_height = 0.0
clad_bot_gap_height = 0.0
clad_thickness = 0.38e-3
pellet_height = 0.5
pellet_quantity = 1
clad_mesh_density = customize
nx_c = 2
ny_c = 50
elem_type = QUAD8
[]
[]
[Variables]
[temperature]
initial_condition = 600.0
[]
[]
[AuxVariables]
[creep_rate_aux]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[total_hoop_strain]
order = CONSTANT
family = MONOMIAL
[]
[burst_stress]
order = CONSTANT
family = MONOMIAL
[]
[burst]
order = CONSTANT
family = MONOMIAL
[]
[]
[Functions]
[pressure_function]
type = PiecewiseLinear
x = '0 40'
y = '1 1'
[]
[temp_function]
type = PiecewiseLinear
y = '600 1600'
[]
[temperature_profile]
type = PiecewiseBilinear
y = '0 40'
x = '0 0.25224 0.50448'
z = '0.995 1.01 0.995 0.995 1.01 0.995'
axis = 1
[]
[inner_temperature]
type = CompositeFunction
functions = 'temp_function temperature_profile'
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[clad]
block = clad
add_variables = true
strain = FINITE
decomposition_method = EigenSolution
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz elastic_strain_xx elastic_strain_yy elastic_strain_zz
creep_strain_xx creep_strain_yy creep_strain_zz hoop_stress'
extra_vector_tags = 'ref'
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
extra_vector_tags = 'ref'
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
extra_vector_tags = 'ref'
[]
[]
[AuxKernels]
[creep_rate_aux]
type = MaterialRealAux
variable = creep_rate_aux
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[creep_rate]
type = MaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[total_hoop_strain]
type = RankTwoAux
rank_two_tensor = total_strain
variable = total_hoop_strain
index_i = 2
index_j = 2
execute_on = timestep_end
block = clad
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = clad_outside_right
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = clad_outside_right
execute_on = timestep_end
[]
[]
[BCs]
[Pressure]
[outer_surface]
boundary = 'clad_outside_bottom clad_outside_right clad_outside_top'
factor = 0.0
function = pressure_function
[]
[inner_surface]
boundary = 'clad_inside_right clad_inside_bottom clad_inside_top'
function = pressure_function
[]
[]
[u_bottom_fix]
type = DirichletBC
variable = disp_y
boundary = 1001
value = 0.0
[]
[x_fix]
type = DirichletBC
variable = disp_x
boundary = centerline
value = 0.0
[]
[temp_bc]
type = FunctionDirichletBC
function = inner_temperature
variable = temperature
boundary = 'clad_inside_bottom clad_inside_right clad_inside_top'
[]
[]
[Materials]
[clad_thermal]
type = ZryThermal
block = clad
zry_thermal_properties_model = MATPRO
temperature = temperature
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = clad
matpro_youngs_modulus = true
matpro_poissons_ratio = true
temperature = temperature
[]
[clad_stress]
type = ComputeMultipleInelasticStress
inelastic_models = 'clad_zrycreep'
block = clad
tangent_operator = nonlinear
[]
[clad_zrycreep]
type = ZryCreepLOCAUpdate
block = clad
temperature = temperature
model_irradiation_creep = false
model_primary_creep = true
model_thermal_creep = true
temperature_loca_creep_begin = 840 # values from the report
temperature_standard_thermal_creep_end = 975
[]
[thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = clad
temperature = temperature
stress_free_temperature = 600.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[clad_density]
type = Density
block = clad
density = 6550.0
[]
[phase]
type = ZrPhase
block = clad
temperature = temperature
numerical_method = 2
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = clad_outside_right
failure_criterion = combined_overstress_and_overstrain
hoop_stress = hoop_stress
hoop_creep_strain = creep_strain_zz
effective_strain_rate_creep = creep_rate_aux
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.0e-5
nl_abs_tol = 1.0e-8
start_time = 0
n_startup_steps = 1
end_time = 40
dtmax = 1
dtmin = 0.0000001
[TimeStepper]
type = IterationAdaptiveDT
timestep_limiting_postprocessor = material_timestep
dt = 1.0
[]
[]
[Postprocessors]
[ave_clad_temp]
type = SideAverageValue
boundary = clad_outside_right
variable = temperature
[]
[gas_volume]
type = InternalVolume
boundary = all_clad_interior
execute_on = 'initial linear'
[]
[max_clad_temp]
type = NodalExtremeValue
block = clad
value_type = max
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = clad
[]
[max_hoop_stress]
type = ElementExtremeValue
block = clad
value_type = max
variable = hoop_stress
[]
[vonmises_stress_clad]
type = ElementAverageValue
block = clad
variable = vonmises_stress
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = total_hoop_strain
[]
[max_disp_x]
type = NodalExtremeValue
block = clad
value_type = max
variable = disp_x
[]
[min_burst_stress]
type = ElementExtremeValue
block = clad
value_type = min
variable = burst_stress
[]
[burst]
type = ElementExtremeValue
block = clad
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = clad
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
[]
[PerformanceMetricOutputs]
[]
[Outputs]
color = false
perf_graph = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[csv]
type = CSV
[]
[chkfile]
type = CSV
show = 'max_disp_x max_hoop_stress vonmises_stress_clad'
execute_on = 'FINAL'
[]
[]
[UserObjects]
[terminator1]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '5'
include_fuel = false
[]
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-24/puzry-24_aniso.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-24.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 6000. '
y = '1.e+05 1.e+05 9.05e+06' # Linear increase at 0.0179 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 6000. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
# Circumferential steady-state creep test and analysis of Zircaloy-4 fuel cladding
# Nuclear Engineering and Design, 53, 2312-2322 (2021)
[F]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.738 0.738 0.57'
[]
[G]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.174 0.174 0.45'
[]
[H]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.588 0.588 0.48'
[]
[L]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[M]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[N]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = TaylorExpansion
use_automatic_differentiation = true
[]
[]
[]
[]
[Kernels]
[heat]
type = ADHeatConduction
variable = temperature
[]
[heat_ie]
type = ADHeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = ADMaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = ADMaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = ADMaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = ADMaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = ADMaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = ADFunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = ADDirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = ADDirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ADZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1.e+11
poissons_ratio = 0.3
block = 1
[]
[hill_constants]
type = ADHillConstants
hill_constants = "0.738 0.174 0.588 1.0 1.0 1.0"
function_names = "F G H L M N"
temperature = temperature
[]
[creep_update]
type = ADZryAnisoCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 1.5e-05
temperature = temperature
temperature_standard_thermal_creep_end = 700
temperature_loca_creep_begin = 900.
fract_beta_phase_name = 'fract_beta_phase'
max_integration_error = 1000000.0
absolute_tolerance = 1e-13
relative_tolerance = 1e-11
[]
[creep]
type = ADComputeMultipleInelasticStress
block = 1
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ADZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = ADDensity
block = 1
[]
[phase]
type = ADZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ADZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = NEWTON
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-07
start_time = 0.
n_startup_steps = 1
end_time = 2500.
dtmax = 1.
dtmin = 1.0e-9
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-24_aniso_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/LOCA_Hardy_cladding_test/analysis/3pt8MPa/25C_sec/25C_sec_Hardy_Tube_Test_3pt8MPa.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
volumetric_locking_correction = false
displacements = 'disp_x disp_y'
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
group_variables = 'disp_x disp_y'
[]
[Mesh]
coord_type = RZ
patch_size = 10
patch_update_strategy = iteration
partitioner = centroid
centroid_partitioner_direction = y
[gen]
type = FuelPinMeshGenerator
include_fuel = false
include_clad = true
pellet_outer_radius = 0.0072527
clad_gap_width = 0.0
clad_top_gap_height = 0.0
clad_bot_gap_height = 0.0
clad_thickness = 0.38e-3
pellet_height = 0.5
pellet_quantity = 1
clad_mesh_density = customize
nx_c = 2
ny_c = 50
elem_type = QUAD8
[]
[]
[Variables]
[temperature]
initial_condition = 600.0
[]
[]
[AuxVariables]
[creep_rate_aux]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[total_hoop_strain]
order = CONSTANT
family = MONOMIAL
[]
[burst_stress]
order = CONSTANT
family = MONOMIAL
[]
[burst]
order = CONSTANT
family = MONOMIAL
[]
[]
[Functions]
[pressure_function]
type = PiecewiseLinear
x = '0 40'
y = '1 1'
[]
[temp_function]
type = PiecewiseLinear
y = '600 1600'
[]
[temperature_profile]
type = PiecewiseBilinear
y = '0 40'
x = '0 0.25224 0.50448'
z = '0.995 1.01 0.995 0.995 1.01 0.995'
axis = 1
[]
[inner_temperature]
type = CompositeFunction
functions = 'temp_function temperature_profile'
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[clad]
block = clad
add_variables = true
strain = FINITE
decomposition_method = EigenSolution
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz elastic_strain_xx elastic_strain_yy elastic_strain_zz
creep_strain_xx creep_strain_yy creep_strain_zz hoop_stress'
extra_vector_tags = 'ref'
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
extra_vector_tags = 'ref'
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
extra_vector_tags = 'ref'
[]
[]
[AuxKernels]
[creep_rate_aux]
type = MaterialRealAux
variable = creep_rate_aux
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[creep_rate]
type = MaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[total_hoop_strain]
type = RankTwoAux
rank_two_tensor = total_strain
variable = total_hoop_strain
index_i = 2
index_j = 2
execute_on = timestep_end
block = clad
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = clad_outside_right
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = clad_outside_right
execute_on = timestep_end
[]
[]
[BCs]
[Pressure]
[outer_surface]
boundary = 'clad_outside_bottom clad_outside_right clad_outside_top'
factor = 0.0
function = pressure_function
[]
[inner_surface]
boundary = 'clad_inside_right clad_inside_bottom clad_inside_top'
function = pressure_function
[]
[]
[u_bottom_fix]
type = DirichletBC
variable = disp_y
boundary = 1001
value = 0.0
[]
[x_fix]
type = DirichletBC
variable = disp_x
boundary = centerline
value = 0.0
[]
[temp_bc]
type = FunctionDirichletBC
function = inner_temperature
variable = temperature
boundary = 'clad_inside_bottom clad_inside_right clad_inside_top'
[]
[]
[Materials]
[clad_thermal]
type = ZryThermal
block = clad
zry_thermal_properties_model = MATPRO
temperature = temperature
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = clad
matpro_youngs_modulus = true
matpro_poissons_ratio = true
temperature = temperature
[]
[clad_stress]
type = ComputeMultipleInelasticStress
inelastic_models = 'clad_zrycreep'
block = clad
tangent_operator = nonlinear
[]
[clad_zrycreep]
type = ZryCreepLOCAUpdate
block = clad
temperature = temperature
model_irradiation_creep = false
model_primary_creep = true
model_thermal_creep = true
temperature_loca_creep_begin = 840 # values from the report
temperature_standard_thermal_creep_end = 975
[]
[thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = clad
temperature = temperature
stress_free_temperature = 600.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[clad_density]
type = Density
block = clad
density = 6550.0
[]
[phase]
type = ZrPhase
block = clad
temperature = temperature
numerical_method = 2
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = clad_outside_right
failure_criterion = combined_overstress_and_overstrain
hoop_stress = hoop_stress
hoop_creep_strain = creep_strain_zz
effective_strain_rate_creep = creep_rate_aux
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.0e-5
nl_abs_tol = 1.0e-8
start_time = 0
n_startup_steps = 1
end_time = 40
dtmax = 1
dtmin = 0.0000001
[TimeStepper]
type = IterationAdaptiveDT
timestep_limiting_postprocessor = material_timestep
dt = 1.0
[]
[]
[Postprocessors]
[ave_clad_temp]
type = SideAverageValue
boundary = clad_outside_right
variable = temperature
[]
[gas_volume]
type = InternalVolume
boundary = all_clad_interior
execute_on = 'initial linear'
[]
[max_clad_temp]
type = NodalExtremeValue
block = clad
value_type = max
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = clad
[]
[max_hoop_stress]
type = ElementExtremeValue
block = clad
value_type = max
variable = hoop_stress
[]
[vonmises_stress_clad]
type = ElementAverageValue
block = clad
variable = vonmises_stress
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = total_hoop_strain
[]
[max_disp_x]
type = NodalExtremeValue
block = clad
value_type = max
variable = disp_x
[]
[min_burst_stress]
type = ElementExtremeValue
block = clad
value_type = min
variable = burst_stress
[]
[burst]
type = ElementExtremeValue
block = clad
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = clad
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
[]
[PerformanceMetricOutputs]
[]
[Outputs]
color = false
perf_graph = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[csv]
type = CSV
[]
[chkfile]
type = CSV
show = 'max_disp_x max_hoop_stress vonmises_stress_clad'
execute_on = 'FINAL'
[]
[]
[UserObjects]
[terminator1]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '5'
include_fuel = false
[]
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-01/puzry-01_aniso.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-01.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 2000. '
y = '1.e+05 1.e+05 7.4e+05' # Linear increase at 0.064 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 2000. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
# Circumferential steady-state creep test and analysis of Zircaloy-4 fuel cladding
# Nuclear Engineering and Design, 53, 2312-2322 (2021)
[F]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.738 0.738 0.57'
[]
[G]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.174 0.174 0.45'
[]
[H]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.588 0.588 0.48'
[]
[L]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[M]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[N]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = TaylorExpansion
use_automatic_differentiation = true
[]
[]
[]
[]
[Kernels]
[heat]
type = ADHeatConduction
variable = temperature
[]
[heat_ie]
type = ADHeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = ADMaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = ADMaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = ADMaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = ADMaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = ADMaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = ADFunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = ADDirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = ADDirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ADZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1.e+11
poissons_ratio = 0.3
block = 1
[]
[hill_constants]
type = ADHillConstants
hill_constants = "0.738 0.174 0.588 1.0 1.0 1.0"
function_names = "F G H L M N"
temperature = temperature
[]
[creep_update]
type = ADZryAnisoCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 1.5e-05
temperature = temperature
temperature_standard_thermal_creep_end = 700
temperature_loca_creep_begin = 900.
fract_beta_phase_name = 'fract_beta_phase'
max_integration_error = 1000000.0
absolute_tolerance = 1e-07
relative_tolerance = 1e-07
[]
[creep]
type = ADComputeMultipleInelasticStress
block = 1
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ADZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = ADDensity
block = 1
[]
[phase]
type = ADZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ADZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = NEWTON
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0.
n_startup_steps = 1
end_time = 2500.
dtmax = 1.
dtmin = 1.0e-9
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-01_aniso_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-27/puzry-27_aniso.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-27.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 3000. '
y = '1.e+05 1.e+05 5.06e+06' # Linear increase at 0.0248 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 3000. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
# Circumferential steady-state creep test and analysis of Zircaloy-4 fuel cladding
# Nuclear Engineering and Design, 53, 2312-2322 (2021)
[F]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.738 0.738 0.57'
[]
[G]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.174 0.174 0.45'
[]
[H]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.588 0.588 0.48'
[]
[L]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[M]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[N]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = TaylorExpansion
use_automatic_differentiation = true
[]
[]
[]
[]
[Kernels]
[heat]
type = ADHeatConduction
variable = temperature
[]
[heat_ie]
type = ADHeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = ADMaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = ADMaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = ADMaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = ADMaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = ADMaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = ADFunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = ADDirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = ADDirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ADZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1.e+11
poissons_ratio = 0.3
block = 1
[]
[hill_constants]
type = ADHillConstants
hill_constants = "0.738 0.174 0.588 1.0 1.0 1.0"
function_names = "F G H L M N"
temperature = temperature
[]
[creep_update]
type = ADZryAnisoCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 1.5e-05
temperature = temperature
temperature_standard_thermal_creep_end = 700
temperature_loca_creep_begin = 900.
fract_beta_phase_name = 'fract_beta_phase'
max_integration_error = 1000000.0
absolute_tolerance = 1e-13
relative_tolerance = 1e-11
[]
[creep]
type = ADComputeMultipleInelasticStress
block = 1
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ADZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = ADDensity
block = 1
[]
[phase]
type = ADZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ADZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = NEWTON
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-07
start_time = 0.
n_startup_steps = 1
end_time = 2500.
dtmax = 1.
dtmin = 1.0e-9
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-27_aniso_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/LOCA_REBEKA_cladding_burst_tests/analysis/rebeka_2d_10MPa/rebeka_singlerod_2d_10MPa.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
order = SECOND
family = LAGRANGE
displacements = 'disp_x disp_y'
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = rebeka_singlerod.e
[]
[]
[Variables]
[temperature]
initial_condition = 573.0
[]
[]
[Functions]
[temperature_func]
type = PiecewiseLinear
x = '0. 700. '
y = '573. 1273.' # From 300 to 1000 C at 1 K/s
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 700. '
y = '1.e+07 1.e+07' # 100 bar
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 700. '
y = '1.e+05 1.e+05' # atmospheric pressure
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[clad]
block = cladding
add_variables = true
strain = FINITE
decomposition_method = EigenSolution
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz hoop_stress'
[]
[]
[AuxVariables]
[creep_rate_aux]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[scale_thickness]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfract_total]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfgain_total]
order = CONSTANT
family = MONOMIAL
[]
[burst_stress]
order = CONSTANT
family = MONOMIAL
[]
[burst]
order = CONSTANT
family = MONOMIAL
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate_aux]
type = MaterialRealAux
variable = creep_rate_aux
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[scl_thickness]
type = MaterialRealAux
variable = scale_thickness
property = oxide_scale_thickness
boundary = 2
[]
[ofract_total]
type = MaterialRealAux
variable = oxywtfract_total
property = current_oxygen_weight_frac_total
boundary = 2
[]
[ofgain_total]
type = MaterialRealAux
boundary = 2
variable = oxywtfgain_total
property = oxygen_weight_frac_gained_total
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = 2
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = 2
execute_on = timestep_end
[]
[]
[BCs]
[inner_temperature]
type = REBEKADirichletBC
variable = temperature
function_tempm = temperature_func
minimum_temperature = 573.
translation = 0.1625
boundary = 4
[]
[no_y_midsection]
type = DirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply steam pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 101 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[CoolantChannel]
[convective_clad_surface]
boundary = 2
variable = temperature
inlet_temperature = 473.
inlet_pressure = 1.e+05
inlet_massflux = 1.0 # kg/m^2-sec # almost stagnant steam
rod_diameter = 10.75e-03
rod_pitch = 1.26e-02 # default
oxide_thickness = scale_thickness
[]
[]
[Materials]
[thermal]
type = ZryThermal
block = cladding
temperature = temperature
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = cladding
matpro_youngs_modulus = false
matpro_poissons_ratio = false
[]
[clad_stress]
type = ComputeMultipleInelasticStress
tangent_operator = elastic
inelastic_models = 'clad_zrycreep'
block = cladding
[]
[clad_zrycreep]
type = ZryCreepLOCAUpdate
block = cladding
temperature = temperature
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
temperature_loca_creep_begin = 501
temperature_standard_thermal_creep_end = 500
[]
[thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = cladding
temperature = temperature
stress_free_temperature = 573.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[density]
type = Density
block = cladding
[]
[phase]
type = ZrPhase
block = cladding
temperature = temperature
numerical_method = 2
[]
[oxidation]
type = ZryOxidation
boundary = 2
temperature = temperature
clad_inner_radius = 0.00465
clad_outer_radius = 0.005375
normal_operating_temperature_model = epri_kwu_ce
high_temperature_model = leistikow
use_coolant_channel = true
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = 2
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate_aux
temperature = temperature
fraction_beta_phase = fract_beta_phase
fraction_oxygen_gain = oxywtfgain_total
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-06
nl_abs_tol = 1.e-08
start_time = 0
n_startup_steps = 1
end_time = 700.
dtmax = 1.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[Postprocessors]
[ave_clad_exterior_temp]
type = SideAverageValue
boundary = 2
variable = temperature
[]
[max_clad_temp]
type = NodalExtremeValue
block = cladding
value_type = max
variable = temperature
[]
[min_clad_temp]
type = NodalExtremeValue
block = cladding
value_type = min
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = cladding
[]
[max_oxygen_fract]
type = ElementExtremeValue
block = cladding
value_type = max
variable = oxywtfract_total
[]
[max_betaph_fract]
type = ElementExtremeValue
block = cladding
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
block = cladding
value_type = max
variable = creep_rate_aux
[]
[max_creep_strain_mag]
type = ElementExtremeValue
block = cladding
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
block = cladding
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
block = cladding
value_type = max
variable = hoop_stress
[]
[vonmises_stress_clad]
type = ElementAverageValue
block = cladding
variable = vonmises_stress
[]
[min_burst_stress]
type = ElementExtremeValue
block = cladding
value_type = min
variable = burst_stress
[]
[burst]
type = ElementExtremeValue
block = cladding
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = cladding
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[top_disp_r_clad] # this is mid height
type = NodalVariableValue
variable = disp_x
nodeid = 0 #coords (0.005375, 0.1625)
[]
[top_disp_r_clad_slice] # this is mid height matched to the 1.5d
type = NodalVariableValue
variable = disp_x
nodeid = 3 #coords (0.005375, 0.1625)
[]
[top_disp_z_clad]
type = NodalVariableValue
variable = disp_y
nodeid = 0 #coords (0.005375, 0.1625)
[]
[stress_xx] # stess in the top Element
type = ElementalVariableValue
variable = stress_xx
elementid = 0
[]
[stress_yy] # stess in the top Element
type = ElementalVariableValue
variable = stress_yy
elementid = 0
[]
[stress_zz] # stess in the top Element
type = ElementalVariableValue
variable = stress_zz
elementid = 0
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = cladding
plenum_boundary_name = 4
external_clad_boundary_name = 2
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = rebeka_2d_10MPa_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
(assessment/LWR/validation/LOCA_Hardy_cladding_test/analysis/base_input/Hardy_Tube_Test.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
volumetric_locking_correction = false
displacements = 'disp_x disp_y'
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
group_variables = 'disp_x disp_y'
[]
[Mesh]
coord_type = RZ
patch_size = 10
patch_update_strategy = iteration
partitioner = centroid
centroid_partitioner_direction = y
[gen]
type = FuelPinMeshGenerator
include_fuel = false
include_clad = true
pellet_outer_radius = 0.0072527
clad_gap_width = 0.0
clad_top_gap_height = 0.0
clad_bot_gap_height = 0.0
clad_thickness = 0.38e-3
pellet_height = 0.5
pellet_quantity = 1
clad_mesh_density = customize
nx_c = 2
ny_c = 50
elem_type = QUAD8
[]
[]
[Variables]
[temperature]
initial_condition = 600.0
[]
[]
[AuxVariables]
[creep_rate_aux]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[total_hoop_strain]
order = CONSTANT
family = MONOMIAL
[]
[burst_stress]
order = CONSTANT
family = MONOMIAL
[]
[burst]
order = CONSTANT
family = MONOMIAL
[]
[]
[Functions]
[pressure_function]
type = PiecewiseLinear
x = '0 40'
y = '1 1'
[]
[temp_function]
type = PiecewiseLinear
y = '600 1600'
[]
[temperature_profile]
type = PiecewiseBilinear
y = '0 40'
x = '0 0.25224 0.50448'
z = '0.995 1.01 0.995 0.995 1.01 0.995'
axis = 1
[]
[inner_temperature]
type = CompositeFunction
functions = 'temp_function temperature_profile'
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[clad]
block = clad
add_variables = true
strain = FINITE
decomposition_method = EigenSolution
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz elastic_strain_xx elastic_strain_yy elastic_strain_zz
creep_strain_xx creep_strain_yy creep_strain_zz hoop_stress'
extra_vector_tags = 'ref'
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
extra_vector_tags = 'ref'
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
extra_vector_tags = 'ref'
[]
[]
[AuxKernels]
[creep_rate_aux]
type = MaterialRealAux
variable = creep_rate_aux
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[creep_rate]
type = MaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[total_hoop_strain]
type = RankTwoAux
rank_two_tensor = total_strain
variable = total_hoop_strain
index_i = 2
index_j = 2
execute_on = timestep_end
block = clad
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = clad_outside_right
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = clad_outside_right
execute_on = timestep_end
[]
[]
[BCs]
[Pressure]
[outer_surface]
boundary = 'clad_outside_bottom clad_outside_right clad_outside_top'
factor = 0.0
function = pressure_function
[]
[inner_surface]
boundary = 'clad_inside_right clad_inside_bottom clad_inside_top'
function = pressure_function
[]
[]
[u_bottom_fix]
type = DirichletBC
variable = disp_y
boundary = 1001
value = 0.0
[]
[x_fix]
type = DirichletBC
variable = disp_x
boundary = centerline
value = 0.0
[]
[temp_bc]
type = FunctionDirichletBC
function = inner_temperature
variable = temperature
boundary = 'clad_inside_bottom clad_inside_right clad_inside_top'
[]
[]
[Materials]
[clad_thermal]
type = ZryThermal
block = clad
zry_thermal_properties_model = MATPRO
temperature = temperature
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = clad
matpro_youngs_modulus = true
matpro_poissons_ratio = true
temperature = temperature
[]
[clad_stress]
type = ComputeMultipleInelasticStress
inelastic_models = 'clad_zrycreep'
block = clad
tangent_operator = nonlinear
[]
[clad_zrycreep]
type = ZryCreepLOCAUpdate
block = clad
temperature = temperature
model_irradiation_creep = false
model_primary_creep = true
model_thermal_creep = true
temperature_loca_creep_begin = 840 # values from the report
temperature_standard_thermal_creep_end = 975
[]
[thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = clad
temperature = temperature
stress_free_temperature = 600.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[clad_density]
type = Density
block = clad
density = 6550.0
[]
[phase]
type = ZrPhase
block = clad
temperature = temperature
numerical_method = 2
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = clad_outside_right
failure_criterion = combined_overstress_and_overstrain
hoop_stress = hoop_stress
hoop_creep_strain = creep_strain_zz
effective_strain_rate_creep = creep_rate_aux
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.0e-5
nl_abs_tol = 1.0e-8
start_time = 0
n_startup_steps = 1
end_time = 40
dtmax = 1
dtmin = 0.0000001
[TimeStepper]
type = IterationAdaptiveDT
timestep_limiting_postprocessor = material_timestep
dt = 1.0
[]
[]
[Postprocessors]
[ave_clad_temp]
type = SideAverageValue
boundary = clad_outside_right
variable = temperature
[]
[gas_volume]
type = InternalVolume
boundary = all_clad_interior
execute_on = 'initial linear'
[]
[max_clad_temp]
type = NodalExtremeValue
block = clad
value_type = max
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = clad
[]
[max_hoop_stress]
type = ElementExtremeValue
block = clad
value_type = max
variable = hoop_stress
[]
[vonmises_stress_clad]
type = ElementAverageValue
block = clad
variable = vonmises_stress
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = total_hoop_strain
[]
[max_disp_x]
type = NodalExtremeValue
block = clad
value_type = max
variable = disp_x
[]
[min_burst_stress]
type = ElementExtremeValue
block = clad
value_type = min
variable = burst_stress
[]
[burst]
type = ElementExtremeValue
block = clad
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = clad
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
[]
[PerformanceMetricOutputs]
[]
[Outputs]
color = false
perf_graph = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[csv]
type = CSV
[]
[chkfile]
type = CSV
show = 'max_disp_x max_hoop_stress vonmises_stress_clad'
execute_on = 'FINAL'
[]
[]
[UserObjects]
[terminator1]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '5'
include_fuel = false
[]
[]
(test/tests/zry_oxidation_cladding/adZryoxidation.i)
# This test demonstrates the usage of the model for cladding oxidation from
# normal operating to high temperature (accident) conditions, through the
# epri_kwu_ce, Leistikow, and Prater relations.
#
# The purpose of this input is to be a control for the FuelPinGeometry version
# to compare against and confirm the error checking through cli-args.
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Mesh]
coord_type = RZ
[smeared_pellet_mesh]
type = FuelPinMeshGenerator
include_fuel = false
pellet_quantity = 1
pellet_height = 0.011143
pellet_outer_radius = 4.57e-3
clad_mesh_density = coarse
clad_gap_width = 70.0e-6
clad_thickness = 0.735e-3
clad_bot_gap_height = 1.0e-3
bottom_clad_height = 2.5e-3
top_clad_height = 2.5e-3
clad_top_gap_height = 5.0e-3
elem_type = QUAD4
[]
patch_size = 10
patch_update_strategy = iteration
partitioner = centroid
centroid_partitioner_direction = y
[]
[Functions]
[Temp_func]
type = PiecewiseLinear
x = '0.0 100000000.0 100000010.0 100000100.0 100000110.0 100000200.0 100000210.0 100000300.0'
y = '600.0 600.0 1100.0 1100.0 1850.0 1850.0 1950.0 1950.0 '
[]
[FNFlux_func]
type = PiecewiseLinear
x = '0.0 100000300.0'
y = '1.0e+17 1.0e+17 '
[]
[]
[Variables]
[temp]
order = FIRST
family = LAGRANGE
initial_condition = 600.0
[]
[disp_x]
order = FIRST
family = LAGRANGE
[]
[disp_y]
order = FIRST
family = LAGRANGE
[]
[]
[AuxVariables]
[fast_neutron_flux]
order = FIRST
family = LAGRANGE
initial_condition = 1.0e+17
[]
[scale_thickness] # ZrO2 scale thickness (m)
order = CONSTANT
family = MONOMIAL
[]
[oxyconc2_scale] # Oxygen concentration in ZrO2 scale (kg/m**2)
order = CONSTANT
family = MONOMIAL
[]
[oxyconc2_metal] # Oxygen concentration in metal (kg/m**2)
order = CONSTANT
family = MONOMIAL
[]
[oxyconc2_total] # Total oxygen concentration (oxide + metal) (kg/m**2)
order = CONSTANT
family = MONOMIAL
[]
[oxywtfract_metal] # Oxygen weight fraction in metal (/)
order = CONSTANT
family = MONOMIAL
[]
[oxywtfract_total] # Total oxygen weight fraction (oxide+metal) (/)
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[all]
strain = finite
use_automatic_differentiation = true
[]
[]
[Kernels]
[heat]
type = ADHeatConduction
variable = temp
[]
[]
[AuxKernels]
[fnflux]
type = FastNeutronFluxAux
variable = fast_neutron_flux
block = 1
function = FNFlux_func
execute_on = timestep_begin
[]
[scl_thickness]
type = ADMaterialRealAux
variable = scale_thickness
property = oxide_scale_thickness
boundary = 1
[]
[oconc_scale]
type = ADMaterialRealAux
variable = oxyconc2_scale
property = gained_oxygen_concentration_scale
boundary = 1
[]
[oconc_metal]
type = ADMaterialRealAux
variable = oxyconc2_metal
property = gained_oxygen_concentration_metal_wall
boundary = 1
[]
[oconc_total]
type = ADMaterialRealAux
variable = oxyconc2_total
property = gained_oxygen_concentration_total
boundary = 1
[]
[ofract_metal]
type = ADMaterialRealAux
variable = oxywtfract_metal
property = current_oxygen_weight_frac_metal_wall
boundary = 1
[]
[ofract_total]
type = ADMaterialRealAux
variable = oxywtfract_total
property = current_oxygen_weight_frac_total
boundary = 1
[]
[]
[BCs]
[bottom_T]
type = ADFunctionDirichletBC
variable = temp
function = Temp_func
boundary = 1
[]
[x_disp]
type = ADDirichletBC
variable = disp_x
value = 0
boundary = 1
[]
[y_disp]
type = ADDirichletBC
variable = disp_y
value = 0
boundary = 2
[]
[]
[Materials]
[elasticity_tensor]
type = ADZryElasticityTensor
block = 1
[]
[stress]
type = ADComputeFiniteStrainElasticStress
block = 1
[]
[thermal]
type = ADZryThermal
block = 1
temperature = temp
[]
[oxidation_zry]
type = ADZryOxidation
boundary = 1
normal_operating_temperature_model = epri_kwu_ce
high_temperature_model = leistikow
temperature = temp
fast_neutron_flux = fast_neutron_flux
[]
[]
[Executioner]
type = Transient
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = 'lu superlu_dist'
l_tol = 1.0e-08
nl_abs_tol = 1.0e-08
nl_rel_tol = 1.0e-08
start_time = 0.0
num_steps = 5000
end_time = 100000300
[TimeStepper]
type = IterationAdaptiveDT
dt = 1.0e+06
optimal_iterations = 6
iteration_window = 2
linear_iteration_ratio = 100
time_t = '0.0 100000000.'
time_dt = '1.0e+06 10.0 '
growth_factor = 1.0
[]
[]
[Postprocessors]
[_dt]
type = TimestepSize
[]
[temp]
type = NodalVariableValue
variable = temp
nodeid = 0
execute_on = 'initial timestep_end'
[]
[scale_thickness]
type = ElementalVariableValue
elementid = 0
variable = scale_thickness
[]
[oxyconc2_scale]
type = ElementalVariableValue
elementid = 0
variable = oxyconc2_scale
[]
[oxyconc2_metal]
type = ElementalVariableValue
elementid = 0
variable = oxyconc2_metal
[]
[oxyconc2_total]
type = ElementalVariableValue
elementid = 0
variable = oxyconc2_total
[]
[oxywtfract_metal]
type = ElementalVariableValue
elementid = 0
variable = oxywtfract_metal
[]
[oxywtfract_total]
type = ElementalVariableValue
elementid = 0
variable = oxywtfract_total
[]
[]
[Outputs]
exodus = true
[]
(assessment/LWR/validation/RIA_NSRR_FK/analysis/FK3/FK03_ccm.i)
# This file was created using BIF with the following inputs:
# FK03/FK03.var - md5sum: 63fb064f9380e246b80d3fb7762c0b71
# pulse.tpl - md5sum: 37e5a6b8a0c63ad020906dada3472585
[GlobalParams]
density = 10020.6066633
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
energy_per_fission = 3.2e-11
a_lower = 0.01822
a_upper = 0.12422
temperature = temp
volumetric_locking_correction = false
[]
[Mesh]
coord_type = RZ
[smeared_pellet_mesh]
type = FuelPinMeshGenerator
clad_mesh_density = customize
pellet_mesh_density = customize
elem_type = QUAD8
ny_p = 100
nx_c = 4
ny_c = 100
nx_p = 12
ny_cu = 3
ny_cl = 3
bx_p = 0.75
clad_bot_gap_height = 0.00152
bottom_clad_height = 0.0167
top_clad_height = 0.0167
clad_thickness = 0.00086
pellet_outer_radius = 0.00527
clad_top_gap_height = 0.05265
pellet_height = 0.106
clad_gap_width = 1e-05
pellet_quantity = 1
[]
patch_size = 5
patch_update_strategy = auto
partitioner = centroid
centroid_partitioner_direction = y
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
[]
[Variables]
[temp]
initial_condition = 293
[]
[]
[AuxVariables]
[BuTC]
[]
[gap]
order = CONSTANT
family = MONOMIAL
[]
[fast_neutron_flux]
block = 1
[]
[fast_neutron_fluence]
block = 1
[]
[buavg]
order = CONSTANT
family = MONOMIAL
[]
[fission_rate]
initial_condition = 0
[]
[grain_radius]
block = 3
initial_condition = 5.96e-6
[]
[integral_burnup]
order = CONSTANT
family = MONOMIAL
[]
[pellet_id]
order = CONSTANT
family = MONOMIAL
block = 3
[]
[gap_conductivity]
order = CONSTANT
family = MONOMIAL
[]
[porosity]
order = CONSTANT
family = MONOMIAL
initial_condition = 0.085711070864
[]
[SED]
order = CONSTANT
family = MONOMIAL
[]
[coolant_channel_htc]
order = CONSTANT
family = MONOMIAL
[]
[coolant_channel_hmode]
order = CONSTANT
family = MONOMIAL
[]
[coolant_channel_htype]
order = CONSTANT
family = MONOMIAL
[]
[critical_heat_flux]
order = CONSTANT
family = MONOMIAL
[]
[]
[Functions]
[linear_heat_rate_profile]
type = PiecewiseLinear
data_file = pulse.csv
format = columns
[]
[flux]
type = ConstantFunction
value = 0.0
[]
[axial_peaking_factors]
type = ConstantFunction
value = 1
[]
[coolant_pressure_ramp]
type = ConstantFunction
value = 101325
[]
[linear_heat_generation_rate]
type = CompositeFunction
functions = 'linear_heat_rate_profile axial_peaking_factors'
[]
[axial_flux]
type = CompositeFunction
functions = 'flux axial_peaking_factors'
[]
[burnup_thermal_conductivity]
type = ConstantFunction
value = 1 # should be burnup / 950
[]
[radial_power_profile]
type = PiecewiseLinear
data_file = RadialPowerProfile.csv
format = columns
axis = X
[]
[radial_burnup_profile]
type = PiecewiseLinear
data_file = RadialBurnupProfile.csv
format = columns
axis = X
[]
[initial_burnup]
type = CompositeFunction
functions = 'burnup_thermal_conductivity radial_burnup_profile'
[]
[]
[Burnup]
[burnup]
block = 3
rod_ave_lin_pow = linear_heat_rate_profile
axial_power_profile = axial_peaking_factors
rpf_input = radial_power_profile
num_radial = 80
num_axial = 49
fuel_inner_radius = 0.0
fuel_outer_radius = 0.00527
fuel_volume_ratio = 1.0
isotopes = 'U235 U238 Pu239 Pu240 Pu241 Pu242'
isotope_fractions = '0.039 0.961 0.0 0.0 0.0 0.0'
[]
[]
[Physics/SolidMechanics/QuasiStatic]
add_variables = true
[fuel]
block = 3
strain = FINITE
incremental = true
eigenstrain_names = 'fuel_thermal_eigenstrain
fuel_volumetric_swelling_eigenstrain'
extra_vector_tags = 'ref'
generate_output = 'vonmises_stress hydrostatic_stress elastic_strain_xx
elastic_strain_yy elastic_strain_zz stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz'
decomposition_method = EigenSolution
[]
[clad]
block = 1
strain = FINITE
incremental = true
eigenstrain_names = 'clad_thermal_eigenstrain'
extra_vector_tags = 'ref'
generate_output = 'vonmises_stress elastic_strain_xx
elastic_strain_yy elastic_strain_zz stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz creep_strain_xx creep_strain_yy creep_strain_zz'
decomposition_method = EigenSolution
[]
[]
[Kernels]
[gravity]
type = Gravity
variable = disp_y
value = -9.81
extra_vector_tags = 'ref'
[]
[heat]
type = HeatConduction
variable = temp
extra_vector_tags = 'ref'
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temp
extra_vector_tags = 'ref'
[]
[heat_source]
type = NeutronHeatSource
fission_rate = fission_rate
variable = temp
block = 3
extra_vector_tags = 'ref'
[]
[]
[AuxKernels]
[BuTC]
type = FunctionAux
block = 3
variable = BuTC
function = initial_burnup
[]
[pelletid]
type = PelletIdAux
block = 3
variable = pellet_id
number_pellets = 1
execute_on = initial
[]
[gap]
type = SpatialUserObjectAux
block = 3
variable = gap
execute_on = timestep_end
user_object = avg_gap
[]
[buavg]
type = SpatialUserObjectAux
block = 3
variable = buavg
execute_on = timestep_end
user_object = integral_burnup
[]
[fast_neutron_flux]
type = FastNeutronFluxAux
variable = fast_neutron_flux
function = axial_flux
block = 1
execute_on = timestep_begin
[]
[fast_neutron_fluence]
type = FastNeutronFluenceAux
variable = fast_neutron_fluence
block = 1
fast_neutron_flux = fast_neutron_flux
execute_on = timestep_begin
[]
[fuel_porosity]
type = PorosityAuxUO2
block = 3
variable = porosity
execute_on = timestep_begin
[]
[grain_radius]
type = GrainRadiusAux
block = 3
variable = grain_radius
temperature = temp
execute_on = timestep_begin
[]
[gap_conductance]
type = MaterialRealAux
property = gap_conductance
variable = gap_conductivity
boundary = 10
[]
[SED]
type = MaterialRealAux
variable = SED
property = strain_energy_density
execute_on = timestep_end
block = 1
[]
[coolant_channel_htc]
type = MaterialRealAux
variable = coolant_channel_htc
property = coolant_channel_htc
boundary = 2
[]
[coolant_channel_hmode]
type = MaterialRealAux
variable = coolant_channel_hmode
property = coolant_channel_hmode
boundary = 2
[]
[coolant_channel_htype]
type = MaterialRealAux
variable = coolant_channel_htype
property = coolant_channel_htype
boundary = 2
[]
[critical_heat_flux]
type = MaterialRealAux
variable = critical_heat_flux
property = critical_heat_flux
boundary = 2
[]
[]
[Contact]
[pellet_clad_mechanical]
primary = 5
secondary = 10
penalty = 1e14
normalize_penalty = true
model = frictionless
friction_coefficient = 2.5
normal_smoothing_distance = 0.1
formulation = penalty
[]
[]
[ThermalContact]
[thermal_contact]
type = GasGapHeatTransfer
variable = temp
primary = 5
secondary = 10
roughness_coef = 3.2
roughness_primary = 1.5e-6
roughness_secondary = 1.75e-6
jump_distance_model = LANNING
plenum_pressure = plenum_pressure
contact_pressure = contact_pressure
initial_moles = initial_moles
gas_released = fission_gas_released
tangential_tolerance = 1.0e-6
quadrature = true
[]
[]
[BCs]
[no_x_all]
type = DirichletBC
variable = disp_x
boundary = 12
value = 0.0
[]
[no_y_fuel_bottom]
type = DirichletBC
variable = disp_y
boundary = 20
value = 0.0
[]
[no_y_clad_bottom]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[]
[Pressure]
[coolantPressure]
boundary = '1 2 3'
factor = 1
function = coolant_pressure_ramp
[]
[]
[PlenumPressure]
[plenumPressure]
boundary = '10 5'
initial_pressure = 0.3e6
startup_time = 0
R = 8.314462
output_initial_moles = initial_moles
temperature = plenum_temperature
volume = plenum_volume
material_input = fission_gas_released
output = plenum_pressure
initial_temperature = 293
[]
[]
[]
[CoolantChannel]
[clad_outer_surface]
boundary = '1 2 3'
variable = temp
inlet_temperature = 295
inlet_pressure = 0.1E6 # Pa
inlet_massflux = 100.0 # kg/m^2-sec
rod_diameter = 1.10e-2 # m
rod_pitch = 1.26e-2 # m
compute_enthalpy = false
chf_scalef = 5.0
htc_correlation_type = 9
chf_correlation_type = 5
[]
[]
[Materials]
[fuel_swelling]
type = UO2VolumetricSwellingEigenstrain
block = 3
burnup = burnup
initial_fuel_density = 10020.6066633
total_densification = 0.006
gas_swelling_model_type = SIFGRS
eigenstrain_name = 'fuel_volumetric_swelling_eigenstrain'
[]
[fuel_thermal]
type = UO2Thermal
thermal_conductivity_model = NFIR
block = 3
temperature = temp
burnup = BuTC
initial_porosity = 0.085711070864
[]
[fuel_elasticity_tensor]
type = UO2ElasticityTensor
block = 3
[]
[fuel_thermal_expansion]
type = UO2ThermalExpansionMartinEigenstrain
block = 3
stress_free_temperature = 293
eigenstrain_name = 'fuel_thermal_eigenstrain'
[]
[fuel_elastic_stress]
type = ComputeFiniteStrainElasticStress
block = '3'
[]
[clad_thermal]
type = ZryThermal
block = 1
temperature = temp
[]
[clad_inelastic_stress]
type = ComputeMultipleInelasticStress
block = 1
tangent_operator = elastic
inelastic_models ='plasticity'
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = 1
fast_neutron_fluence = fast_neutron_fluence
initial_fast_fluence = 8.40e25
cold_work_factor = 0.01
matpro_youngs_modulus = true
matpro_poissons_ratio = true
[]
## TODO: Creep is not active, but is transfered from the SM version.
## Adding creep causes the Peak Hoop strain to best match the FALCON
## results given by R. Montgomery and D. Sunderland. Only retaining
## plasticity matches the results from Wenfeng Liu, John Alvis, Robert Montgomery, and Ken Yueh
[clad_creep_stress]
type = ZryCreepLimbackHoppeUpdate
block = 1
fast_neutron_flux = fast_neutron_flux
fast_neutron_fluence = fast_neutron_fluence
initial_fast_fluence = 8.40e25
[]
[clad_thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 293.0
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[plasticity]
type = ZryPlasticityUpdate
block = 1
initial_fast_fluence = 8.40e25
fast_neutron_flux = fast_neutron_flux
fast_neutron_fluence = fast_neutron_fluence
cold_work_factor = .01
plasticity_model_type = MATPRO
output_properties = yield_stress
outputs = all
zircaloy_alloy_type = 4
[]
[fission_gas_release]
type = UO2Sifgrs
block = 3
temperature = temp
fission_rate = fission_rate
grain_radius = grain_radius
gbs_model = true
burnup = BuTC
transient_option = MICROCRACKING
[]
[clad_density]
type = Density
block = 1
density = 6551
[]
[fuel_density]
type = Density
block = 3
[]
[strain_energy_density]
type = StrainEnergyDensity
incremental = true
[]
[]
[UserObjects]
[avg_gap]
type = LayeredAverage
block = 3
variable = penetration
direction = y
num_layers = 48
[]
[pbz]
type = PelletBrittleZone
block = 3
pellet_id = pellet_id
temperature = temp
pellet_radius = 0.00527
number_pellets = 1
execute_on = timestep_begin
[]
[integral_burnup]
type = LayeredAverage
block = 3
variable = burnup
direction = y
num_layers = 1
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
l_max_its = 40
l_tol = 8e-3
nl_max_its = 40
nl_rel_tol = 1e-3
nl_abs_tol = 1e-10
dtmin = 0.00001
dtmax = 1.0
start_time = 0
end_time = 100
[TimeStepper]
type = IterationAdaptiveDT
dt = 0.0001
optimal_iterations = 200
linear_iteration_ratio = 100
timestep_limiting_function = linear_heat_rate_profile
max_function_change = 550000
force_step_every_function_point = true
[]
[]
[Dampers]
[limitT]
type = MaxIncrement
max_increment = 100.0
variable = temp
[]
[limitX]
type = MaxIncrement
max_increment = 1e-5
variable = disp_x
[]
[contactslip]
type = ContactSlipDamper
primary = 5
secondary = 8
min_damping_factor = 0.05
[]
[]
[Postprocessors]
[max_hoop_strain]
type = ElementExtremeValue
variable = strain_zz
block = 1
[]
[max_SED]
type = ElementExtremeValue
variable = SED
block = 1
[]
[average_grain_radius]
type = ElementAverageValue
block = 3
outputs = 'exodus'
variable = grain_radius
[]
[clad_inner_vol]
type = InternalVolume
boundary = 7
outputs = 'exodus'
execute_on = 'timestep_begin initial'
[]
[flux_from_clad]
type = SideDiffusiveFluxIntegral
variable = temp
boundary = 5
diffusivity = thermal_conductivity
outputs = 'exodus'
[]
[flux_from_fuel]
type = SideDiffusiveFluxIntegral
variable = temp
boundary = 10
diffusivity = thermal_conductivity
outputs = 'exodus'
[]
[rod_total_power]
type = ElementIntegralPower
variable = temp
fission_rate = fission_rate
block = 3
[]
[rod_input_power]
type = FunctionValuePostprocessor
function = linear_heat_rate_profile
scale_factor = 0.106
[]
[average_fission_rate]
type = ElementAverageValue
variable = fission_rate
block = '3'
[]
[RAE]
type = RadialAverageEnthalpy
vector_postprocessor = rad_temp
radial_direction = x
axial_direction = y
axial_position = 0.0503
temperature_name = temp
[]
[peak_RAE]
type = TimeExtremeValue
postprocessor = RAE
[]
[]
[VectorPostprocessors]
[rad_temp]
type = NodalValueSampler
block = 3
sort_by = y
variable = temp
execute_on = timestep_end
outputs = dummy
[]
[]
[StandardLWRFuelRodOutputs]
fuel_pellet_blocks = 3
cladding_blocks = 1
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[chkfile]
type = CSV
show = 'average_centerline_fuel_temperature average_fission_rate fission_gas_released_percentage peak_RAE rod_total_power'
execute_on = 'FINAL'
[]
[console]
type = Console
max_rows = 25
output_linear = true
[]
[dummy]
type = CSV
enable = false
[]
[]
(assessment/LWR/validation/LOCA_ORNL_cladding_burst_tests/analysis/Zr4_1/ornl_zr4_1.i)
# Simulation ORNL burst tests Zr4_1
[GlobalParams]
density = 6550.
order = SECOND
family = LAGRANGE
displacements = 'disp_x disp_y'
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = zr4_ornl_burst_test_mesh.e
[]
[]
[Variables]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func] # only 10 inches of the rod are within the heated zone (cf. Terrani email)
type = PiecewiseBilinear
data_file = temperature_ornl_zr4_1.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
data_file = pressure_inner_ornl_zr4_1.csv
scale_factor = 1.e+06
format = columns
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 373.9'
y = '0.1 0.1 ' # atmospheric pressure
scale_factor = 1.e+06
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[clad]
block = cladding
add_variables = true
strain = FINITE
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
decomposition_method = EigenSolution
eigenstrain_names = 'clad_thermal_eigenstrain'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz hoop_stress'
[]
[]
[AuxVariables]
[creep_rate_aux]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[scale_thickness]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfract_total]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfgain_total]
order = CONSTANT
family = MONOMIAL
[]
[burst_stress]
order = CONSTANT
family = MONOMIAL
[]
[burst]
order = CONSTANT
family = MONOMIAL
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate_aux]
type = MaterialRealAux
variable = creep_rate_aux
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[scl_thickness]
type = MaterialRealAux
variable = scale_thickness
property = oxide_scale_thickness
boundary = 2
[]
[ofract_total]
type = MaterialRealAux
variable = oxywtfract_total
property = current_oxygen_weight_frac_total
boundary = 2
[]
[ofgain_total]
type = MaterialRealAux
boundary = 2
variable = oxywtfgain_total
property = oxygen_weight_frac_gained_total
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = 2
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = 2
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = FunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 4'
preset = false
[]
[no_y_top]
type = DirichletBC
variable = disp_y
boundary = 3
value = 0.
preset = false
[]
[Pressure]
[outer_pressure] # apply steam pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[mid_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 98 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
type = ZryThermal
block = cladding
temperature = temperature
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = cladding
matpro_youngs_modulus = false
matpro_poissons_ratio = false
[]
[clad_stress]
type = ComputeMultipleInelasticStress
tangent_operator = elastic
inelastic_models = 'clad_zrycreep'
block = cladding
[]
[clad_zrycreep]
type = ZryCreepLOCAUpdate
block = cladding
temperature = temperature
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
temperature_loca_creep_begin = 301
temperature_standard_thermal_creep_end = 300
[]
[thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = cladding
temperature = temperature
stress_free_temperature = 300.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[density]
type = Density
block = cladding
[]
[phase]
type = ZrPhase
block = cladding
temperature = temperature
numerical_method = 2
[]
[oxidation]
type = ZryOxidation
boundary = 2
temperature = temperature
clad_inner_radius = 0.004175
clad_outer_radius = 0.004750
normal_operating_temperature_model = epri_kwu_ce
high_temperature_model = leistikow
#use_coolant_channel = true
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = 2
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate_aux
temperature = temperature
fraction_beta_phase = fract_beta_phase
fraction_oxygen_gain = oxywtfgain_total
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0
n_startup_steps = 1
end_time = 373.9
dtmax = 1.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[Postprocessors]
[pressure_inner]
type = FunctionValuePostprocessor
function = inner_pressure_func
execute_on = 'initial timestep_end'
[]
[pressure_outer]
type = FunctionValuePostprocessor
function = outer_pressure_func
execute_on = 'initial timestep_end'
[]
[ave_clad_temp]
type = SideAverageValue
boundary = 2
variable = temperature
execute_on = 'initial timestep_end'
[]
[max_clad_temp]
type = NodalExtremeValue
block = cladding
value_type = max
variable = temperature
execute_on = 'initial timestep_end'
[]
[min_clad_temp]
type = NodalExtremeValue
block = cladding
value_type = min
variable = temperature
execute_on = 'initial timestep_end'
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = cladding
[]
[max_oxygen_fract]
type = ElementExtremeValue
block = cladding
value_type = max
variable = oxywtfract_total
execute_on = 'initial timestep_end'
[]
[max_betaph_fract]
type = ElementExtremeValue
block = cladding
value_type = max
variable = fract_beta_phase
execute_on = 'initial timestep_end'
[]
[max_creep_rate]
type = ElementExtremeValue
block = cladding
value_type = max
variable = creep_rate_aux
execute_on = 'initial timestep_end'
[]
[max_creep_strain_mag]
type = ElementExtremeValue
block = cladding
value_type = max
variable = creep_strain_mag
execute_on = 'initial timestep_end'
[]
[max_hoop_strain]
type = ElementExtremeValue
block = cladding
value_type = max
variable = strain_zz
execute_on = 'initial timestep_end'
[]
[max_hoop_stress]
type = ElementExtremeValue
block = cladding
value_type = max
variable = hoop_stress
[]
[vonmises_stress_clad]
type = ElementAverageValue
block = cladding
variable = vonmises_stress
execute_on = 'initial timestep_end'
[]
[min_burst_stress]
type = ElementExtremeValue
block = cladding
value_type = min
variable = burst_stress
execute_on = 'initial timestep_end'
[]
[burst]
type = ElementExtremeValue
block = cladding
value_type = max
variable = burst
execute_on = 'initial timestep_end'
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = cladding
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[mid_disp_r_clad]
type = NodalVariableValue
variable = disp_x
nodeid = 22
[]
[stress_xx_midplane] # stress in the mid Element
type = ElementalVariableValue
variable = stress_xx
elementid = 19
[]
[stress_yy_midplane] # stress in the mid Element
type = ElementalVariableValue
variable = stress_yy
elementid = 19
[]
[stress_zz_midplane] # stress in the mid Element
type = ElementalVariableValue
variable = stress_zz
elementid = 19
[]
[strain_zz_midplane] # strain in the mid Element
type = ElementalVariableValue
variable = strain_zz
elementid = 19
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
plenum_boundary_name = 4
cladding_blocks = cladding
[]
[PerformanceMetricOutputs]
[]
[Outputs]
exodus = true
perf_graph = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 20
[]
[chkfile]
type = CSV
file_base = ornl_zr4_1_chkfile
show = 'pressure_inner max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-18/puzry-18.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-18.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 1500. '
y = '1.e+05 1.e+05 5.855e+06' # Linear increase at 0.1151 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 1500. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = EigenSolution
[]
[]
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = MaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = FunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = DirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = DirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1.e+11
poissons_ratio = 0.3
block = 1
[]
[creep_update]
type = ZryCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 1.e-04
temperature = temperature
temperature_standard_thermal_creep_end = 700
temperature_loca_creep_begin = 900.
[]
[creep]
type = ComputeMultipleInelasticStress
block = 1
tangent_operator = elastic
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = Density
block = 1
[]
[phase]
type = ZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
active = 'smp'
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0.
n_startup_steps = 1
end_time = 1500.
dtmax = 1.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-18_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/LOCA_IFA_650/analysis/IFA_650_4/IFA_650_4_part1.i)
[GlobalParams]
density = 10452.96
initial_porosity = 0.048
order = SECOND
family = LAGRANGE
displacements = disp_x
temperature = temperature
energy_per_fission = 3.2e-11 #J/fission
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
acceptable_multiplier = 10
[]
[Mesh]
coord_type = RZ
[layered1D_mesh]
type = Layered1DMeshGenerator
slices_per_block = 30
pellet_outer_radius = 4.565e-3
clad_gap_width = 0.085e-3
clad_thickness = 0.725e-3
fuel_height = 0.480
plenum_height = 0.291185
pellet_mesh_density = customize
clad_mesh_density = customize
nx_p = 11
nx_c = 5
[]
patch_update_strategy = auto
partitioner = centroid
centroid_partitioner_direction = y
[]
[Variables]
[disp_x]
[]
[temperature]
initial_condition = 295.0
[]
[]
[Functions]
[power_history]
type = PiecewiseLinear
data_file = power_history.csv
scale_factor = 1.0
format = columns
[]
[axial_peaking_factors]
type = PiecewiseBilinear
data_file = axial_peaking_factors.csv
axis = 1
scale_factor = 1
[]
[pressure_ramp]
type = PiecewiseLinear
data_file = coolant_pressure.csv
scale_factor = 1
format = columns
[]
[average_htc]
type = PiecewiseLinear
data_file = average_coolant_htc.csv
format = columns
scale_factor = 1
[]
[forced_times]
type = PiecewiseLinear
data_file = timestep_limiting.csv
scale_factor = 1
format = columns
[]
[heat_sink_temperature]
type = PiecewiseBilinear
data_file = heater_temp.csv
scale_factor = 1
axis = 1
[]
[clad_outer_temperature]
type = PiecewiseBilinear
data_file = clad_surface_temp.csv
scale_factor = 1
axis = 1
[]
[heat_transfer_mode]
type = PiecewiseConstant
x = '-200 172489073 172489661'
y = '9 9 8 '
direction = 'right'
[]
[clad_axial_pressure]
type = CladdingAxialPressureFunction
plenum_pressure = plenum_pressure
coolant_pressure = pressure_ramp
coolant_pressure_scaling_factor = 1.0
fuel_pin_geometry = fuel_pin_geometry
[]
[fuel_axial_pressure]
type = ParsedFunction
expression = plenum_pressure
symbol_names = plenum_pressure
symbol_values = plenum_pressure
[]
[]
[AuxVariables]
[disp_y]
[]
[disp_z]
[]
[fast_neutron_flux]
block = clad
[]
[fast_neutron_fluence]
block = clad
[]
[grain_radius]
block = fuel
initial_condition = 5.0e-6
[]
[hoop_stress]
order = CONSTANT
family = MONOMIAL
[]
[effective_creep_strain]
block = clad
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[oxide_thickness]
order = CONSTANT
family = MONOMIAL
[]
[burst]
order = CONSTANT
family = MONOMIAL
[]
[gap_conductance]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[layered_maximum_clad_radius]
order = CONSTANT
family = MONOMIAL
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
extra_vector_tags = 'ref'
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
extra_vector_tags = 'ref'
[]
[heat_source]
type = NeutronHeatSource
variable = temperature
block = fuel
burnup_function = burnup
axial_relocation_object = axial_relocation
extra_vector_tags = 'ref'
[]
[]
[Physics]
[SolidMechanics]
[Layered1D]
[fuel]
add_scalar_variables = true
out_of_plane_strain_name = strain_yy
fuel_pin_geometry = fuel_pin_geometry
out_of_plane_pressure_function = fuel_axial_pressure
strain = finite
block = fuel
eigenstrain_names = 'fuel_thermal_strain fuel_swelling_strain fuel_relocation_strain axial_relocation_eigenstrain'
decomposition_method = EigenSolution
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress'
extra_vector_tags = 'ref'
group_scalar_vars_in_reference_residual = true
mesh_generator = layered1D_mesh
[]
[clad]
add_scalar_variables = true
out_of_plane_strain_name = strain_yy
fuel_pin_geometry = fuel_pin_geometry
strain = finite
out_of_plane_pressure_function = clad_axial_pressure
block = clad
eigenstrain_names = 'clad_thermal_strain clad_irradiation_strain'
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress strain_zz creep_strain_zz'
decomposition_method = EigenSolution
extra_vector_tags = 'ref'
group_scalar_vars_in_reference_residual = true
mesh_generator = layered1D_mesh
[]
[]
[]
[]
[Burnup]
[burnup]
block = fuel
rod_ave_lin_pow = power_history
axial_power_profile = axial_peaking_factors
num_radial = 80
num_axial = 11
fuel_pin_geometry = fuel_pin_geometry
fuel_volume_ratio = 1.0
order = CONSTANT
family = MONOMIAL
RPF = RPF
isotopes = 'U235 U238 Pu239 Pu240 Pu241 Pu242'
isotope_fractions = '0.035 0.965 0 0 0 0'
[]
[]
[AuxKernels]
[fast_neutron_flux]
type = FastNeutronFluxAux
block = clad
variable = fast_neutron_flux
rod_ave_lin_pow = power_history
axial_power_profile = axial_peaking_factors
factor = 3e13
execute_on = timestep_begin
[]
[fast_neutron_fluence]
type = FastNeutronFluenceAux
block = clad
variable = fast_neutron_fluence
fast_neutron_flux = fast_neutron_flux
execute_on = timestep_begin
[]
[grain_radius]
type = GrainRadiusAux
block = fuel
variable = grain_radius
temperature = temperature
execute_on = linear
[]
[hoop_stress]
type = RankTwoScalarAux
rank_two_tensor = stress
variable = hoop_stress
scalar_type = HoopStress
execute_on = timestep_end
[]
[effective_creep_strain]
type = MaterialRealAux
block = clad
variable = effective_creep_strain
property = effective_creep_strain
execute_on = 'timestep_end'
[]
[fract_bphase]
type = MaterialRealAux
block = clad
variable = fract_beta_phase
property = fract_beta_phase
execute_on = 'initial linear'
[]
[oxide_thickness]
type = MaterialRealAux
boundary = 2
variable = oxide_thickness
property = oxide_scale_thickness
execute_on = 'initial linear'
[]
[hasburst]
type = MaterialRealAux
boundary = 2
variable = burst
property = failed
execute_on = timestep_end
[]
[conductance]
type = MaterialRealAux
boundary = 10
property = gap_conductance
variable = gap_conductance
execute_on = 'initial linear'
[]
[coolant_htc]
type = MaterialRealAux
property = coolant_channel_htc
variable = coolant_htc
boundary = 2
execute_on = 'initial linear'
[]
[creep_rate]
type = MaterialRealAux
block = clad
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[]
[AxialRelocation]
[relocation]
mesh_generator = layered1D_mesh
rod_ave_lin_pow = power_history
axial_direction = y
fuel_blocks = fuel
clad_blocks = clad
contact_pressure_variable = contact_pressure
out_of_plane_strain_variable = strain_yy
penetration_variable = penetration
clad_inner_volume_addition = 0
burnup_variable = burnup
temperature = temperature
axial_relocation_output_options = MASS_FRACTION
[]
[]
[CoolantChannel]
[convective_clad_surface] # apply convective boundary to clad outer surface
boundary = 2
variable = temperature
heat_transfer_mode = heat_transfer_mode
heat_transfer_coefficient = average_htc # Calculated from an initial simulation of the base irradiation using the inlet_pressure, inlet_massflux, and inlet_temperature commented out below.
inlet_temperature = heat_sink_temperature # K
effective_emissivity = 0.75
# inlet_temperature = 580
# inlet_pressure = 15.3e6 # Pa
# inlet_massflux = 3800 # kg/m^2-sec
rod_diameter = 0.01075 # m
rod_pitch = 1.26e-2 # m
compute_enthalpy = false
linear_heat_rate = power_history
axial_power_profile = axial_peaking_factors
output_properties = 'coolant_channel_htype coolant_channel_hmode'
[]
[]
[Contact]
[pellet_clad_mechanical]
primary = 5
secondary = 10
penalty = 1e7
formulation = kinematic
model = frictionless
[]
[]
[ThermalContact]
[thermal_contact]
type = GasGapHeatTransfer
variable = temperature
primary = 5
secondary = 10
initial_moles = initial_moles
gas_released = fis_gas_released
plenum_pressure = plenum_pressure
contact_pressure = contact_pressure
jump_distance_model = LANNING
roughness_coef = 3.2
refab_gas_types = 'He Ar'
refab_fractions = '0.05 0.95'
refab_time = 172387800
refab_type = 0
[]
[]
[BCs]
[no_x_all]
type = DirichletBC
variable = disp_x
boundary = 12
value = 0.0
[]
[Pressure]
[coolantPressure]
boundary = 2
function = pressure_ramp
factor = 1.0
[]
[]
[clad_outer_temp]
type = FunctionDirichletBC
boundary = 2
variable = temperature
function = clad_outer_temperature
[]
[PlenumPressure]
[plenumPressure]
boundary = 9
initial_pressure = 2.0e6
startup_time = 0
R = 8.3143
output_initial_moles = initial_moles
temperature = plenum_temp
volume = 'clad_volume pellet_volume'
material_input = fis_gas_released
output = plenum_pressure
refab_time = 172387800
refab_pressure = 4.0e6
refab_temperature = 295.0
refab_volume = 2.15e-05
[]
[]
[]
[LayeredPlenumTemperature]
[plenum_temp]
boundary = 5
fuel_pin_geometry = fuel_pin_geometry
out_of_plane_strain = strain_yy
inner_surfaces = '5'
outer_surfaces = '10'
temperature = temperature
[]
[]
[Controls]
[period0]
type = TimePeriod
disable_objects = 'BCs/clad_outer_temp'
start_time = -200.0
end_time = 172387800.0
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
execute_on = timestep_end
[]
[]
[Materials]
[fuel_thermal]
type = UO2Thermal
block = fuel
thermal_conductivity_model = STAICU
hbs_porosity_correction = KAMPF
model_hbs_formation = true
temperature = temperature
burnup_function = burnup
axial_relocation_object = axial_relocation
gap_thermal_conductivity = layered_average_gap_conductivity
[]
[relocation]
type = UO2RelocationEigenstrain
block = fuel
burnup_function = burnup
rod_ave_lin_pow = power_history
axial_power_profile = axial_peaking_factors
fuel_pin_geometry = fuel_pin_geometry
burnup_relocation_stop = 0.024
relocation_activation1 = 5000.0
relocation_model = ESCORE_modified
eigenstrain_name = fuel_relocation_strain
[]
[fuel_thermal_strain]
type = ComputeThermalExpansionEigenstrain
block = fuel
thermal_expansion_coeff = 10.0e-6
stress_free_temperature = 295.0
eigenstrain_name = fuel_thermal_strain
[]
[fuel_swelling]
type = UO2VolumetricSwellingEigenstrain
gas_swelling_model_type = SIFGRS
block = fuel
burnup_function = burnup
initial_fuel_density = 10452.96
eigenstrain_name = fuel_swelling_strain
[]
[fission_gas_release]
type = UO2Sifgrs
block = fuel
temperature = temperature
burnup_function = burnup
grain_radius = grain_radius
transient_option = MICROCRACKING_BURNUP
diff_coeff_option = TURNBULL_D1_D2
gbs_model = true
[]
[fuel_elasticity_tensor]
type = UO2IsotropicDamageElasticityTensor
block = fuel
fragmentation_model = BARANI
temperature = temperature
rod_ave_lin_pow = power_history
axial_relocation_object = axial_relocation
crumbling_scale_factor = 0.0001
[]
[fuel_stress]
type = ComputeMultipleInelasticStress
tangent_operator = elastic
inelastic_models = 'fuel_creep'
block = fuel
[]
[fuel_creep]
type = UO2CreepUpdate
block = fuel
temperature = temperature
burnup_function = burnup
initial_grain_radius = 5.0e-6
[]
[HBS]
type = HighBurnupStructureFormation
block = fuel
burnup_function = burnup
temperature = temperature
output_properties = 'hbs_volume_fraction'
outputs = 'exodus'
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = clad
[]
[stress]
type = ComputeMultipleInelasticStress
tangent_operator = elastic
inelastic_models = 'zrycreep'
block = clad
[]
[zrycreep]
type = ZryCreepLOCAUpdate
fast_neutron_flux = fast_neutron_flux
fast_neutron_fluence = fast_neutron_fluence
model_irradiation_creep = true
model_primary_creep = true
model_thermal_creep = true
max_inelastic_increment = 5e-4
zircaloy_material_type = stress_relief_annealed
block = clad
[]
[thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = clad
stress_free_temperature = 295.0
eigenstrain_name = clad_thermal_strain
[]
[irradiation_swelling]
type = ZryIrradiationGrowthEigenstrain
block = clad
fast_neutron_fluence = fast_neutron_fluence
zircaloy_material_type = stress_relief_annealed
eigenstrain_name = clad_irradiation_strain
[]
[clad_phase]
type = ZrPhase
block = clad
temperature = temperature
numerical_method = 2
[]
[clad_oxidation]
type = ZryOxidation
boundary = 2
temperature = temperature
clad_inner_radius = 4.65e-03
clad_outer_radius = 5.375e-03
normal_operating_temperature_model = epri_kwu_ce
high_temperature_model = cathcart
use_coolant_channel = true
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = 2
failure_criterion = overstrain
hoop_stress = hoop_stress
hoop_creep_strain = creep_strain_zz
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[clad_thermal]
type = ZryThermal
block = clad
temperature = temperature
[]
[fuel_density]
type = Density
block = fuel
[]
[clad_density]
type = Density
block = clad
density = 6551.0
[]
[]
[Postprocessors]
[ave_temp_interior]
type = LayeredSideAverageValuePostprocessor
boundary = 9
variable = temperature
execute_on = 'initial linear'
fuel_pin_geometry = fuel_pin_geometry
[]
[pellet_volume_2]
type = LayeredInternalVolumePostprocessor
boundary = 8
component = 0
fuel_pin_geometry = fuel_pin_geometry
out_of_plane_strain = strain_yy
execute_on = 'initial linear'
[]
[avg_clad_temp]
type = LayeredSideAverageValuePostprocessor
boundary = 7
variable = temperature
fuel_pin_geometry = fuel_pin_geometry
execute_on = 'initial linear'
[]
[fis_gas_produced]
type = LayeredElementIntegralFisGasGeneratedSifgrsPostprocessor
block = fuel
fuel_pin_geometry = fuel_pin_geometry
[]
[fis_gas_released]
type = LayeredElementIntegralFisGasReleasedSifgrsPostprocessor
block = fuel
fuel_pin_geometry = fuel_pin_geometry
[]
[fis_gas_grain]
type = LayeredElementIntegralFisGasGrainSifgrsPostprocessor
block = fuel
outputs = exodus
fuel_pin_geometry = fuel_pin_geometry
[]
[fis_gas_boundary]
type = LayeredElementIntegralFisGasBoundarySifgrsPostprocessor
block = fuel
outputs = exodus
fuel_pin_geometry = fuel_pin_geometry
[]
[fission_gas_release]
type = FGRPercent
fission_gas_released = fis_gas_released
fission_gas_generated = fis_gas_produced
[]
[average_coolant_htc]
type = LayeredSideAverageValuePostprocessor
boundary = 2
variable = coolant_htc
execute_on = 'initial linear'
fuel_pin_geometry = fuel_pin_geometry
[]
[average_burnup]
type = RodAverageBurnup
burnup_function = burnup
[]
[temp_clad_max]
type = NodalExtremeValue
block = clad
value_type = max
variable = temperature
execute_on = 'initial timestep_end'
[]
[betaph_fract_max]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
block = clad
execute_on = 'initial timestep_end'
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
block = clad
execute_on = 'initial timestep_end'
[]
[timestep_material]
type = MaterialTimeStepPostprocessor
block = clad
execute_on = 'initial timestep_end'
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = clad
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geometry
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[Dampers]
[limitT]
type = BoundingValueNodalDamper
variable = temperature
max_value = 3200.0
min_value = 0.0
[]
[limitX]
type = MaxIncrement
max_increment = 1e-5
variable = disp_x
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package -ksp_gmres_restart'
petsc_options_value = 'lu superlu_dist 51'
line_search = 'none'
l_max_its = 50
l_tol = 1e-3
nl_max_its = 30
nl_rel_tol = 1e-4
nl_abs_tol = 1e-8
dtmax = 5e5
dtmin = 1e-5
start_time = -200.0
end_time = 172387800 # End base irradiation
# end_time = 172489043 # Begin Blowdown
# end_time = 172489661 # End
[TimeStepper]
type = IterationAdaptiveDT
dt = 200
timestep_limiting_postprocessor = timestep_material
optimal_iterations = 20
iteration_window = 4
linear_iteration_ratio = 100
timestep_limiting_function = forced_times
force_step_every_function_point = true
max_function_change = 2000
time_t = '172387800 172388043 172488043 172489043 172489073 172489661'
time_dt = '1.0e04 1.0e04 10.0 5.0 0.5 5.0'
[]
[]
[VectorPostprocessors]
[clad_radial_disp]
type = NodalValueSampler
variable = disp_x
boundary = 2
sort_by = y
outputs = 'outfile_1'
[]
[clad_out_temp]
type = NodalValueSampler
variable = temperature
boundary = 2
sort_by = y
outputs = 'outfile_temp_1'
[]
[mass_fraction]
type = LineValueSampler
start_point = '0 0.01124 0'
end_point = '0 0.47524 0'
num_points = 30
sort_by = y
variable = layered_mass_fraction
outputs = 'outfile_mass_1'
[]
[]
[PerformanceMetricOutputs]
[]
[Outputs]
csv = true
color = false
perf_graph = true
[exodus]
type = Exodus
file_base = IFA_650_4_part1_out
execute_on = 'initial timestep_end'
[]
[checkpoint]
type = Checkpoint
time_step_interval = 1
num_files = 1
[]
[outfile_1]
type = CSV
execute_on = 'FINAL'
create_final_symlink = true
[]
[outfile_temp_1]
type = CSV
execute_on = 'FINAL'
create_final_symlink = true
[]
[outfile_mass_1]
type = CSV
execute_on = 'FINAL'
create_final_symlink = true
[]
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-25/puzry-25_aniso.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-25.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 6000. '
y = '1.e+05 1.e+05 8.75e+06' # Linear increase at 0.0173 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 6000. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
# Circumferential steady-state creep test and analysis of Zircaloy-4 fuel cladding
# Nuclear Engineering and Design, 53, 2312-2322 (2021)
[F]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.738 0.738 0.57'
[]
[G]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.174 0.174 0.45'
[]
[H]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.588 0.588 0.48'
[]
[L]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[M]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[N]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = TaylorExpansion
use_automatic_differentiation = true
[]
[]
[]
[]
[Kernels]
[heat]
type = ADHeatConduction
variable = temperature
[]
[heat_ie]
type = ADHeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = ADMaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = ADMaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = ADMaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = ADMaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = ADMaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = ADFunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = ADDirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = ADDirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ADZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1.e+11
poissons_ratio = 0.3
block = 1
[]
[hill_constants]
type = ADHillConstants
hill_constants = "0.738 0.174 0.588 1.0 1.0 1.0"
function_names = "F G H L M N"
temperature = temperature
[]
[creep_update]
type = ADZryAnisoCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 7.5e-05
temperature = temperature
temperature_standard_thermal_creep_end = 700
temperature_loca_creep_begin = 900.
fract_beta_phase_name = 'fract_beta_phase'
max_integration_error = 1000000.0
absolute_tolerance = 1e-13
relative_tolerance = 1e-11
[]
[creep]
type = ADComputeMultipleInelasticStress
block = 1
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ADZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = ADDensity
block = 1
[]
[phase]
type = ADZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ADZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = NEWTON
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-07
start_time = 0.
n_startup_steps = 1
end_time = 2500.
dtmax = 1.
dtmin = 1.0e-9
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-25_aniso_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(test/tests/phase_transition_zircaloy/ad_test_zrphase.i)
# This test demonstrates the usage of the model for the high-temperature alpha <--> beta phase transition of Zircaloy. This is implemented in the class ZrPhase.
# Only Zircaloy-4 is considered at the moment.
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
temperature = temp
[]
[Mesh]
[mesh]
type = FileMeshGenerator
file = cube_111.e
[]
[]
[Functions]
[Temp_func]
type = PiecewiseLinear
x = '0. 10800. 50000. 50075. 50150. 50260.'
y = '300. 650. 650. 1400. 1400. 300. '
[]
[]
[Variables]
[temp]
order = FIRST
family = LAGRANGE
initial_condition = 300.
[]
[]
[AuxVariables]
[ratep_zrphase] # rate parameter
order = CONSTANT
family = MONOMIAL
[]
[fract_bp_equilibrium] # equilibrium beta/alpha phase fraction
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # actual beta/alpha phase fraction
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[solid]
block = 1
strain = FINITE
incremental = true
add_variables = true
use_automatic_differentiation = true
[]
[]
[Kernels]
[heat]
type = ADHeatConduction
variable = temp
[]
[]
[AuxKernels]
[rateparam]
type = ADMaterialRealAux
variable = ratep_zrphase
property = ratep_zrphase
block = 1
[]
[fractbp_eq]
type = ADMaterialRealAux
variable = fract_bp_equilibrium
property = fract_bp_equilibrium
block = 1
[]
[fract_bphase]
type = ADMaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
block = 1
[]
[]
[BCs]
[bottom_T]
type = ADFunctionDirichletBC
variable = temp
function = Temp_func
boundary = 1
[]
[x_disp]
type = ADDirichletBC
variable = disp_x
value = 0
boundary = 1
[]
[y_disp]
type = ADDirichletBC
variable = disp_y
value = 0
boundary = 2
[]
[z_disp]
type = ADDirichletBC
variable = disp_z
value = 0
boundary = 3
[]
[]
[Materials]
[felasticity_tensor]
type = ADComputeIsotropicElasticityTensor
block = 1
youngs_modulus = 7.5e+10
poissons_ratio = 0.3
[]
[elastic_stress]
type = ADComputeFiniteStrainElasticStress
block = 1
[]
[thermal]
type = ADZryThermal
block = 1
temperature = temp
[]
[phase]
type = ADZrPhase
block = 1
numerical_method = 2
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
l_tol = 1.e-08
nl_abs_tol = 1.e-08
nl_rel_tol = 1.e-08
start_time = 0.
num_steps = 5000
end_time = 50260
[TimeStepper]
type = IterationAdaptiveDT
dt = 1.e+02
optimal_iterations = 6
iteration_window = 2
linear_iteration_ratio = 100
time_t = '0. 10800. 50000. 50090. 50180. 50290.'
time_dt = '1.e+03 2.e+03 1. 1. 1. 1. '
growth_factor = 1.
[]
[]
[Postprocessors]
[_dt]
type = TimestepSize
[]
[temp]
type = NodalVariableValue
variable = temp
nodeid = 0
execute_on = 'initial timestep_end'
[]
[rate_parameter]
type = ElementalVariableValue
elementid = 0
variable = ratep_zrphase
[]
[beta_equilibrium]
type = ElementalVariableValue
elementid = 0
variable = fract_bp_equilibrium
[]
[beta_phase_fraction]
type = ElementalVariableValue
elementid = 0
variable = fract_beta_phase
[]
[]
[Outputs]
file_base = out_ad_test_zrphase
[exodus]
type = Exodus
[]
[]
(assessment/LWR/validation/RIA_CABRI_REP_Na/analysis/REP_Na_10/REP_Na_10.i)
# REP Na 10 Rodlet
[GlobalParams]
density = 10448.925 # assumed TD = 10970
displacements = 'disp_x disp_y'
temperature = temp
order = SECOND
family = LAGRANGE
energy_per_fission = 3.2e-11
volumetric_locking_correction = false
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
acceptable_iterations = 30
acceptable_multiplier = 10
[]
[Mesh]
coord_type = RZ
[smeared_pellet_mesh]
type = FuelPinMeshGenerator
clad_mesh_density = customize
pellet_mesh_density = customize
nx_p = 11
ny_p = 156
ny_cu = 3
ny_c = 160
ny_cl = 3
nx_c = 4
clad_thickness = 0.0005753
pellet_outer_radius = 0.004096055
pellet_quantity = 39
pellet_height = 0.01425001
clad_top_gap_height = 0.032027026
clad_bot_gap_height = 0.003
clad_gap_width = 82.0e-6
bottom_clad_height = 0.0015
top_clad_height = 0.0015
elem_type = QUAD8
[]
patch_size = 40
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temp]
initial_condition = 293.15
[]
[]
[AuxVariables]
[fast_neutron_flux]
block = 1
[]
[fast_neutron_fluence]
block = 1
[]
[grain_radius]
block = 3
initial_condition = 5.0e-6
[]
[gap_cond]
order = CONSTANT
family = MONOMIAL
[]
[fuel_cond]
order = CONSTANT
family = MONOMIAL
[]
[swelling_strain]
order = CONSTANT
family = MONOMIAL
block = 3
[]
[total_hoop_strain]
order = CONSTANT
family = MONOMIAL
[]
[total_axial_strain]
order = CONSTANT
family = MONOMIAL
[]
[clad_coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[coolant_temp]
order = CONSTANT
family = MONOMIAL
[]
[clad_coolant_flux]
order = CONSTANT
family = MONOMIAL
[]
[coolant_channel_hmode]
order = CONSTANT
family = MONOMIAL
[]
[coolant_channel_htype]
order = CONSTANT
family = MONOMIAL
[]
[critical_heat_flux]
order = CONSTANT
family = MONOMIAL
[]
[oxide_thickness]
order = CONSTANT
family = MONOMIAL
[]
[SED]
order = CONSTANT
family = MONOMIAL
block = 1
[]
[oxywtfract_total]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfgain_total]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[]
[Functions]
[power_profile]
type = PiecewiseLinear
data_file = REPNa10_power_history_Full.csv
format = columns
[]
[axial_peaking_factors]
type = PiecewiseBilinear
data_file = REPNa10_axial_peaking_Full.csv
axis = 1
[]
[pressure_ramp]
type = PiecewiseLinear
xy_data = '0 101325
8640 15499970
125280000 15499970
125366400 101325
125798400 101325
125798410 101325
125798450 500008
125798500 500008
125798700 500008
125798800 101325
125798900 101325'
[]
[temp_ramp]
type = PiecewiseLinear
xy_data = '0 293.15
8640 588.706
125280000 588.706
125366400 293.15
125798400 293.15
125798410 293.15
125798450 553.15
125798500 553.15
125798700 553.15
125798800 293.15
125798900 293.15'
[]
[Fuel_CTE_function] #Fuel CTE as a function of temp from MATPRO data
type = PiecewiseLinear
xy_data = ' 0 1.000E-05
300 1.000E-05
350 1.000E-05
400 1.000E-05
450 1.000E-05
500 1.001E-05
550 1.002E-05
600 1.003E-05
650 1.005E-05
700 1.008E-05
750 1.011E-05
800 1.015E-05
850 1.020E-05
900 1.026E-05
950 1.032E-05
1000 1.039E-05
1050 1.046E-05
1100 1.053E-05
1150 1.061E-05
1200 1.069E-05
1250 1.077E-05
1300 1.085E-05
1350 1.094E-05
1400 1.102E-05
1450 1.111E-05
1500 1.119E-05
1550 1.127E-05
1600 1.135E-05
1650 1.143E-05
1700 1.151E-05
1750 1.158E-05
1800 1.166E-05
1850 1.173E-05
1900 1.180E-05
1950 1.187E-05
2000 1.193E-05
2050 1.199E-05
2100 1.205E-05
2150 1.211E-05
2200 1.217E-05
2250 1.222E-05
2300 1.227E-05
2350 1.232E-05
2400 1.237E-05
2450 1.242E-05
2500 1.246E-05
2550 1.250E-05
2600 1.254E-05
2650 1.258E-05
2700 1.262E-05
2750 1.265E-05
2800 1.268E-05
2850 1.271E-05
2900 1.274E-05
2950 1.277E-05
3000 1.280E-05
3050 1.282E-05
3100 1.285E-05'
[]
[burnup_GWd]
type = ParsedFunction
expression = bu*950
symbol_names = 'bu'
symbol_values = 'average_burnup'
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[fuel]
block = 3
strain = FINITE
incremental = true
eigenstrain_names = 'fuel_relocation_eigenstrain fuel_thermal_eigenstrain
fuel_volumetric_swelling_eigenstrain'
extra_vector_tags = 'ref'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz'
[]
[clad]
block = 1
strain = FINITE
incremental = true
eigenstrain_names = 'clad_irradiation_growth_eigenstrain
clad_thermal_eigenstrain'
extra_vector_tags = 'ref'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz plastic_strain_xx plastic_strain_yy plastic_strain_zz
creep_strain_xx creep_strain_yy creep_strain_zz elastic_strain_xx
elastic_strain_yy elastic_strain_zz hoop_stress'
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temp
extra_vector_tags = 'ref'
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temp
extra_vector_tags = 'ref'
[]
[heat_source_fuel]
type = NeutronHeatSource
variable = temp
block = 3
burnup_function = burnup
extra_vector_tags = 'ref'
[]
[]
[Burnup]
[burnup]
block = 3
rod_ave_lin_pow = power_profile
axial_power_profile = axial_peaking_factors
num_radial = 80
num_axial = 40
a_upper = 0.5602504
a_lower = 0.0045
fuel_inner_radius = 0
fuel_outer_radius = 0.004096055
fuel_volume_ratio = 1
isotopes = 'U235 U238 Pu239 Pu240 Pu241 Pu242'
isotope_fractions = '0.045 0.955 0 0 0 0'
RPF = RPF
order = CONSTANT
family = MONOMIAL
[]
[]
[AuxKernels]
[fast_neutron_flux]
type = FastNeutronFluxAux
variable = fast_neutron_flux
block = 1
axial_power_profile = axial_peaking_factors
rod_ave_lin_pow = power_profile
factor = 3e13 #n/m2-s
execute_on = timestep_begin
[]
[fast_neutron_fluence]
type = FastNeutronFluenceAux
variable = fast_neutron_fluence
fast_neutron_flux = fast_neutron_flux
block = 1
execute_on = timestep_begin
[]
[grain_radius]
type = GrainRadiusAux
block = 3
variable = grain_radius
temperature = temp
execute_on = linear
[]
[gap_conductance]
type = MaterialRealAux
property = gap_conductance
variable = gap_cond
boundary = 10
[]
[fuel_conductance]
type = MaterialRealAux
property = thermal_conductivity
variable = fuel_cond
block = 3
[]
[swelling_strain]
type = MaterialRealAux
property = volumetric_swelling_strain
variable = swelling_strain
block = 3
[]
[total_hoop_strain]
type = RankTwoScalarAux
rank_two_tensor = total_strain
variable = total_hoop_strain
scalar_type = HoopStress
execute_on = timestep_end
block = 1
[]
[total_axial_strain]
type = RankTwoScalarAux
rank_two_tensor = total_strain
variable = total_axial_strain
scalar_type = AxialStress
execute_on = timestep_end
block = 1
[]
[clad_coolant_htc]
type = MaterialRealAux
property = coolant_channel_htc
variable = clad_coolant_htc
boundary = 2
[]
[coolant_temp]
type = MaterialRealAux
property = coolant_temperature
variable = coolant_temp
boundary = 2
[]
[clad_coolant_flux]
type = MaterialRealAux
property = output_heat_flux
variable = clad_coolant_flux
boundary = 2
[]
[coolant_channel_hmode]
type = MaterialRealAux
property = coolant_channel_hmode
variable = coolant_channel_hmode
boundary = 2
[]
[coolant_channel_htype]
type = MaterialRealAux
property = coolant_channel_htype
variable = coolant_channel_htype
boundary = 2
[]
[critical_heat_flux]
type = MaterialRealAux
property = critical_heat_flux
variable = critical_heat_flux
boundary = 2
[]
[oxide]
type = MaterialRealAux
property = oxide_scale_thickness
variable = oxide_thickness
boundary = 2
[]
[SED]
type = MaterialRealAux
variable = SED
property = strain_energy_density
execute_on = timestep_end
[]
[ofract_total]
type = MaterialRealAux
variable = oxywtfract_total
property = current_oxygen_weight_frac_total
execute_on = timestep_end
boundary = 2
[]
[ofgain_total]
type = MaterialRealAux
variable = oxywtfgain_total
property = oxygen_weight_frac_gained_total
execute_on = timestep_end
boundary = 2
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
block = 1
[]
[]
[Contact]
[pellet_clad_mechanical]
primary = 5
secondary = 10
penalty = 1e10
formulation = penalty
normalize_penalty = false
model = frictionless
normal_smoothing_distance = 0.1
[]
[]
[ThermalContact]
[thermal_contact]
type = GasGapHeatTransfer
variable = temp
primary = 5
secondary = 10
initial_moles = initial_moles
gas_released = fission_gas_released
jump_distance_model = LANNING
plenum_pressure = plenum_pressure
contact_pressure = contact_pressure
roughness_primary = 2.0e-6
roughness_secondary = 0.5e-6
roughness_coef = 3.2
normal_smoothing_distance = 0.1
quadrature = true
emissivity_primary = 0.797698
emissivity_secondary = 0.325
refab_time = 125712000
refab_gas_types = He
refab_fractions = 1
[]
[]
[BCs]
[no_x_all]
type = DirichletBC
variable = disp_x
boundary = 12
value = 0.0
[]
[no_y_clad_bottom]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[]
[no_y_fuel_bottom]
type = DirichletBC
variable = disp_y
boundary = 20
value = 0.0
[]
[Pressure]
[coolantPressure]
boundary = '1 2 3'
function = pressure_ramp
[]
[]
[PlenumPressure]
[plenumPressure]
boundary = 9
initial_temperature = 293.15
initial_pressure = 2.60e6
startup_time = 0
R = 8.3143
output_initial_moles = initial_moles
temperature = plenum_temperature
volume = plenum_volume
material_input = fission_gas_released
output = plenum_pressure
refab_time = 125712000
refab_pressure = 0.301e6
refab_temperature = 293.15
refab_volume = 2.0e-6
[]
[]
[]
[CoolantChannel]
[convective_clad_surface]
boundary = '1 2 3'
variable = temp
inlet_temperature = temp_ramp # K
inlet_pressure = pressure_ramp # Pa
inlet_massflux = 3244.044104 # kg/m^2-sec
rod_diameter = 0.00951 # m
rod_pitch = 1.26e-2 # m
coolant_material = 'water'
compute_enthalpy = true
oxide_thickness = oxide_thickness
number_axial_zone = 50
[]
[]
[Materials]
[swelling]
type = UO2VolumetricSwellingEigenstrain
block = 3
burnup_function = burnup
initial_fuel_density = 10448.925
include_solid_swelling = true
include_densification = true
total_densification = 0.00675
initial_porosity = 0.0475
eigenstrain_name = 'fuel_volumetric_swelling_eigenstrain'
[]
[fuel_thermal]
type = UO2Thermal
block = 3
thermal_conductivity_model = NFIR
temperature = temp
burnup_function = burnup
initial_porosity = 0.0475
[]
[fuel_elastic_stress]
type = ComputeFiniteStrainElasticStress
block = 3
[]
[fuel_elasticity_tensor]
type = UO2ElasticityTensor
block = 3
[]
[fuel_thermal_expansion]
type = ComputeInstantaneousThermalExpansionFunctionEigenstrain
block = 3
stress_free_temperature = 293.15
thermal_expansion_function = Fuel_CTE_function
eigenstrain_name = 'fuel_thermal_eigenstrain'
[]
[fuel_relocation]
type = UO2RelocationEigenstrain
block = 3
burnup_function = burnup
diameter = 0.00819211 #Fuel pellet diameter in m
rod_ave_lin_pow = power_profile
axial_power_profile = axial_peaking_factors
diametral_gap =164.0e-6
burnup_relocation_stop = 0.0246
relocation_activation1 = 5000
eigenstrain_name = 'fuel_relocation_eigenstrain'
[]
[clad_thermal]
type = ZryThermal
block = 1
temperature = temp
[]
[clad_zrycreep]
type = ZryCreepLimbackHoppeUpdate
block = 1
fast_neutron_flux = fast_neutron_flux
fast_neutron_fluence = fast_neutron_fluence
zircaloy_material_type = stress_relief_annealed
max_inelastic_increment = 1.0e-4
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = 1
fast_neutron_fluence = fast_neutron_fluence
cold_work_factor = 0.5
oxygen_concentration = 0.0
matpro_poissons_ratio = false
matpro_youngs_modulus = true
[]
[clad_inelastic_stress]
type = ComputeMultipleInelasticStress
block = 1
tangent_operator = elastic
inelastic_models = 'clad_zrycreep plasticity'
[]
[clad_thermal_eigenstrain]
type = ZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 293.15
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[clad_irradiation_eigenstrain]
type = ZryIrradiationGrowthEigenstrain
block = 1
fast_neutron_fluence = fast_neutron_fluence
zircaloy_material_type = stress_relief_annealed
eigenstrain_name = 'clad_irradiation_growth_eigenstrain'
[]
[plasticity]
type = ZryPlasticityUpdate
block = 1
cold_work_factor = 0.5
fast_neutron_fluence = fast_neutron_fluence
fast_neutron_flux = fast_neutron_flux
plasticity_model_type = MATPRO
oxygen_concentration = 0.0
max_inelastic_increment = 1.0e-4
[]
[density_clad]
type = Density
block = 1
density = 6550
[]
[density_fuel]
type = Density
block = 3
[]
[fission_gas_release]
type = UO2Sifgrs
block = 3
temperature = temp
burnup_function = burnup
initial_porosity = 0.0475
grain_radius = grain_radius
gbs_model = true
transient_option = NO_TRANSIENT
[]
[ZryOxidation]
type = ZryOxidation
boundary = 2
clad_inner_radius = 0.00417806
clad_outer_radius = 0.00475336
use_coolant_channel = true
fast_neutron_flux = fast_neutron_flux
[]
[phase]
type = ZrPhase
block = 1
numerical_method = 2
[]
[strain_energy_density]
type = StrainEnergyDensity
incremental = true
[]
[]
[Dampers]
[BoundingValueNodalDamper]
type = BoundingValueNodalDamper
max_value = 3200
min_value = 200
variable = temp
[]
[contact_slip]
type = ContactSlipDamper
primary = 5
secondary = 10
min_damping_factor = 0.05
[]
[]
[Preconditioning]
[SMP]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-3
nl_max_its = 40
nl_rel_tol = 1e-4
nl_abs_tol = 1e-10
start_time = 0
end_time = 125798400
dtmax = 1e6
dtmin = 1e-7
[TimeStepper]
type = IterationAdaptiveDT
dt = 1.0e3
optimal_iterations = 100
iteration_window = 4
linear_iteration_ratio = 100
timestep_limiting_function = power_profile
max_function_change = 1e6
force_step_every_function_point = true
timestep_limiting_postprocessor = material_timestep_control
time_t = '125798410 125798420 125798430 125798440 125798450 125798460 125798470 125798480 125798500 125798500.1 125798500.2 125798500.3 125798500.32 125798500.35'
time_dt = '1 1 1 1 1 1 1 1 0.001 0.001 0.001 0.001 0.001 0.001'
[]
[Quadrature]
order = FIFTH
side_order = SEVENTH
[]
[]
[Postprocessors]
[fis_gas_grain]
type = ElementIntegralFisGasGrainSifgrs
block = 3
outputs = exodus
[]
[fis_gas_boundary]
type = ElementIntegralFisGasBoundarySifgrs
block = 3
outputs = exodus
[]
[rod_input_power]
type = FunctionValuePostprocessor
function = power_profile
[]
[burnup_GWd]
type = FunctionValuePostprocessor
function = burnup_GWd
[]
#######################################
[penetration]
type = NodalVariableValue
variable = penetration
nodeid = 5535
use_displaced_mesh = 1
[]
[contact_pressure]
type = NodalVariableValue
variable = contact_pressure
nodeid = 5535
use_displaced_mesh = 1
[]
[gap_cond]
type = ElementalVariableValue
variable = gap_cond
elementid = 1664
use_displaced_mesh = 1
[]
[creep_hoop_strain]
type = ElementalVariableValue
variable = creep_strain_zz
elementid = 376
use_displaced_mesh = 1
[]
[elastic_hoop_strain]
type = ElementalVariableValue
variable = elastic_strain_zz
elementid = 376
use_displaced_mesh = 1
[]
[plastic_hoop_strain]
type = ElementalVariableValue
variable = plastic_strain_zz
elementid = 376
use_displaced_mesh = 1
[]
[total_hoop_strain]
type = ElementalVariableValue
variable = total_hoop_strain
elementid = 376
use_displaced_mesh = 1
[]
[clad_hoop_stress]
type = ElementalVariableValue
variable = hoop_stress
elementid = 376
use_displaced_mesh = 1
[]
[clad_axial_elongation]
type = NodalVariableValue
variable = disp_y
nodeid = 2451
use_displaced_mesh = 1
[]
[clad_oxide_thickness]
type = ElementalVariableValue
variable = oxide_thickness
elementid = 376
use_displaced_mesh = 1
[]
[clad_coolant_htc]
type = ElementalVariableValue
variable = clad_coolant_htc
elementid = 376
use_displaced_mesh = 1
[]
[coolant_temp]
type = ElementalVariableValue
variable = coolant_temp
elementid = 376
use_displaced_mesh = 1
[]
[fuel_centerline_temp]
type = NodalVariableValue
variable = temp
nodeid = 5504
[]
[fuel_surface_temp]
type = NodalVariableValue
variable = temp
nodeid = 5535
[]
[clad_inner_surface_temp]
type = NodalVariableValue
variable = temp
nodeid = 1307
[]
[clad_outer_surface_temp]
type = NodalVariableValue
variable = temp
nodeid = 1317
[]
[fuel_axial_elongation]
type = NodalVariableValue
variable = disp_y
nodeid = 8055
[]
[clad_radial_elongation]
type = NodalVariableValue
variable = disp_x
nodeid = 1317
[]
[fuel_radial_elongation]
type = NodalVariableValue
variable = disp_x
nodeid = 5535
[]
[SED_PPN_O]
type = ElementalVariableValue
variable = SED
elementid = 376
use_displaced_mesh = 1
[]
[SED_PPN_I]
type = ElementalVariableValue
variable = SED
elementid = 373
use_displaced_mesh = 1
[]
[OFract_PPN_O]
type = ElementalVariableValue
variable = oxywtfract_total
elementid = 376
use_displaced_mesh = 1
[]
[OGain_PPN_O]
type = ElementalVariableValue
variable = oxywtfgain_total
elementid = 376
use_displaced_mesh = 1
[]
#######################################
[max_fuel_temp]
type = NodalExtremeValue
block = 3
variable = temp
[]
[max_clad_temp]
type = NodalExtremeValue
block = 1
variable = temp
[]
[max_clad_SED]
type = ElementExtremeValue
block = 1
variable = SED
value_type = max
[]
[RAE]
type = RadialAverageEnthalpy
vector_postprocessor = rad_temp
radial_direction = x
axial_direction = y
axial_position = 0.3
temperature_name = temp
[]
[material_timestep_control]
type = MaterialTimeStepPostprocessor
block = 1
[]
[peak_RAE]
type = TimeExtremeValue
postprocessor = RAE
[]
[]
[VectorPostprocessors]
[ox_thick]
type = SideValueSampler
variable = oxide_thickness
boundary = 2
sort_by = y
outputs = 'outfile_oxide_thickness'
[]
[rad_temp]
type = NodalValueSampler
block = 3
sort_by = y
variable = temp
execute_on = timestep_end
outputs = 'outfile_radial_temp'
[]
[]
[StandardLWRFuelRodOutputs]
fuel_pellet_blocks = 3
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
csv = true
color = true
[outfile_oxide_thickness]
type = CSV
sync_times = '125798400 125798900'
sync_only = true
[]
[outfile_radial_temp]
type = CSV
enable = false
[]
[console]
type = Console
output_linear = true
max_rows = 10
[]
[checkpoint]
type = Checkpoint
num_files = 2
file_base = recover_files
sync_times = '125798400'
sync_only = true
[]
[chkfile]
type = CSV
show = 'plenum_temperature fission_gas_released_percentage
average_centerline_fuel_temperature average_burnup peak_RAE'
execute_on = 'FINAL'
[]
[exodus]
type = Exodus
time_step_interval = 4
end_time = 125798500
[]
[exodus_RIA]
type = Exodus
time_step_interval = 2
start_time = 125798495
[]
[]
(assessment/LWR/validation/RIA_CABRI_REP_Na/analysis/REP_Na_2/REP_Na_2_RIA.i)
# REP Na 2 RIA
[GlobalParams]
density = 10344.71
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
energy_per_fission = 3.2e-11
temperature = temp
volumetric_locking_correction = false
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
acceptable_iterations = 30
acceptable_multiplier = 10
restart_file_base = 'recover_files_cp/LATEST'
[]
[Mesh]
coord_type = RZ
[smeared_pellet_mesh]
type = FuelPinMeshGenerator
clad_mesh_density = customize
pellet_mesh_density = customize
nx_p = 11
ny_p = 336
ny_cu = 3
ny_c = 350
ny_cl = 3
nx_c = 4
clad_thickness = 0.000637
pellet_outer_radius = 0.0040248
pellet_quantity = 84
pellet_height = 0.0119888
clad_top_gap_height = 0.041077
clad_bot_gap_height = 0.003
clad_gap_width = 93.0e-6
bottom_clad_height = 0.0015
top_clad_height = 0.0015
elem_type = QUAD8
[]
patch_size = 40
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temp]
[]
[]
[AuxVariables]
[fast_neutron_flux]
block = 1
[]
[fast_neutron_fluence]
block = 1
[]
[grain_radius]
block = 3
[]
[gap_cond]
order = CONSTANT
family = MONOMIAL
[]
[fuel_cond]
order = CONSTANT
family = MONOMIAL
[]
[swelling_strain]
order = CONSTANT
family = MONOMIAL
block = 3
[]
[total_hoop_strain]
order = CONSTANT
family = MONOMIAL
[]
[total_axial_strain]
order = CONSTANT
family = MONOMIAL
[]
[clad_coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[coolant_temp]
order = CONSTANT
family = MONOMIAL
[]
[clad_coolant_flux]
order = CONSTANT
family = MONOMIAL
[]
[coolant_channel_hmode]
order = CONSTANT
family = MONOMIAL
[]
[coolant_channel_htype]
order = CONSTANT
family = MONOMIAL
[]
[critical_heat_flux]
order = CONSTANT
family = MONOMIAL
[]
[oxide_thickness]
order = CONSTANT
family = MONOMIAL
[]
[SED]
order = CONSTANT
family = MONOMIAL
block = 1
[]
[oxywtfract_total]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfgain_total]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[]
[Functions]
[power_profile]
type = PiecewiseLinear
data_file = REPNa2_power_history_Full.csv
format = columns
[]
[axial_peaking_factors]
type = PiecewiseBilinear
data_file = REPNa2_axial_peaking_Full.csv
axis = 1
[]
[pressure_ramp]
type = PiecewiseLinear
xy_data = '0 101325
8640 13999808
57067200 13999808
57110400 101325
57542410 101325
57542450 500008
57542700 500008
57542800 101325
57542900 101325'
[]
[temp_ramp]
type = PiecewiseLinear
xy_data = '0 293.15
8640 543.15
57067200 543.15
57110400 293.15
57542410 293.15
57542450 553.15
57542700 553.15
57542800 293.15
57542900 293.15'
[]
[Fuel_CTE_function] #Fuel CTE as a function of temp from MATPRO data
type = PiecewiseLinear
xy_data = ' 0 1.000E-05
300 1.000E-05
350 1.000E-05
400 1.000E-05
450 1.000E-05
500 1.001E-05
550 1.002E-05
600 1.003E-05
650 1.005E-05
700 1.008E-05
750 1.011E-05
800 1.015E-05
850 1.020E-05
900 1.026E-05
950 1.032E-05
1000 1.039E-05
1050 1.046E-05
1100 1.053E-05
1150 1.061E-05
1200 1.069E-05
1250 1.077E-05
1300 1.085E-05
1350 1.094E-05
1400 1.102E-05
1450 1.111E-05
1500 1.119E-05
1550 1.127E-05
1600 1.135E-05
1650 1.143E-05
1700 1.151E-05
1750 1.158E-05
1800 1.166E-05
1850 1.173E-05
1900 1.180E-05
1950 1.187E-05
2000 1.193E-05
2050 1.199E-05
2100 1.205E-05
2150 1.211E-05
2200 1.217E-05
2250 1.222E-05
2300 1.227E-05
2350 1.232E-05
2400 1.237E-05
2450 1.242E-05
2500 1.246E-05
2550 1.250E-05
2600 1.254E-05
2650 1.258E-05
2700 1.262E-05
2750 1.265E-05
2800 1.268E-05
2850 1.271E-05
2900 1.274E-05
2950 1.277E-05
3000 1.280E-05
3050 1.282E-05
3100 1.285E-05'
[]
[burnup_GWd]
type = ParsedFunction
expression = bu*950
symbol_names = 'bu'
symbol_values = 'average_burnup'
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[fuel]
block = 3
strain = FINITE
incremental = true
eigenstrain_names = 'fuel_relocation_eigenstrain fuel_thermal_eigenstrain
fuel_volumetric_swelling_eigenstrain'
extra_vector_tags = 'ref'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz'
[]
[clad]
block = 1
strain = FINITE
incremental = true
eigenstrain_names = 'clad_irradiation_growth_eigenstrain
clad_thermal_eigenstrain'
extra_vector_tags = 'ref'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz plastic_strain_xx plastic_strain_yy plastic_strain_zz
creep_strain_xx creep_strain_yy creep_strain_zz elastic_strain_xx
elastic_strain_yy elastic_strain_zz hoop_stress'
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temp
extra_vector_tags = 'ref'
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temp
extra_vector_tags = 'ref'
[]
[heat_source_fuel]
type = NeutronHeatSource
variable = temp
block = 3
burnup_function = burnup
extra_vector_tags = 'ref'
[]
[]
[Burnup]
[burnup]
block = 3
rod_ave_lin_pow = power_profile
axial_power_profile = axial_peaking_factors
num_radial = 80
num_axial = 85
a_upper = 1.0115592
a_lower = 0.0045
fuel_inner_radius = 0
fuel_outer_radius = 0.0040248
fuel_volume_ratio = 1
isotopes = 'U235 U238 Pu239 Pu240 Pu241 Pu242'
isotope_fractions = '0.0685 0.9315 0 0 0 0'
RPF = RPF
order = CONSTANT
family = MONOMIAL
[]
[]
[AuxKernels]
[fast_neutron_flux]
type = FastNeutronFluxAux
variable = fast_neutron_flux
block = 1
axial_power_profile = axial_peaking_factors
rod_ave_lin_pow = power_profile
factor = 3e13 #n/m2-s
execute_on = timestep_begin
[]
[fast_neutron_fluence]
type = FastNeutronFluenceAux
variable = fast_neutron_fluence
fast_neutron_flux = fast_neutron_flux
block = 1
execute_on = timestep_begin
[]
[grain_radius]
type = GrainRadiusAux
block = 3
variable = grain_radius
temperature = temp
execute_on = linear
[]
[gap_conductance]
type = MaterialRealAux
property = gap_conductance
variable = gap_cond
boundary = 10
[]
[fuel_conductance]
type = MaterialRealAux
property = thermal_conductivity
variable = fuel_cond
block = 3
[]
[swelling_strain]
type = MaterialRealAux
property = volumetric_swelling_strain
variable = swelling_strain
block = 3
[]
[total_hoop_strain]
type = RankTwoScalarAux
rank_two_tensor = total_strain
variable = total_hoop_strain
scalar_type = HoopStress
execute_on = timestep_end
block = 1
[]
[total_axial_strain]
type = RankTwoScalarAux
rank_two_tensor = total_strain
variable = total_axial_strain
scalar_type = AxialStress
execute_on = timestep_end
block = 1
[]
[clad_coolant_htc]
type = MaterialRealAux
property = coolant_channel_htc
variable = clad_coolant_htc
boundary = 2
[]
[coolant_temp]
type = MaterialRealAux
property = coolant_temperature
variable = coolant_temp
boundary = 2
[]
[clad_coolant_flux]
type = MaterialRealAux
property = output_heat_flux
variable = clad_coolant_flux
boundary = 2
[]
[coolant_channel_hmode]
type = MaterialRealAux
property = coolant_channel_hmode
variable = coolant_channel_hmode
boundary = 2
[]
[coolant_channel_htype]
type = MaterialRealAux
property = coolant_channel_htype
variable = coolant_channel_htype
boundary = 2
[]
[critical_heat_flux]
type = MaterialRealAux
property = critical_heat_flux
variable = critical_heat_flux
boundary = 2
[]
[oxide]
type = MaterialRealAux
property = oxide_scale_thickness
variable = oxide_thickness
boundary = 2
[]
[SED]
type = MaterialRealAux
variable = SED
property = strain_energy_density
execute_on = timestep_end
[]
[ofract_total]
type = MaterialRealAux
variable = oxywtfract_total
property = current_oxygen_weight_frac_total
execute_on = timestep_end
boundary = 2
[]
[ofgain_total]
type = MaterialRealAux
variable = oxywtfgain_total
property = oxygen_weight_frac_gained_total
execute_on = timestep_end
boundary = 2
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
block = 1
[]
[]
[Contact]
[pellet_clad_mechanical]
primary = 5
secondary = 10
penalty = 1e10
formulation = penalty
normalize_penalty = false
model = frictionless
normal_smoothing_distance = 0.1
[]
[]
[ThermalContact]
[thermal_contact]
type = GasGapHeatTransfer
variable = temp
primary = 5
secondary = 10
initial_moles = initial_moles
gas_released = fission_gas_released
jump_distance_model = LANNING
plenum_pressure = plenum_pressure
contact_pressure = contact_pressure
roughness_primary = 2.0e-6
roughness_secondary = 0.5e-6
roughness_coef = 3.2
normal_smoothing_distance = 0.1
quadrature = true
contact_coef = 20
emissivity_primary = 1
emissivity_secondary = 1
refab_time = 57456000
refab_gas_types = He
refab_fractions = 1
[]
[]
[BCs]
[no_x_all]
type = DirichletBC
variable = disp_x
boundary = 12
value = 0.0
[]
[no_y_clad_bottom]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[]
[no_y_fuel_bottom]
type = DirichletBC
variable = disp_y
boundary = 20
value = 0.0
[]
[Pressure]
[coolantPressure]
boundary = '1 2 3'
function = pressure_ramp
[]
[]
[PlenumPressure]
[plenumPressure]
boundary = 9
initial_temperature = 293.15
initial_pressure = 1.70e6
startup_time = 0
R = 8.3143
output_initial_moles = initial_moles
temperature = plenum_temperature
volume = plenum_volume
material_input = fission_gas_released
output = plenum_pressure
refab_time = 57456000
refab_pressure = 0.1e6
refab_temperature = 293.15
refab_volume = 2.3e-6
[]
[]
[]
[CoolantChannel]
[convective_clad_surface]
boundary = '1 2 3'
variable = temp
inlet_temperature = temp_ramp # K
inlet_pressure = pressure_ramp # Pa
inlet_massflux = 3533 # kg/m^2-sec Based on flow rate provided and flow area and estimated density of 885.1 kg/m^3
flow_area = 8.74855e-5 #m^2
heated_diameter = 1.172526e-2 #m
hydraulic_diameter = 4.7e-3 #m
heated_perimeter = 2.984513e-2 #m
coolant_material = 'sodium'
compute_enthalpy = true
heat_transfer_mode = 0
#oxide_thickness = oxide_thickness # coupled oxide_thickness
number_axial_zone = 50
rod_pitch = 1.26e-2 # m
rod_diameter = 0.0095 # m
[]
[]
[Materials]
[swelling]
type = UO2VolumetricSwellingEigenstrain
block = 3
burnup_function = burnup
initial_fuel_density = 10344.71
include_solid_swelling = true
include_densification = true
total_densification = 0.00676
initial_porosity = 0.057
eigenstrain_name = 'fuel_volumetric_swelling_eigenstrain'
[]
[fuel_thermal]
type = UO2Thermal
block = 3
thermal_conductivity_model = NFIR
temperature = temp
burnup_function = burnup
initial_porosity = 0.057
[]
[fuel_elastic_stress]
type = ComputeFiniteStrainElasticStress
block = 3
[]
[fuel_elasticity_tensor]
type = UO2ElasticityTensor
block = 3
[]
[fuel_thermal_expansion]
type = ComputeInstantaneousThermalExpansionFunctionEigenstrain
block = 3
stress_free_temperature = 293.15
thermal_expansion_function = Fuel_CTE_function
eigenstrain_name = 'fuel_thermal_eigenstrain'
[]
[fuel_relocation]
type = UO2RelocationEigenstrain
block = 3
burnup_function = burnup
diameter = 0.0080496
rod_ave_lin_pow = power_profile
axial_power_profile = axial_peaking_factors
diametral_gap =186.0e-6
burnup_relocation_stop = 0.0
relocation_activation1 = 5000
eigenstrain_name = 'fuel_relocation_eigenstrain'
[]
[clad_thermal]
type = ZryThermal
block = 1
temperature = temp
[]
[clad_zrycreep]
type = ZryCreepLimbackHoppeUpdate
block = 1
fast_neutron_flux = fast_neutron_flux
fast_neutron_fluence = fast_neutron_fluence
zircaloy_material_type = stress_relief_annealed
max_inelastic_increment = 5.0e-3
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = 1
fast_neutron_fluence = fast_neutron_fluence
cold_work_factor = 0.5
oxygen_concentration = 0.00357
matpro_poissons_ratio = true
matpro_youngs_modulus = true
[]
[clad_inelastic_stress]
type = ComputeMultipleInelasticStress
block = 1
tangent_operator = elastic
inelastic_models = 'plasticity' #only use plasticity
[]
[clad_thermal_eigenstrain]
type = ZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 293.15
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[clad_irradiation_eigenstrain]
type = ZryIrradiationGrowthEigenstrain
block = 1
fast_neutron_fluence = fast_neutron_fluence
zircaloy_material_type = stress_relief_annealed
eigenstrain_name = 'clad_irradiation_growth_eigenstrain'
[]
[plasticity]
type = ZryPlasticityUpdate
block = 1
cold_work_factor = 0.5
fast_neutron_fluence = fast_neutron_fluence
fast_neutron_flux = fast_neutron_flux
plasticity_model_type = MATPRO
oxygen_concentration = 0.0
max_inelastic_increment = 5.0e-3
[]
[density_clad]
type = Density
block = 1
density = 6550
[]
[density_fuel]
type = Density
block = 3
[]
[fission_gas_release]
type = UO2Sifgrs
block = 3
temperature = temp
burnup_function = burnup
initial_porosity = 0.057
grain_radius_const = 5.0e-6
gbs_model = false
transient_option = MICROCRACKING_BURNUP
[]
[ZryOxidation]
type = ZryOxidation
boundary = 2
clad_inner_radius = 0.0041178
clad_outer_radius = 0.0047549
use_coolant_channel = true
fast_neutron_flux = fast_neutron_flux
[]
[phase]
type = ZrPhase
block = 1
numerical_method = 2
[]
[strain_energy_density]
type = StrainEnergyDensity
incremental = true
[]
[]
[Dampers]
[BoundingValueNodalDamper]
type = BoundingValueNodalDamper
max_value = 3200
min_value = 200
variable = temp
[]
[contact_slip]
type = ContactSlipDamper
primary = 5
secondary = 10
min_damping_factor = 0.05
[]
[]
[Preconditioning]
[SMP]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-3
nl_max_its = 40
nl_rel_tol = 1e-4
nl_abs_tol = 1e-10
#start_time = 0
end_time = 57542900
dtmax = 10
dtmin = 1e-7
[TimeStepper]
type = IterationAdaptiveDT
dt = 10
optimal_iterations = 20
iteration_window = 4
linear_iteration_ratio = 100
timestep_limiting_function = power_profile
max_function_change = 1e5
force_step_every_function_point = true
timestep_limiting_postprocessor = material_timestep_control
time_t = '57542410 57542420 57542430 57542440 57542450 57542460 57542470 57542480 57542500 57542500.01 57542500.02 57542500.03 57542500.04 57542500.05 57542500.06 57542500.07'
time_dt = '10 10 10 10 10 10 10 10 0.001 0.001 0.001 0.001 0.001 0.001 0.001 0.001'
[]
[Quadrature]
order = FIFTH
side_order = SEVENTH
[]
[]
[Postprocessors]
[fis_gas_grain]
type = ElementIntegralFisGasGrainSifgrs
block = 3
outputs = exodus
[]
[fis_gas_boundary]
type = ElementIntegralFisGasBoundarySifgrs
block = 3
outputs = exodus
[]
[rod_input_power]
type = FunctionValuePostprocessor
function = power_profile
[]
[burnup_GWd]
type = FunctionValuePostprocessor
function = burnup_GWd
[]
#######################################
[penetration]
type = NodalVariableValue
variable = penetration
nodeid = 11625
use_displaced_mesh = 1
[]
[contact_pressure]
type = NodalVariableValue
variable = contact_pressure
nodeid = 11625
use_displaced_mesh = 1
[]
[gap_cond]
type = ElementalVariableValue
variable = gap_cond
elementid = 3502
use_displaced_mesh = 1
[]
[creep_hoop_strain]
type = ElementalVariableValue
variable = creep_strain_zz
elementid = 780
use_displaced_mesh = 1
[]
[elastic_hoop_strain]
type = ElementalVariableValue
variable = elastic_strain_zz
elementid = 780
use_displaced_mesh = 1
[]
[plastic_hoop_strain]
type = ElementalVariableValue
variable = plastic_strain_zz
elementid = 780
use_displaced_mesh = 1
[]
[total_hoop_strain]
type = ElementalVariableValue
variable = total_hoop_strain
elementid = 780
use_displaced_mesh = 1
[]
[clad_hoop_stress]
type = ElementalVariableValue
variable = hoop_stress
elementid = 780
use_displaced_mesh = 1
[]
[clad_axial_elongation]
type = NodalVariableValue
variable = disp_y
nodeid = 5111
use_displaced_mesh = 1
[]
[clad_oxide_thickness]
type = ElementalVariableValue
variable = oxide_thickness
elementid = 780
use_displaced_mesh = 1
[]
[clad_coolant_htc]
type = ElementalVariableValue
variable = clad_coolant_htc
elementid = 780
use_displaced_mesh = 1
[]
[coolant_temp]
type = ElementalVariableValue
variable = coolant_temp
elementid = 780
use_displaced_mesh = 1
[]
[fuel_centerline_temp]
type = NodalVariableValue
variable = temp
nodeid = 11594
[]
[fuel_surface_temp]
type = NodalVariableValue
variable = temp
nodeid = 11625
[]
[clad_inner_surface_temp]
type = NodalVariableValue
variable = temp
nodeid = 2721
[]
[clad_outer_surface_temp]
type = NodalVariableValue
variable = temp
nodeid = 2731
[]
[fuel_axial_elongation]
type = NodalVariableValue
variable = disp_y
nodeid = 17015
[]
[clad_radial_elongation]
type = NodalVariableValue
variable = disp_x
nodeid = 2731
[]
[fuel_radial_elongation]
type = NodalVariableValue
variable = disp_x
nodeid = 11625
[]
[SED_PPN_O]
type = ElementalVariableValue
variable = SED
elementid = 780
use_displaced_mesh = 1
[]
[SED_PPN_I]
type = ElementalVariableValue
variable = SED
elementid = 777
use_displaced_mesh = 1
[]
[OFract_PPN_O]
type = ElementalVariableValue
variable = oxywtfract_total
elementid = 780
use_displaced_mesh = 1
[]
[OGain_PPN_O]
type = ElementalVariableValue
variable = oxywtfgain_total
elementid = 780
use_displaced_mesh = 1
[]
#######################################
[max_fuel_temp]
type = NodalExtremeValue
block = 3
variable = temp
[]
[max_clad_temp]
type = NodalExtremeValue
block = 1
variable = temp
[]
[max_clad_SED]
type = ElementExtremeValue
block = 1
variable = SED
value_type = max
[]
[RAE]
type = RadialAverageEnthalpy
vector_postprocessor = rad_temp
radial_direction = x
axial_direction = y
axial_position = 0.55
temperature_name = temp
[]
[material_timestep_control]
type = MaterialTimeStepPostprocessor
block = 1
[]
[peak_RAE]
type = TimeExtremeValue
postprocessor = RAE
[]
[]
[VectorPostprocessors]
[ox_thick]
type = SideValueSampler
variable = oxide_thickness
boundary = 2
sort_by = y
outputs = 'outfile_oxide_thickness'
[]
[rad_temp]
type = NodalValueSampler
block = 3
sort_by = y
variable = temp
execute_on = timestep_end
outputs = 'outfile_radial_temp'
[]
[]
[StandardLWRFuelRodOutputs]
fuel_pellet_blocks = 3
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
csv = true
color = true
[outfile_oxide_thickness]
type = CSV
sync_times = '57542400 57542900'
sync_only = true
[]
[outfile_radial_temp]
type = CSV
enable = false
[]
[console]
type = Console
output_linear = true
max_rows = 10
[]
[chkfile]
type = CSV
show = 'plenum_temperature fission_gas_released_percentage
average_centerline_fuel_temperature average_burnup peak_RAE'
execute_on = 'FINAL'
[]
[exodus]
type = Exodus
time_step_interval = 4
end_time = 57542500
[]
[exodus_RIA]
type = Exodus
time_step_interval = 2
start_time = 57542495
[]
[]
(assessment/LWR/validation/LOCA_REBEKA_cladding_burst_tests/analysis/rebeka_2d_06MPa/rebeka_singlerod_2d_06MPa_aniso.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
order = SECOND
family = LAGRANGE
displacements = 'disp_x disp_y'
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = rebeka_singlerod.e
[]
[]
[Variables]
[temperature]
initial_condition = 573.0
[]
[]
[Functions]
[temperature_func]
type = PiecewiseLinear
x = '0. 700. '
y = '573. 1273.' # From 300 to 1000 C at 1 K/s
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 700. '
y = '6.e+06 6.e+06' # 10 bar
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 700. '
y = '1.e+05 1.e+05' # atmospheric pressure
[]
# Circumferential steady-state creep test and analysis of Zircaloy-4 fuel cladding
# Nuclear Engineering and Design, 53, 2312-2322 (2021)
[F]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.738 0.738 0.57'
[]
[G]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.174 0.174 0.45'
[]
[H]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.588 0.588 0.48'
[]
[L]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[M]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[N]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[clad]
block = cladding
add_variables = true
strain = FINITE
decomposition_method = TaylorExpansion
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz hoop_stress'
use_automatic_differentiation = true
[]
[]
[AuxVariables]
[creep_rate_aux]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[scale_thickness]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfract_total]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfgain_total]
order = CONSTANT
family = MONOMIAL
[]
[burst_stress]
order = CONSTANT
family = MONOMIAL
[]
[burst]
order = CONSTANT
family = MONOMIAL
[]
[]
[Kernels]
[heat]
type = ADHeatConduction
variable = temperature
[]
[heat_ie]
type = ADHeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate_aux]
type = ADMaterialRealAux
variable = creep_rate_aux
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = ADMaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[scl_thickness]
type = ADMaterialRealAux
variable = scale_thickness
property = oxide_scale_thickness
boundary = 2
[]
[ofract_total]
type = ADMaterialRealAux
variable = oxywtfract_total
property = current_oxygen_weight_frac_total
boundary = 2
[]
[ofgain_total]
type = ADMaterialRealAux
boundary = 2
variable = oxywtfgain_total
property = oxygen_weight_frac_gained_total
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = 2
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = 2
execute_on = timestep_end
[]
[]
[BCs]
[inner_temperature]
type = REBEKADirichletBC
variable = temperature
function_tempm = temperature_func
minimum_temperature = 573.
translation = 0.1625
boundary = 4
[]
[no_y_midsection]
type = ADDirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply steam pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 101 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[CoolantChannel]
[convective_clad_surface]
boundary = 2
variable = temperature
inlet_temperature = 473.
inlet_pressure = 1.e+05
inlet_massflux = 1.0 # kg/m^2-sec # almost stagnant steam
rod_diameter = 10.75e-03
rod_pitch = 1.26e-02 # default
oxide_thickness = scale_thickness
number_axial_zone = 15
use_ad = true
[]
[]
[Materials]
[converter]
type = MaterialADConverter
reg_props_in = 'fract_beta_phase'
ad_props_out = 'ad_fract_beta_phase'
[]
[thermal]
type = ADZryThermal
block = cladding
temperature = temperature
[]
[clad_elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
block = cladding
youngs_modulus = 1.0e11
poissons_ratio = 0.3
[]
[clad_stress]
type = ADComputeMultipleInelasticStress
inelastic_models = 'clad_zrycreep'
block = cladding
[]
[hill_constants]
type = ADHillConstants
hill_constants = "0.738 0.174 0.588 1.0 1.0 1.0"
function_names = "F G H L M N"
temperature = temperature
[]
[clad_zrycreep]
type = ADZryAnisoCreepLOCAUpdate
block = cladding
temperature = temperature
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
temperature_loca_creep_begin = 501
temperature_standard_thermal_creep_end = 500
fract_beta_phase_name = 'ad_fract_beta_phase'
[]
[thermal_expansion]
type = ADZryThermalExpansionMATPROEigenstrain
block = cladding
temperature = temperature
stress_free_temperature = 573.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[density]
type = ADDensity
block = cladding
[]
[phase]
type = ZrPhase
block = cladding
temperature = temperature
numerical_method = 2
[]
[oxidation]
type = ADZryOxidation
boundary = 2
temperature = temperature
clad_inner_radius = 0.00465
clad_outer_radius = 0.005375
normal_operating_temperature_model = epri_kwu_ce
high_temperature_model = leistikow
use_coolant_channel = true
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = 2
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate_aux
temperature = temperature
fraction_beta_phase = fract_beta_phase
fraction_oxygen_gain = oxywtfgain_total
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-06
nl_abs_tol = 1.e-08
start_time = 0
n_startup_steps = 1
end_time = 700.
dtmax = 1.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[Postprocessors]
[ave_clad_exterior_temp]
type = SideAverageValue
boundary = 2
variable = temperature
[]
[max_clad_temp]
type = NodalExtremeValue
block = cladding
value_type = max
variable = temperature
[]
[min_clad_temp]
type = NodalExtremeValue
block = cladding
value_type = min
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = cladding
[]
[max_oxygen_fract]
type = ElementExtremeValue
block = cladding
value_type = max
variable = oxywtfract_total
[]
[max_betaph_fract]
type = ElementExtremeValue
block = cladding
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
block = cladding
value_type = max
variable = creep_rate_aux
[]
[max_creep_strain_mag]
type = ElementExtremeValue
block = cladding
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
block = cladding
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
block = cladding
value_type = max
variable = hoop_stress
[]
[vonmises_stress_clad]
type = ElementAverageValue
block = cladding
variable = vonmises_stress
[]
[min_burst_stress]
type = ElementExtremeValue
block = cladding
value_type = min
variable = burst_stress
[]
[burst]
type = ElementExtremeValue
block = cladding
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = cladding
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[top_disp_r_clad] # this is mid height
type = NodalVariableValue
variable = disp_x
nodeid = 0 #coords (0.005375, 0.1625)
[]
[top_disp_r_clad_slice] # this is mid height matched to the 1.5d
type = NodalVariableValue
variable = disp_x
nodeid = 3 #coords (0.005375, 0.1625)
[]
[top_disp_z_clad]
type = NodalVariableValue
variable = disp_y
nodeid = 0 #coords (0.005375, 0.1625)
[]
[stress_xx] # stess in the top Element
type = ElementalVariableValue
variable = stress_xx
elementid = 0
[]
[stress_yy] # stess in the top Element
type = ElementalVariableValue
variable = stress_yy
elementid = 0
[]
[stress_zz] # stess in the top Element
type = ElementalVariableValue
variable = stress_zz
elementid = 0
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = cladding
plenum_boundary_name = 4
external_clad_boundary_name = 2
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = rebeka_2d_06MPa_aniso_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
(assessment/LWR/validation/LOCA_REBEKA_cladding_burst_tests/analysis/rebeka_2d_04MPa/rebeka_singlerod_2d_04MPa_aniso.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
order = SECOND
family = LAGRANGE
displacements = 'disp_x disp_y'
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = rebeka_singlerod.e
[]
[]
[Variables]
[temperature]
initial_condition = 573.0
[]
[]
[Functions]
[temperature_func]
type = PiecewiseLinear
x = '0. 700. '
y = '573. 1273.' # From 300 to 1000 C at 1 K/s
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 700. '
y = '4.e+06 4.e+06' # 10 bar
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 700. '
y = '1.e+05 1.e+05' # atmospheric pressure
[]
# Circumferential steady-state creep test and analysis of Zircaloy-4 fuel cladding
# Nuclear Engineering and Design, 53, 2312-2322 (2021)
[F]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.738 0.738 0.57'
[]
[G]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.174 0.174 0.45'
[]
[H]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.588 0.588 0.48'
[]
[L]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[M]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[N]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[clad]
block = cladding
add_variables = true
strain = FINITE
decomposition_method = TaylorExpansion
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz hoop_stress'
use_automatic_differentiation = true
[]
[]
[AuxVariables]
[creep_rate_aux]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[scale_thickness]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfract_total]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfgain_total]
order = CONSTANT
family = MONOMIAL
[]
[burst_stress]
order = CONSTANT
family = MONOMIAL
[]
[burst]
order = CONSTANT
family = MONOMIAL
[]
[]
[Kernels]
[heat]
type = ADHeatConduction
variable = temperature
[]
[heat_ie]
type = ADHeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate_aux]
type = ADMaterialRealAux
variable = creep_rate_aux
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = ADMaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = ADMaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[scl_thickness]
type = ADMaterialRealAux
variable = scale_thickness
property = oxide_scale_thickness
boundary = 2
[]
[ofract_total]
type = ADMaterialRealAux
variable = oxywtfract_total
property = current_oxygen_weight_frac_total
boundary = 2
[]
[ofgain_total]
type = ADMaterialRealAux
boundary = 2
variable = oxywtfgain_total
property = oxygen_weight_frac_gained_total
[]
[sigmaburst]
type = ADMaterialRealAux
variable = burst_stress
property = burst_stress
boundary = 2
[]
[hasburst]
type = ADMaterialRealAux
variable = burst
property = failed
boundary = 2
execute_on = timestep_end
[]
[]
[BCs]
[inner_temperature]
type = REBEKADirichletBC
variable = temperature
function_tempm = temperature_func
minimum_temperature = 573.
translation = 0.1625
boundary = 4
[]
[no_y_midsection]
type = ADDirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply steam pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 101 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[CoolantChannel]
[convective_clad_surface]
boundary = 2
variable = temperature
inlet_temperature = 473.
inlet_pressure = 1.e+05
inlet_massflux = 1.0 # kg/m^2-sec # almost stagnant steam
rod_diameter = 10.75e-03
rod_pitch = 1.26e-02 # default
oxide_thickness = scale_thickness
number_axial_zone = 15
use_ad = true
[]
[]
[Materials]
[thermal]
type = ADZryThermal
block = cladding
temperature = temperature
[]
[clad_elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
block = cladding
youngs_modulus = 1.0e11
poissons_ratio = 0.3
[]
[clad_stress]
type = ADComputeMultipleInelasticStress
inelastic_models = 'clad_zrycreep'
block = cladding
[]
[hill_constants]
type = ADHillConstants
hill_constants = "0.738 0.174 0.588 1.0 1.0 1.0"
function_names = "F G H L M N"
temperature = temperature
[]
[clad_zrycreep]
type = ADZryAnisoCreepLOCAUpdate
block = cladding
temperature = temperature
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
temperature_loca_creep_begin = 501
temperature_standard_thermal_creep_end = 500
fract_beta_phase_name = 'fract_beta_phase'
[]
[thermal_expansion]
type = ADZryThermalExpansionMATPROEigenstrain
block = cladding
temperature = temperature
stress_free_temperature = 573.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[density]
type = ADDensity
block = cladding
[]
[phase]
type = ADZrPhase
block = cladding
temperature = temperature
numerical_method = 2
[]
[oxidation]
type = ADZryOxidation
boundary = 2
temperature = temperature
clad_inner_radius = 0.00465
clad_outer_radius = 0.005375
normal_operating_temperature_model = epri_kwu_ce
high_temperature_model = leistikow
use_coolant_channel = true
[]
[clad_failure_criterion]
type = ADZryCladdingFailure
boundary = 2
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate_aux
temperature = temperature
fraction_beta_phase = fract_beta_phase
fraction_oxygen_gain = oxywtfgain_total
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = NEWTON
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-06
nl_abs_tol = 1.e-08
start_time = 0
n_startup_steps = 1
end_time = 700.
dtmax = 1.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[Postprocessors]
[ave_clad_exterior_temp]
type = SideAverageValue
boundary = 2
variable = temperature
[]
[max_clad_temp]
type = NodalExtremeValue
block = cladding
value_type = max
variable = temperature
[]
[min_clad_temp]
type = NodalExtremeValue
block = cladding
value_type = min
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = cladding
[]
[max_oxygen_fract]
type = ElementExtremeValue
block = cladding
value_type = max
variable = oxywtfract_total
[]
[max_betaph_fract]
type = ElementExtremeValue
block = cladding
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
block = cladding
value_type = max
variable = creep_rate_aux
[]
[max_creep_strain_mag]
type = ElementExtremeValue
block = cladding
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
block = cladding
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
block = cladding
value_type = max
variable = hoop_stress
[]
[vonmises_stress_clad]
type = ElementAverageValue
block = cladding
variable = vonmises_stress
[]
[min_burst_stress]
type = ElementExtremeValue
block = cladding
value_type = min
variable = burst_stress
[]
[burst]
type = ElementExtremeValue
block = cladding
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = cladding
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[top_disp_r_clad] # this is mid height
type = NodalVariableValue
variable = disp_x
nodeid = 0 #coords (0.005375, 0.1625)
[]
[top_disp_r_clad_slice] # this is mid height matched to the 1.5d
type = NodalVariableValue
variable = disp_x
nodeid = 3 #coords (0.005375, 0.1625)
[]
[top_disp_z_clad]
type = NodalVariableValue
variable = disp_y
nodeid = 0 #coords (0.005375, 0.1625)
[]
[stress_xx] # stess in the top Element
type = ElementalVariableValue
variable = stress_xx
elementid = 0
[]
[stress_yy] # stess in the top Element
type = ElementalVariableValue
variable = stress_yy
elementid = 0
[]
[stress_zz] # stess in the top Element
type = ElementalVariableValue
variable = stress_zz
elementid = 0
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = cladding
plenum_boundary_name = 4
external_clad_boundary_name = 2
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = rebeka_2d_04MPa_aniso_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
(test/tests/zry_oxidation_cladding/zryoxidation_pingeo.i)
# This test demonstrates the usage of the model for cladding oxidation from
# normal operating to high temperature (accident) conditions, through the
# epri_kwu_ce, Leistikow, and Prater relations.
#
# The purpose of this test is to run zryoxidation.i while using FuelPinGeometry
# and then exodiff against the non-FuelPinGeometry version
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Mesh]
coord_type = RZ
[smeared_pellet_mesh]
type = FuelPinMeshGenerator
include_fuel = false
pellet_quantity = 1
pellet_height = 0.011143
pellet_outer_radius = 4.57e-3
clad_mesh_density = coarse
clad_gap_width = 70.0e-6
clad_thickness = 0.735e-3
clad_bot_gap_height = 1.0e-3
bottom_clad_height = 2.5e-3
top_clad_height = 2.5e-3
clad_top_gap_height = 5.0e-3
elem_type = QUAD4
[]
patch_size = 10
patch_update_strategy = iteration
partitioner = centroid
centroid_partitioner_direction = y
[]
[Functions]
[Temp_func]
type = PiecewiseLinear
x = '0.0 100000000.0 100000010.0 100000100.0 100000110.0 100000200.0 100000210.0 100000300.0'
y = '600.0 600.0 1100.0 1100.0 1850.0 1850.0 1950.0 1950.0 '
[]
[FNFlux_func]
type = PiecewiseLinear
x = '0.0 100000300.0'
y = '1.0e+17 1.0e+17 '
[]
[]
[Variables]
[temp]
order = FIRST
family = LAGRANGE
initial_condition = 600.0
[]
[disp_x]
order = FIRST
family = LAGRANGE
[]
[disp_y]
order = FIRST
family = LAGRANGE
[]
[]
[AuxVariables]
[fast_neutron_flux]
order = FIRST
family = LAGRANGE
initial_condition = 1.0e+17
[]
[scale_thickness] # ZrO2 scale thickness (m)
order = CONSTANT
family = MONOMIAL
[]
[oxyconc2_scale] # Oxygen concentration in ZrO2 scale (kg/m**2)
order = CONSTANT
family = MONOMIAL
[]
[oxyconc2_metal] # Oxygen concentration in metal (kg/m**2)
order = CONSTANT
family = MONOMIAL
[]
[oxyconc2_total] # Total oxygen concentration (oxide + metal) (kg/m**2)
order = CONSTANT
family = MONOMIAL
[]
[oxywtfract_metal] # Oxygen weight fraction in metal (/)
order = CONSTANT
family = MONOMIAL
[]
[oxywtfract_total] # Total oxygen weight fraction (oxide+metal) (/)
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[all]
strain = finite
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temp
[]
[]
[AuxKernels]
[fnflux]
type = FastNeutronFluxAux
variable = fast_neutron_flux
block = 1
function = FNFlux_func
execute_on = timestep_begin
[]
[scl_thickness]
type = MaterialRealAux
variable = scale_thickness
property = oxide_scale_thickness
boundary = 1
[]
[oconc_scale]
type = MaterialRealAux
variable = oxyconc2_scale
property = gained_oxygen_concentration_scale
boundary = 1
[]
[oconc_metal]
type = MaterialRealAux
variable = oxyconc2_metal
property = gained_oxygen_concentration_metal_wall
boundary = 1
[]
[oconc_total]
type = MaterialRealAux
variable = oxyconc2_total
property = gained_oxygen_concentration_total
boundary = 1
[]
[ofract_metal]
type = MaterialRealAux
variable = oxywtfract_metal
property = current_oxygen_weight_frac_metal_wall
boundary = 1
[]
[ofract_total]
type = MaterialRealAux
variable = oxywtfract_total
property = current_oxygen_weight_frac_total
boundary = 1
[]
[]
[BCs]
[bottom_T]
type = FunctionDirichletBC
variable = temp
function = Temp_func
boundary = 1
[]
[x_disp]
type = DirichletBC
variable = disp_x
value = 0
boundary = 1
[]
[y_disp]
type = DirichletBC
variable = disp_y
value = 0
boundary = 2
[]
[]
[Materials]
[elasticity_tensor]
type = ZryElasticityTensor
block = 1
[]
[stress]
type = ComputeFiniteStrainElasticStress
block = 1
[]
[thermal]
type = ZryThermal
block = 1
temperature = temp
[]
[oxidation_zry]
type = ZryOxidation
boundary = 1
normal_operating_temperature_model = epri_kwu_ce
high_temperature_model = leistikow
temperature = temp
fast_neutron_flux = fast_neutron_flux
fuel_pin_geometry = pin_geometry
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = 'lu superlu_dist'
l_tol = 1.0e-08
nl_abs_tol = 1.0e-08
nl_rel_tol = 1.0e-08
start_time = 0.0
num_steps = 5000
end_time = 100000300
[TimeStepper]
type = IterationAdaptiveDT
dt = 1.0e+06
optimal_iterations = 6
iteration_window = 2
linear_iteration_ratio = 100
time_t = '0.0 100000000.0'
time_dt = '1.e+06 10.0 '
growth_factor = 1.0
[]
[]
[Postprocessors]
[_dt]
type = TimestepSize
[]
[temp]
type = NodalVariableValue
variable = temp
nodeid = 0
execute_on = 'initial timestep_end'
[]
[scale_thickness]
type = ElementalVariableValue
elementid = 0
variable = scale_thickness
[]
[oxyconc2_scale]
type = ElementalVariableValue
elementid = 0
variable = oxyconc2_scale
[]
[oxyconc2_metal]
type = ElementalVariableValue
elementid = 0
variable = oxyconc2_metal
[]
[oxyconc2_total]
type = ElementalVariableValue
elementid = 0
variable = oxyconc2_total
[]
[oxywtfract_metal]
type = ElementalVariableValue
elementid = 0
variable = oxywtfract_metal
[]
[oxywtfract_total]
type = ElementalVariableValue
elementid = 0
variable = oxywtfract_total
[]
[]
[Outputs]
file_base = zryoxidation_out
exodus = true
[]
[UserObjects]
[pin_geometry]
type = FuelPinGeometry
include_fuel = false
[]
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-21/puzry-21.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-21.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 4000. '
y = '1.e+05 1.e+05 5.14e+06' # Linear increase at 0.0168 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 4000. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = EigenSolution
[]
[]
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = MaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = FunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = DirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = DirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1.e+11
poissons_ratio = 0.3
block = 1
[]
[creep_update]
type = ZryCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 1.e-04
temperature = temperature
temperature_standard_thermal_creep_end = 700
temperature_loca_creep_begin = 900.
[]
[creep]
type = ComputeMultipleInelasticStress
block = 1
tangent_operator = elastic
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = Density
block = 1
[]
[phase]
type = ZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
active = 'smp'
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0.
n_startup_steps = 1
end_time = 4000.
dtmax = 1.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-21_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/LOCA_Hardy_cladding_test/analysis/1pt4MPa/25C_sec/25C_sec_Hardy_Tube_Test_1pt4MPa.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
volumetric_locking_correction = false
displacements = 'disp_x disp_y'
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
group_variables = 'disp_x disp_y'
[]
[Mesh]
coord_type = RZ
patch_size = 10
patch_update_strategy = iteration
partitioner = centroid
centroid_partitioner_direction = y
[gen]
type = FuelPinMeshGenerator
include_fuel = false
include_clad = true
pellet_outer_radius = 0.0072527
clad_gap_width = 0.0
clad_top_gap_height = 0.0
clad_bot_gap_height = 0.0
clad_thickness = 0.38e-3
pellet_height = 0.5
pellet_quantity = 1
clad_mesh_density = customize
nx_c = 2
ny_c = 50
elem_type = QUAD8
[]
[]
[Variables]
[temperature]
initial_condition = 600.0
[]
[]
[AuxVariables]
[creep_rate_aux]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[total_hoop_strain]
order = CONSTANT
family = MONOMIAL
[]
[burst_stress]
order = CONSTANT
family = MONOMIAL
[]
[burst]
order = CONSTANT
family = MONOMIAL
[]
[]
[Functions]
[pressure_function]
type = PiecewiseLinear
x = '0 40'
y = '1 1'
[]
[temp_function]
type = PiecewiseLinear
y = '600 1600'
[]
[temperature_profile]
type = PiecewiseBilinear
y = '0 40'
x = '0 0.25224 0.50448'
z = '0.995 1.01 0.995 0.995 1.01 0.995'
axis = 1
[]
[inner_temperature]
type = CompositeFunction
functions = 'temp_function temperature_profile'
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[clad]
block = clad
add_variables = true
strain = FINITE
decomposition_method = EigenSolution
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz elastic_strain_xx elastic_strain_yy elastic_strain_zz
creep_strain_xx creep_strain_yy creep_strain_zz hoop_stress'
extra_vector_tags = 'ref'
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
extra_vector_tags = 'ref'
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
extra_vector_tags = 'ref'
[]
[]
[AuxKernels]
[creep_rate_aux]
type = MaterialRealAux
variable = creep_rate_aux
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[creep_rate]
type = MaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[total_hoop_strain]
type = RankTwoAux
rank_two_tensor = total_strain
variable = total_hoop_strain
index_i = 2
index_j = 2
execute_on = timestep_end
block = clad
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = clad_outside_right
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = clad_outside_right
execute_on = timestep_end
[]
[]
[BCs]
[Pressure]
[outer_surface]
boundary = 'clad_outside_bottom clad_outside_right clad_outside_top'
factor = 0.0
function = pressure_function
[]
[inner_surface]
boundary = 'clad_inside_right clad_inside_bottom clad_inside_top'
function = pressure_function
[]
[]
[u_bottom_fix]
type = DirichletBC
variable = disp_y
boundary = 1001
value = 0.0
[]
[x_fix]
type = DirichletBC
variable = disp_x
boundary = centerline
value = 0.0
[]
[temp_bc]
type = FunctionDirichletBC
function = inner_temperature
variable = temperature
boundary = 'clad_inside_bottom clad_inside_right clad_inside_top'
[]
[]
[Materials]
[clad_thermal]
type = ZryThermal
block = clad
zry_thermal_properties_model = MATPRO
temperature = temperature
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = clad
matpro_youngs_modulus = true
matpro_poissons_ratio = true
temperature = temperature
[]
[clad_stress]
type = ComputeMultipleInelasticStress
inelastic_models = 'clad_zrycreep'
block = clad
tangent_operator = nonlinear
[]
[clad_zrycreep]
type = ZryCreepLOCAUpdate
block = clad
temperature = temperature
model_irradiation_creep = false
model_primary_creep = true
model_thermal_creep = true
temperature_loca_creep_begin = 840 # values from the report
temperature_standard_thermal_creep_end = 975
[]
[thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = clad
temperature = temperature
stress_free_temperature = 600.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[clad_density]
type = Density
block = clad
density = 6550.0
[]
[phase]
type = ZrPhase
block = clad
temperature = temperature
numerical_method = 2
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = clad_outside_right
failure_criterion = combined_overstress_and_overstrain
hoop_stress = hoop_stress
hoop_creep_strain = creep_strain_zz
effective_strain_rate_creep = creep_rate_aux
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.0e-5
nl_abs_tol = 1.0e-8
start_time = 0
n_startup_steps = 1
end_time = 40
dtmax = 1
dtmin = 0.0000001
[TimeStepper]
type = IterationAdaptiveDT
timestep_limiting_postprocessor = material_timestep
dt = 1.0
[]
[]
[Postprocessors]
[ave_clad_temp]
type = SideAverageValue
boundary = clad_outside_right
variable = temperature
[]
[gas_volume]
type = InternalVolume
boundary = all_clad_interior
execute_on = 'initial linear'
[]
[max_clad_temp]
type = NodalExtremeValue
block = clad
value_type = max
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = clad
[]
[max_hoop_stress]
type = ElementExtremeValue
block = clad
value_type = max
variable = hoop_stress
[]
[vonmises_stress_clad]
type = ElementAverageValue
block = clad
variable = vonmises_stress
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = total_hoop_strain
[]
[max_disp_x]
type = NodalExtremeValue
block = clad
value_type = max
variable = disp_x
[]
[min_burst_stress]
type = ElementExtremeValue
block = clad
value_type = min
variable = burst_stress
[]
[burst]
type = ElementExtremeValue
block = clad
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = clad
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
[]
[PerformanceMetricOutputs]
[]
[Outputs]
color = false
perf_graph = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[csv]
type = CSV
[]
[chkfile]
type = CSV
show = 'max_disp_x max_hoop_stress vonmises_stress_clad'
execute_on = 'FINAL'
[]
[]
[UserObjects]
[terminator1]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '5'
include_fuel = false
[]
[]
(assessment/LWR/validation/LOCA_Hardy_cladding_test/analysis/0pt7MPa/25C_sec/25C_sec_Hardy_Tube_Test_0pt7MPa.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
volumetric_locking_correction = false
displacements = 'disp_x disp_y'
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
group_variables = 'disp_x disp_y'
[]
[Mesh]
coord_type = RZ
patch_size = 10
patch_update_strategy = iteration
partitioner = centroid
centroid_partitioner_direction = y
[gen]
type = FuelPinMeshGenerator
include_fuel = false
include_clad = true
pellet_outer_radius = 0.0072527
clad_gap_width = 0.0
clad_top_gap_height = 0.0
clad_bot_gap_height = 0.0
clad_thickness = 0.38e-3
pellet_height = 0.5
pellet_quantity = 1
clad_mesh_density = customize
nx_c = 2
ny_c = 50
elem_type = QUAD8
[]
[]
[Variables]
[temperature]
initial_condition = 600.0
[]
[]
[AuxVariables]
[creep_rate_aux]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[total_hoop_strain]
order = CONSTANT
family = MONOMIAL
[]
[burst_stress]
order = CONSTANT
family = MONOMIAL
[]
[burst]
order = CONSTANT
family = MONOMIAL
[]
[]
[Functions]
[pressure_function]
type = PiecewiseLinear
x = '0 40'
y = '1 1'
[]
[temp_function]
type = PiecewiseLinear
y = '600 1600'
[]
[temperature_profile]
type = PiecewiseBilinear
y = '0 40'
x = '0 0.25224 0.50448'
z = '0.995 1.01 0.995 0.995 1.01 0.995'
axis = 1
[]
[inner_temperature]
type = CompositeFunction
functions = 'temp_function temperature_profile'
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[clad]
block = clad
add_variables = true
strain = FINITE
decomposition_method = EigenSolution
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz elastic_strain_xx elastic_strain_yy elastic_strain_zz
creep_strain_xx creep_strain_yy creep_strain_zz hoop_stress'
extra_vector_tags = 'ref'
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
extra_vector_tags = 'ref'
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
extra_vector_tags = 'ref'
[]
[]
[AuxKernels]
[creep_rate_aux]
type = MaterialRealAux
variable = creep_rate_aux
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[creep_rate]
type = MaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[total_hoop_strain]
type = RankTwoAux
rank_two_tensor = total_strain
variable = total_hoop_strain
index_i = 2
index_j = 2
execute_on = timestep_end
block = clad
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = clad_outside_right
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = clad_outside_right
execute_on = timestep_end
[]
[]
[BCs]
[Pressure]
[outer_surface]
boundary = 'clad_outside_bottom clad_outside_right clad_outside_top'
factor = 0.0
function = pressure_function
[]
[inner_surface]
boundary = 'clad_inside_right clad_inside_bottom clad_inside_top'
function = pressure_function
[]
[]
[u_bottom_fix]
type = DirichletBC
variable = disp_y
boundary = 1001
value = 0.0
[]
[x_fix]
type = DirichletBC
variable = disp_x
boundary = centerline
value = 0.0
[]
[temp_bc]
type = FunctionDirichletBC
function = inner_temperature
variable = temperature
boundary = 'clad_inside_bottom clad_inside_right clad_inside_top'
[]
[]
[Materials]
[clad_thermal]
type = ZryThermal
block = clad
zry_thermal_properties_model = MATPRO
temperature = temperature
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = clad
matpro_youngs_modulus = true
matpro_poissons_ratio = true
temperature = temperature
[]
[clad_stress]
type = ComputeMultipleInelasticStress
inelastic_models = 'clad_zrycreep'
block = clad
tangent_operator = nonlinear
[]
[clad_zrycreep]
type = ZryCreepLOCAUpdate
block = clad
temperature = temperature
model_irradiation_creep = false
model_primary_creep = true
model_thermal_creep = true
temperature_loca_creep_begin = 840 # values from the report
temperature_standard_thermal_creep_end = 975
[]
[thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = clad
temperature = temperature
stress_free_temperature = 600.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[clad_density]
type = Density
block = clad
density = 6550.0
[]
[phase]
type = ZrPhase
block = clad
temperature = temperature
numerical_method = 2
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = clad_outside_right
failure_criterion = combined_overstress_and_overstrain
hoop_stress = hoop_stress
hoop_creep_strain = creep_strain_zz
effective_strain_rate_creep = creep_rate_aux
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.0e-5
nl_abs_tol = 1.0e-8
start_time = 0
n_startup_steps = 1
end_time = 40
dtmax = 1
dtmin = 0.0000001
[TimeStepper]
type = IterationAdaptiveDT
timestep_limiting_postprocessor = material_timestep
dt = 1.0
[]
[]
[Postprocessors]
[ave_clad_temp]
type = SideAverageValue
boundary = clad_outside_right
variable = temperature
[]
[gas_volume]
type = InternalVolume
boundary = all_clad_interior
execute_on = 'initial linear'
[]
[max_clad_temp]
type = NodalExtremeValue
block = clad
value_type = max
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = clad
[]
[max_hoop_stress]
type = ElementExtremeValue
block = clad
value_type = max
variable = hoop_stress
[]
[vonmises_stress_clad]
type = ElementAverageValue
block = clad
variable = vonmises_stress
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = total_hoop_strain
[]
[max_disp_x]
type = NodalExtremeValue
block = clad
value_type = max
variable = disp_x
[]
[min_burst_stress]
type = ElementExtremeValue
block = clad
value_type = min
variable = burst_stress
[]
[burst]
type = ElementExtremeValue
block = clad
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = clad
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
[]
[PerformanceMetricOutputs]
[]
[Outputs]
color = false
perf_graph = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[csv]
type = CSV
[]
[chkfile]
type = CSV
show = 'max_disp_x max_hoop_stress vonmises_stress_clad'
execute_on = 'FINAL'
[]
[]
[UserObjects]
[terminator1]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '5'
include_fuel = false
[]
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-29/puzry-29.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-29.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 2000. '
y = '1.e+05 1.e+05 7.3e+06' # Linear increase at 0.0720 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 2000. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = EigenSolution
[]
[]
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = MaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = FunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = DirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = DirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1.e+11
poissons_ratio = 0.3
block = 1
[]
[creep_update]
type = ZryCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 1.e-04
temperature = temperature
temperature_standard_thermal_creep_end = 700
temperature_loca_creep_begin = 900.
[]
[creep]
type = ComputeMultipleInelasticStress
block = 1
tangent_operator = elastic
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = Density
block = 1
[]
[phase]
type = ZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
active = 'smp'
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0.
n_startup_steps = 1
end_time = 2000.
dtmax = 1.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-29_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/LOCA_Hardy_cladding_test/analysis/2pt1MPa/100C_sec/100C_sec_Hardy_Tube_Test_2pt1MPa.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
volumetric_locking_correction = false
displacements = 'disp_x disp_y'
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
group_variables = 'disp_x disp_y'
[]
[Mesh]
coord_type = RZ
patch_size = 10
patch_update_strategy = iteration
partitioner = centroid
centroid_partitioner_direction = y
[gen]
type = FuelPinMeshGenerator
include_fuel = false
include_clad = true
pellet_outer_radius = 0.0072527
clad_gap_width = 0.0
clad_top_gap_height = 0.0
clad_bot_gap_height = 0.0
clad_thickness = 0.38e-3
pellet_height = 0.5
pellet_quantity = 1
clad_mesh_density = customize
nx_c = 2
ny_c = 50
elem_type = QUAD8
[]
[]
[Variables]
[temperature]
initial_condition = 600.0
[]
[]
[AuxVariables]
[creep_rate_aux]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[total_hoop_strain]
order = CONSTANT
family = MONOMIAL
[]
[burst_stress]
order = CONSTANT
family = MONOMIAL
[]
[burst]
order = CONSTANT
family = MONOMIAL
[]
[]
[Functions]
[pressure_function]
type = PiecewiseLinear
x = '0 40'
y = '1 1'
[]
[temp_function]
type = PiecewiseLinear
y = '600 1600'
[]
[temperature_profile]
type = PiecewiseBilinear
y = '0 40'
x = '0 0.25224 0.50448'
z = '0.995 1.01 0.995 0.995 1.01 0.995'
axis = 1
[]
[inner_temperature]
type = CompositeFunction
functions = 'temp_function temperature_profile'
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[clad]
block = clad
add_variables = true
strain = FINITE
decomposition_method = EigenSolution
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz elastic_strain_xx elastic_strain_yy elastic_strain_zz
creep_strain_xx creep_strain_yy creep_strain_zz hoop_stress'
extra_vector_tags = 'ref'
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
extra_vector_tags = 'ref'
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
extra_vector_tags = 'ref'
[]
[]
[AuxKernels]
[creep_rate_aux]
type = MaterialRealAux
variable = creep_rate_aux
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[creep_rate]
type = MaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[total_hoop_strain]
type = RankTwoAux
rank_two_tensor = total_strain
variable = total_hoop_strain
index_i = 2
index_j = 2
execute_on = timestep_end
block = clad
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = clad_outside_right
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = clad_outside_right
execute_on = timestep_end
[]
[]
[BCs]
[Pressure]
[outer_surface]
boundary = 'clad_outside_bottom clad_outside_right clad_outside_top'
factor = 0.0
function = pressure_function
[]
[inner_surface]
boundary = 'clad_inside_right clad_inside_bottom clad_inside_top'
function = pressure_function
[]
[]
[u_bottom_fix]
type = DirichletBC
variable = disp_y
boundary = 1001
value = 0.0
[]
[x_fix]
type = DirichletBC
variable = disp_x
boundary = centerline
value = 0.0
[]
[temp_bc]
type = FunctionDirichletBC
function = inner_temperature
variable = temperature
boundary = 'clad_inside_bottom clad_inside_right clad_inside_top'
[]
[]
[Materials]
[clad_thermal]
type = ZryThermal
block = clad
zry_thermal_properties_model = MATPRO
temperature = temperature
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = clad
matpro_youngs_modulus = true
matpro_poissons_ratio = true
temperature = temperature
[]
[clad_stress]
type = ComputeMultipleInelasticStress
inelastic_models = 'clad_zrycreep'
block = clad
tangent_operator = nonlinear
[]
[clad_zrycreep]
type = ZryCreepLOCAUpdate
block = clad
temperature = temperature
model_irradiation_creep = false
model_primary_creep = true
model_thermal_creep = true
temperature_loca_creep_begin = 840 # values from the report
temperature_standard_thermal_creep_end = 975
[]
[thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = clad
temperature = temperature
stress_free_temperature = 600.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[clad_density]
type = Density
block = clad
density = 6550.0
[]
[phase]
type = ZrPhase
block = clad
temperature = temperature
numerical_method = 2
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = clad_outside_right
failure_criterion = combined_overstress_and_overstrain
hoop_stress = hoop_stress
hoop_creep_strain = creep_strain_zz
effective_strain_rate_creep = creep_rate_aux
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.0e-5
nl_abs_tol = 1.0e-8
start_time = 0
n_startup_steps = 1
end_time = 40
dtmax = 1
dtmin = 0.0000001
[TimeStepper]
type = IterationAdaptiveDT
timestep_limiting_postprocessor = material_timestep
dt = 1.0
[]
[]
[Postprocessors]
[ave_clad_temp]
type = SideAverageValue
boundary = clad_outside_right
variable = temperature
[]
[gas_volume]
type = InternalVolume
boundary = all_clad_interior
execute_on = 'initial linear'
[]
[max_clad_temp]
type = NodalExtremeValue
block = clad
value_type = max
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = clad
[]
[max_hoop_stress]
type = ElementExtremeValue
block = clad
value_type = max
variable = hoop_stress
[]
[vonmises_stress_clad]
type = ElementAverageValue
block = clad
variable = vonmises_stress
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = total_hoop_strain
[]
[max_disp_x]
type = NodalExtremeValue
block = clad
value_type = max
variable = disp_x
[]
[min_burst_stress]
type = ElementExtremeValue
block = clad
value_type = min
variable = burst_stress
[]
[burst]
type = ElementExtremeValue
block = clad
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = clad
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
[]
[PerformanceMetricOutputs]
[]
[Outputs]
color = false
perf_graph = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[csv]
type = CSV
[]
[chkfile]
type = CSV
show = 'max_disp_x max_hoop_stress vonmises_stress_clad'
execute_on = 'FINAL'
[]
[]
[UserObjects]
[terminator1]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '5'
include_fuel = false
[]
[]
(test/tests/solid_mechanics/zry_mechanics/elastic_modulus_zry_errorcheck.i)
#--------------------------------------------------------------------------------
#
# This test case is prepared to test error checking with the MATPRO options
#
# - Geometry:
# Ri = 0.005 m
# Ro = 0.0055 m
# H = 0.01 m
#
# - Single element
# - Temperature = 300 - 1000 K
# - Boundary conditions:
# axial stress = -100 MPa at the top.
#--------------------------------------------------------------------------------
[Mesh]
coord_type = RZ
use_displaced_mesh = false
[mesh]
type = FileMeshGenerator
file = clad_rz_short_rev3.e
[]
[]
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Problem]
type = FEProblem
kernel_coverage_check = false
[]
[Variables]
[temp]
order = FIRST
family = LAGRANGE
initial_condition = 300
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[all]
strain = SMALL
block = 1
add_variables = true
[]
[]
[]
[]
[Functions]
[temperature_function]
type = PiecewiseLinear
x = '0 10'
y = '300 1000'
[]
[pressure_function]
type = PiecewiseLinear
x = '0 10'
y = '1 1'
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temp
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temp
[]
[]
[BCs]
[top_pressure] #Simplified BC to apply pressure in only disp_y
type = Pressure
boundary = 2
variable = disp_y
function = pressure_function
factor = 100e6
[]
[u_bottom_fix]
type = DirichletBC
variable = disp_y
boundary = 4
value = 0.0
[]
[temp_bc_1]
type = FunctionDirichletBC
variable = temp
boundary = '1 2 3 4'
function = temperature_function
[]
[]
[Materials]
[elasticity_tensor]
type = ZryElasticityTensor
matpro_poissons_ratio = true
matpro_youngs_modulus = true
[]
[stress]
type = ComputeFiniteStrainElasticStress
[]
[clad_density]
type = Density
density = 7874
[]
[thermal]
type = ZryThermal
temperature = temp
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-ksp_gmres_restart'
petsc_options_value = '101'
line_search = 'none'
l_max_its = 100
nl_max_its = 100
nl_rel_tol = 1e-8
nl_abs_tol = 1e-8
l_tol = 1e-8
start_time = 0.0
end_time = 1
dt = 1
[]
[Outputs]
exodus = false
[]
(assessment/LWR/validation/LOCA_Hardy_cladding_test/analysis/3pt8MPa/100C_sec/100C_sec_Hardy_Tube_Test_3pt8MPa.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
volumetric_locking_correction = false
displacements = 'disp_x disp_y'
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
group_variables = 'disp_x disp_y'
[]
[Mesh]
coord_type = RZ
patch_size = 10
patch_update_strategy = iteration
partitioner = centroid
centroid_partitioner_direction = y
[gen]
type = FuelPinMeshGenerator
include_fuel = false
include_clad = true
pellet_outer_radius = 0.0072527
clad_gap_width = 0.0
clad_top_gap_height = 0.0
clad_bot_gap_height = 0.0
clad_thickness = 0.38e-3
pellet_height = 0.5
pellet_quantity = 1
clad_mesh_density = customize
nx_c = 2
ny_c = 50
elem_type = QUAD8
[]
[]
[Variables]
[temperature]
initial_condition = 600.0
[]
[]
[AuxVariables]
[creep_rate_aux]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[total_hoop_strain]
order = CONSTANT
family = MONOMIAL
[]
[burst_stress]
order = CONSTANT
family = MONOMIAL
[]
[burst]
order = CONSTANT
family = MONOMIAL
[]
[]
[Functions]
[pressure_function]
type = PiecewiseLinear
x = '0 40'
y = '1 1'
[]
[temp_function]
type = PiecewiseLinear
y = '600 1600'
[]
[temperature_profile]
type = PiecewiseBilinear
y = '0 40'
x = '0 0.25224 0.50448'
z = '0.995 1.01 0.995 0.995 1.01 0.995'
axis = 1
[]
[inner_temperature]
type = CompositeFunction
functions = 'temp_function temperature_profile'
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[clad]
block = clad
add_variables = true
strain = FINITE
decomposition_method = EigenSolution
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz elastic_strain_xx elastic_strain_yy elastic_strain_zz
creep_strain_xx creep_strain_yy creep_strain_zz hoop_stress'
extra_vector_tags = 'ref'
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
extra_vector_tags = 'ref'
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
extra_vector_tags = 'ref'
[]
[]
[AuxKernels]
[creep_rate_aux]
type = MaterialRealAux
variable = creep_rate_aux
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[creep_rate]
type = MaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[total_hoop_strain]
type = RankTwoAux
rank_two_tensor = total_strain
variable = total_hoop_strain
index_i = 2
index_j = 2
execute_on = timestep_end
block = clad
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = clad_outside_right
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = clad_outside_right
execute_on = timestep_end
[]
[]
[BCs]
[Pressure]
[outer_surface]
boundary = 'clad_outside_bottom clad_outside_right clad_outside_top'
factor = 0.0
function = pressure_function
[]
[inner_surface]
boundary = 'clad_inside_right clad_inside_bottom clad_inside_top'
function = pressure_function
[]
[]
[u_bottom_fix]
type = DirichletBC
variable = disp_y
boundary = 1001
value = 0.0
[]
[x_fix]
type = DirichletBC
variable = disp_x
boundary = centerline
value = 0.0
[]
[temp_bc]
type = FunctionDirichletBC
function = inner_temperature
variable = temperature
boundary = 'clad_inside_bottom clad_inside_right clad_inside_top'
[]
[]
[Materials]
[clad_thermal]
type = ZryThermal
block = clad
zry_thermal_properties_model = MATPRO
temperature = temperature
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = clad
matpro_youngs_modulus = true
matpro_poissons_ratio = true
temperature = temperature
[]
[clad_stress]
type = ComputeMultipleInelasticStress
inelastic_models = 'clad_zrycreep'
block = clad
tangent_operator = nonlinear
[]
[clad_zrycreep]
type = ZryCreepLOCAUpdate
block = clad
temperature = temperature
model_irradiation_creep = false
model_primary_creep = true
model_thermal_creep = true
temperature_loca_creep_begin = 840 # values from the report
temperature_standard_thermal_creep_end = 975
[]
[thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = clad
temperature = temperature
stress_free_temperature = 600.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[clad_density]
type = Density
block = clad
density = 6550.0
[]
[phase]
type = ZrPhase
block = clad
temperature = temperature
numerical_method = 2
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = clad_outside_right
failure_criterion = combined_overstress_and_overstrain
hoop_stress = hoop_stress
hoop_creep_strain = creep_strain_zz
effective_strain_rate_creep = creep_rate_aux
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.0e-5
nl_abs_tol = 1.0e-8
start_time = 0
n_startup_steps = 1
end_time = 40
dtmax = 1
dtmin = 0.0000001
[TimeStepper]
type = IterationAdaptiveDT
timestep_limiting_postprocessor = material_timestep
dt = 1.0
[]
[]
[Postprocessors]
[ave_clad_temp]
type = SideAverageValue
boundary = clad_outside_right
variable = temperature
[]
[gas_volume]
type = InternalVolume
boundary = all_clad_interior
execute_on = 'initial linear'
[]
[max_clad_temp]
type = NodalExtremeValue
block = clad
value_type = max
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = clad
[]
[max_hoop_stress]
type = ElementExtremeValue
block = clad
value_type = max
variable = hoop_stress
[]
[vonmises_stress_clad]
type = ElementAverageValue
block = clad
variable = vonmises_stress
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = total_hoop_strain
[]
[max_disp_x]
type = NodalExtremeValue
block = clad
value_type = max
variable = disp_x
[]
[min_burst_stress]
type = ElementExtremeValue
block = clad
value_type = min
variable = burst_stress
[]
[burst]
type = ElementExtremeValue
block = clad
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = clad
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
[]
[PerformanceMetricOutputs]
[]
[Outputs]
color = false
perf_graph = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[csv]
type = CSV
[]
[chkfile]
type = CSV
show = 'max_disp_x max_hoop_stress vonmises_stress_clad'
execute_on = 'FINAL'
[]
[]
[UserObjects]
[terminator1]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '5'
include_fuel = false
[]
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-05/puzry-05.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-05.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 2000. '
y = '1.e+05 1.e+05 7.2e+05' # Linear increase at 0.0062 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 2000. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = EigenSolution
[]
[]
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = MaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = FunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = DirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = DirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1.e+11
poissons_ratio = 0.3
block = 1
[]
[creep_update]
type = ZryCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 1.e-04
temperature = temperature
temperature_standard_thermal_creep_end = 700
temperature_loca_creep_begin = 900.
[]
[creep]
type = ComputeMultipleInelasticStress
block = 1
tangent_operator = elastic
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = Density
block = 1
[]
[phase]
type = ZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
active = 'smp'
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0.
n_startup_steps = 1
end_time = 2000.
dtmax = 1.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-05_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-18/puzry-18_aniso.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-18.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 1500. '
y = '1.e+05 1.e+05 5.855e+06' # Linear increase at 0.1151 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 1500. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
# Circumferential steady-state creep test and analysis of Zircaloy-4 fuel cladding
# Nuclear Engineering and Design, 53, 2312-2322 (2021)
[F]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.738 0.738 0.57'
[]
[G]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.174 0.174 0.45'
[]
[H]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.588 0.588 0.48'
[]
[L]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[M]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[N]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = TaylorExpansion
use_automatic_differentiation = true
[]
[]
[]
[]
[Kernels]
[heat]
type = ADHeatConduction
variable = temperature
[]
[heat_ie]
type = ADHeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = ADMaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = ADMaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = ADMaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = ADMaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = ADMaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = ADFunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = ADDirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = ADDirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ADZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1.e+11
poissons_ratio = 0.3
block = 1
[]
[hill_constants]
type = ADHillConstants
hill_constants = "0.738 0.174 0.588 1.0 1.0 1.0"
function_names = "F G H L M N"
temperature = temperature
[]
[creep_update]
type = ADZryAnisoCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 5.0e-05
temperature = temperature
temperature_standard_thermal_creep_end = 700
temperature_loca_creep_begin = 900.
fract_beta_phase_name = 'fract_beta_phase'
max_integration_error = 1000000.0
absolute_tolerance = 1e-13
relative_tolerance = 1e-11
[]
[creep]
type = ADComputeMultipleInelasticStress
block = 1
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ADZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = ADDensity
block = 1
[]
[phase]
type = ADZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ADZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = NEWTON
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0.
n_startup_steps = 1
end_time = 2500.
dtmax = 1.
dtmin = 1.0e-9
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-18_aniso_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/benchmark/RIA_benchmark/analysis/RIA_benchmark.i)
# RIA Benchmark - Case 5 with full output in CSV
[GlobalParams]
density = 10531 # UO2 with 4% porosity
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
acceptable_iterations = 20
acceptable_multiplier = 10
[]
[Mesh]
coord_type = RZ
[smeared_pellet_mesh]
type = FuelPinMeshGenerator
clad_mesh_density = customize
pellet_mesh_density = customize
nx_p = 10
ny_p = 40
ny_cu = 3
ny_c = 40
ny_cl = 3
nx_c = 5
clad_thickness = 5.7e-4
pellet_outer_radius = 4.13e-3
pellet_quantity = 10
pellet_height = 1e-2
clad_top_gap_height = 0.0186616493139897
clad_bot_gap_height = 0.0186616493139897
clad_gap_width = 0.0
bottom_clad_height = 2.24e-3
top_clad_height = 2.24e-3
elem_type = QUAD8
[]
patch_size = 10
patch_update_strategy = auto
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temp]
initial_condition = 293.15
[]
[]
[AuxVariables]
[plastic_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_temp]
order = CONSTANT
family = MONOMIAL
[]
[clad_water_htc]
order = CONSTANT
family = MONOMIAL
[]
[clad_water_flux]
order = CONSTANT
family = MONOMIAL
[]
[gap_cond]
order = CONSTANT
family = MONOMIAL
[]
[burnup]
order = CONSTANT
family = MONOMIAL
initial_condition = 0.0
[]
[]
[Functions]
[power_history] # triangular pulse power history defined by benchmark
type = PiecewiseLinear
scale_factor = 1.0
xy_data = ' 0 0
10 0
20 0
30 0
40 0
50 0
60 0
70 0
80 0
90 0
100 0
100.0003 0.01
100.0006 0.02
100.0009 0.03
100.030 1
100.060 0
100.081 0
100.082 0
100.083 0
100.084 0
100.085 0
100.086 0
100.087 0
100.088 0
100.089 0
100.090 0
100.091 0
100.092 0
100.093 0
100.094 0
100.095 0
100.096 0
100.097 0
100.098 0
100.099 0
100.100 0
100.105 0
100.110 0
100.115 0
100.120 0
100.125 0
100.130 0
100.135 0
100.140 0
100.145 0
100.150 0
100.155 0
100.160 0
100.165 0
100.170 0
100.175 0
100.180 0
100.185 0
100.190 0
100.195 0
100.200 0
100.210 0
100.220 0
100.230 0
100.240 0
100.250 0
100.260 0
100.270 0
100.280 0
100.290 0
100.300 0
100.310 0
100.320 0
100.330 0
100.340 0
100.350 0
100.360 0
100.370 0
100.380 0
100.390 0
100.400 0
100.410 0
100.420 0
100.430 0
100.440 0
100.450 0
100.460 0
100.470 0
100.480 0
100.490 0
100.500 0
100.510 0
100.520 0
100.530 0
100.540 0
100.550 0
100.560 0
100.570 0
100.580 0
100.590 0
100.600 0
100.610 0
100.620 0
100.630 0
100.640 0
100.650 0
100.660 0
100.670 0
100.680 0
100.690 0
100.700 0
100.710 0
100.720 0
100.730 0
100.740 0
100.750 0
100.760 0
100.770 0
100.780 0
100.790 0
100.800 0
100.810 0
100.820 0
100.830 0
100.840 0
100.850 0
100.860 0
100.870 0
100.880 0
100.890 0
100.900 0
100.910 0
100.920 0
100.930 0
100.940 0
100.950 0
100.960 0
100.970 0
100.980 0
100.990 0
101.000 0
101.100 0
101.200 0
101.300 0
101.400 0
101.500 0
101.600 0
101.700 0
101.800 0
101.900 0
102.000 0
102.100 0
102.200 0
102.300 0
102.400 0
102.500 0
102.600 0
102.700 0
102.800 0
102.900 0
103.000 0
103.100 0
103.200 0
103.300 0
103.400 0
103.500 0
103.600 0
103.700 0
103.800 0
103.900 0
104.000 0
104.100 0
104.200 0
104.300 0
104.400 0
104.500 0
104.600 0
104.700 0
104.800 0
104.900 0
105.000 0
105.100 0
105.200 0
105.300 0
105.400 0
105.500 0
105.600 0
105.700 0
105.800 0
105.900 0
106.000 0
106.100 0
106.200 0
106.300 0
106.400 0
106.500 0
106.600 0
106.700 0
106.800 0
106.900 0
107.000 0
107.100 0
107.200 0
107.300 0
107.400 0
107.500 0
107.600 0
107.700 0
107.800 0
107.900 0
108.000 0
108.100 0
108.200 0
108.300 0
108.400 0
108.500 0
108.600 0
108.700 0
108.800 0
108.900 0
109.000 0
109.100 0
109.200 0
109.300 0
109.400 0
109.500 0
109.600 0
109.700 0
109.800 0
109.900 0
110 0
111 0
112 0
113 0
114 0
115 0
116 0
117 0
118 0
119 0
120 0
130 0
140 0
150 0
160 0
170 0
180 0
190 0
200 0'
[]
[pressure_ramp] # inlet coolant pressure evolution
type = PiecewiseLinear
scale_factor = 1.0
xy_data = '0 1e5
50 1.55e7
200 1.55e7'
[]
[temp_ramp] # inlet coolant temperature evolution
type = PiecewiseLinear
scale_factor = 1.0
xy_data = '0 293.15
50 553.15
200 553.15'
[]
[Fuel_CTE_function] #Fuel CTE as a function of temp from MATPRO data
type = PiecewiseLinear
scale_factor = 1.0
xy_data = ' 0 1.00005E-05
300 1.00005E-05
350 1.00005E-05
400 1.00015E-05
450 0.000010004
500 1.00091E-05
550 0.000010018
600 1.00321E-05
650 1.00522E-05
700 1.00791E-05
750 1.01131E-05
800 1.01544E-05
850 1.02028E-05
900 1.02577E-05
950 1.03187E-05
1000 0.000010385
1050 0.000010456
1100 1.05308E-05
1150 1.06087E-05
1200 1.06891E-05
1250 1.07712E-05
1300 1.08545E-05
1350 1.09384E-05
1400 1.10224E-05
1450 1.11061E-05
1500 1.11891E-05
1550 1.12712E-05
1600 1.13519E-05
1650 1.14311E-05
1700 1.15087E-05
1750 1.15844E-05
1800 0.000011658
1850 1.17297E-05
1900 1.17991E-05
1950 1.18664E-05
2000 1.19314E-05
2050 1.19942E-05
2100 1.20547E-05
2150 0.000012113
2200 1.21691E-05
2250 1.22229E-05
2300 1.22746E-05
2350 1.23242E-05
2400 1.23717E-05'
[]
[Clad_CTE_function] #Cladding CTE as a function of temp from MATPRO data
type = PiecewiseLinear
scale_factor = 1.0
xy_data = ' 0 0.00000495
300 0.00000495
350 0.00000495
400 0.00000495
450 0.00000495
500 0.00000495
550 0.00000495
600 0.00000495
650 0.00000495
700 0.00000495
750 0.00000495
800 0.00000495
850 0.00000495
900 0.00000495
950 0.00000495
1000 0.00000495
1050 0.00000495
1083 0.00000495
1100 4.76997E-06
1150 3.60423E-06
1200 2.2888E-06
1244 1.77904E-06
1250 1.81579E-06
1300 0.00000221
1350 2.56667E-06
1400 2.89091E-06
1450 3.18696E-06
1500 3.45833E-06
1550 0.000003708
1600 3.93846E-06
1650 4.15185E-06
1700 0.00000435
1750 4.53448E-06
1800 4.70667E-06
1850 4.86774E-06
1900 5.01875E-06
1950 5.16061E-06
2000 5.29412E-06
2050 0.00000542
2098 5.53426E-06'
[]
[YS_function] #Yield Strength as a function of temp from PNNL report
#Cold work = 0.5, Average oxygen concentration = 0, fast neutron fluence = 0
#Assumed constant strain rate of 0.01
type = PiecewiseLinear
scale_factor = 1.0
xy_data = ' 0 593425301.8
300 593425301.8
320 580674456.3
340 567078477.7
360 552695674.7
380 537584819.6
400 521805085.5
420 505428587.7
440 489716889.1
460 475582155.5
480 462727514.7
500 450878059.4
520 439778204.9
540 429188702.8
560 418888211.8
580 408677370.3
600 398362281.7
620 387769321.2
640 376741767.7
660 365140974.9
680 352847834.1
700 339764457.8
720 325816004.1
740 310952563.6
760 271786784.1
780 222194537.8
800 185377726.5
820 154173430.2
840 130199325.7
860 111396817.2
880 96362607.14
900 84120129.15
920 73977044.17
940 65434357.46
960 58127235.93
980 51785717.25
1000 46208150.84
1020 41242936.22
1040 36775756.82
1060 32720505.36
1080 29012718.16
1090 27273687.16
1100 26355024.23
1120 22442026.84
1140 18753365.2
1160 15296510.38
1180 12079785.07
1200 9113113.474
1220 6409493.205
1240 3988344.555
1250 2893569.671
1255 2377978.33
1260 2323366.884
1280 2116912.621
1300 1928475.009
1320 1756577.201
1340 1599841.384
1360 1456985.125
1380 1326817.541
1400 1208235.326'
[]
#############################
[cp_factor]
type = ConstantFunction
value = 1.0
[]
[total_energy] #total Joules of energy injected into fuel during the RIA pulse
type = ConstantFunction
value = 30000
[]
[FWMH] #Full Width at Mid Height of RIA pulse
type = ConstantFunction
value = 0.03
[]
[fuel_OR] #Fuel outer radius
type = ConstantFunction
value = 0.00413
[]
##########################
[heat_generation] #A factor to multiply the pulse history to get desired energy/gram into the fuel
type = ParsedFunction
expression = 'energy / (pi * fuelradius * fuelradius * height) / pulsewidth'
symbol_names = 'height energy pulsewidth fuelradius'
symbol_values = '0.1 zz_total_energy zz_FWMH zz_fuel_OR'
[]
[power_ramp] #Transient power pulse applied to the fuel as a uniform heat generation term (W/m^3)
type = CompositeFunction
functions = 'power_history heat_generation'
scale_factor = 1.0
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[pellets]
block = pellet
strain = FINITE
temperature = temp
eigenstrain_names = 'fuel_thermal_eigenstrain'
extra_vector_tags = 'ref'
decomposition_method = EigenSolution
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
generate_output = 'stress_yy stress_zz vonmises_stress hoop_stress'
[]
[clad]
block = clad
strain = FINITE
temperature = temp
eigenstrain_names = 'clad_thermal_eigenstrain'
extra_vector_tags = 'ref'
decomposition_method = EigenSolution
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
generate_output = 'stress_yy stress_zz plastic_strain_yy plastic_strain_zz elastic_strain_yy elastic_strain_zz strain_yy strain_zz vonmises_stress hoop_stress axial_stress'
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temp
extra_vector_tags = 'ref'
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temp
extra_vector_tags = 'ref'
[]
[heat_source_fuel]
type = HeatSource
variable = temp
block = 'pellet'
function = power_ramp
value = 1.0
extra_vector_tags = 'ref'
[]
[]
[AuxKernels]
[plastic_strain_mag]
type = MaterialRealAux
property = effective_plastic_strain
variable = plastic_strain_mag
block = clad
execute_on = timestep_end
[]
[clad_water_htc]
type = MaterialRealAux
property = coolant_channel_htc
variable = clad_water_htc
boundary = 2
[]
[coolant_temp]
type = MaterialRealAux
property = coolant_temperature
variable = coolant_temp
boundary = 2
[]
[clad_water_flux]
type = MaterialRealAux
property = output_heat_flux
variable = clad_water_flux
boundary = 2
[]
[conductance]
type = MaterialRealAux
property = gap_conductance
variable = gap_cond
boundary = 10
[]
[]
[Contact]
[pellet_clad_mechanical]
primary = 5
secondary = 10
model = coulomb
friction_coefficient = 100
formulation = tangential_penalty
normalize_penalty = true
penalty = 1e12
normal_smoothing_distance = 0.1
tangential_tolerance = 1e-3
[]
[]
[ThermalContact]
[thermal_contact]
type = GasGapHeatTransfer
variable = temp
primary = 5
secondary = 10
emissivity_primary = 0.797698
emissivity_secondary = 0.325
roughness_secondary = 0.1e-6 #roughness specified in benchmark
roughness_primary = 0.1e-6
roughness_coef = 3.2
plenum_pressure = plenum_pressure
jump_distance_model = LANNING
contact_pressure = contact_pressure
normal_smoothing_distance = 0.1
quadrature = true
order = SECOND
[]
[]
[BCs]
[fixed_external_clad_temp]
type = FunctionDirichletBC
variable = temp
boundary = 1
function = temp_ramp
[]
[fixed_external_clad_temp_2]
type = FunctionDirichletBC
variable = temp
boundary = 3
function = temp_ramp
[]
[no_x_all]
type = DirichletBC
variable = disp_x
boundary = 12
value = 0.0
[]
[no_y_clad_bottom]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[]
[no_y_fuel_bottom]
type = DirichletBC
variable = disp_y
boundary = 20
value = 0.0
[]
[Pressure]
[coolantPressure]
boundary = '1 2 3'
factor = 1
function = pressure_ramp
[]
[]
[PlenumPressure]
[plenumPressure]
boundary = 9
initial_temperature = 293.15
initial_pressure = 2.0e6
startup_time = 0
R = 8.3143
output_initial_moles = initial_moles
temperature = representative_plenum_temperature_node
volume = plenum_volume
output = plenum_pressure
[]
[]
[]
[CoolantChannel]
[convective_clad_surface]
chf_correlation_type = 1 # EPRI
htc_correlation_type = 1 # Thom or McDonough... or Groenveld
boundary = '2'
variable = temp
coolant_material = 'water'
inlet_massflux = 3057.2 #kg/(m^2 s)
inlet_temperature = temp_ramp
inlet_pressure = pressure_ramp
compute_enthalpy = true
flow_area = 1.0731681e-4 #m^2
heated_diameter = 1.4536170e-2 #m
hydraulic_diameter = 5.6e-3 #m
heated_perimeter = 2.9530971e-2 #m
heat_transfer_mode = 0
number_axial_zone = 50
htc_scalef = 1
[]
[]
[Materials]
[density_fuel]
type = Density
block = 'pellet'
[]
[fuel_thermal]
type = UO2Thermal
block = 'pellet'
temperature = temp
burnup = burnup
initial_porosity = 0.04
thermal_conductivity_model = NFIR
[]
[fuel_elasticity_tensor]
type = UO2ElasticityTensor
temperature = temp
block = pellet
[]
[fuel_stress]
type = ComputeFiniteStrainElasticStress
block = pellet
[]
[fuel_thermal_expansion]
type = ComputeInstantaneousThermalExpansionFunctionEigenstrain
block = pellet
temperature = temp
thermal_expansion_function = Fuel_CTE_function
stress_free_temperature = 293.15
eigenstrain_name = 'fuel_thermal_eigenstrain'
[]
[density_clad]
type = Density
block = clad
density = 6551.0
[]
[clad_thermal]
type = ZryThermal
block = clad
temperature = temp
[]
[clad_youngs_modulus]
type = PiecewiseLinearInterpolationMaterial
block = clad
xy_data = ' 0 79375000000
300 79375000000
320 78280000000
340 77185000000
360 76090000000
380 74995000000
400 73900000000
420 72805000000
440 71710000000
460 70615000000
480 69520000000
500 68425000000
520 67330000000
540 66235000000
560 65140000000
580 64045000000
600 62950000000
620 61855000000
640 60760000000
660 59665000000
680 58570000000
700 57475000000
720 56380000000
740 55285000000
760 54190000000
780 53095000000
800 52000000000
820 50905000000
840 49810000000
860 48715000000
880 47620000000
900 46525000000
920 45430000000
940 44335000000
960 43240000000
980 42145000000
1000 41050000000
1020 39955000000
1040 38860000000
1060 37765000000
1080 36670000000
1090 36122500000
1100 36434621212
1120 37058863636
1140 37683106061
1160 38307348485
1180 38931590909
1200 39555833333
1220 40180075758
1240 40804318182
1250 41116439394
1255 41272500000
1260 41070000000
1280 40260000000
1300 39450000000
1320 38640000000
1340 37830000000
1360 37020000000
1380 36210000000
1400 35400000000'
property = clad_youngs_modulus
variable = temp
[]
[clad_elasticity_tensor]
type = ComputeVariableIsotropicElasticityTensor
block = clad
args = temp
youngs_modulus = clad_youngs_modulus
poissons_ratio = 0.3
[]
[clad_stress]
type = ComputeMultipleInelasticStress
block = clad
inelastic_models = 'plasticity'
tangent_operator = elastic
[]
[clad_thermal_expansion]
type = ComputeInstantaneousThermalExpansionFunctionEigenstrain
block = clad
temperature = temp
thermal_expansion_function = Clad_CTE_function
stress_free_temperature = 293.15
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[plasticity]
type = IsotropicPlasticityStressUpdate
block = clad
temperature = temp
hardening_constant = 2.5e9
yield_stress_function = YS_function
[]
[]
[Dampers]
[BoundingValueNodalDamper]
type = BoundingValueNodalDamper
max_value = 3200
min_value = 200
variable = temp
[]
[contact_slip]
type = ContactSlipDamper
primary = 5
secondary = 10
min_damping_factor = 0.05
[]
[]
[Executioner]
type = Transient
line_search = 'none'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
l_max_its = 100
l_tol = 1e-4
nl_max_its = 40
nl_rel_tol = 1e-3
nl_abs_tol = 1e-8
start_time = 0
end_time = 200
dtmax = 10
dtmin = 1e-6
[TimeStepper]
type = IterationAdaptiveDT
dt = 10
force_step_every_function_point = true
timestep_limiting_function = power_history
max_function_change = 0.03
optimal_iterations = 25
iteration_window = 5
linear_iteration_ratio = 1000
growth_factor = 1.2
[]
[Quadrature]
order = FIFTH
side_order = SEVENTH
[]
[]
[Postprocessors]
[representative_plenum_temperature_node] #Temperature used for plenum gas, using a node slightly above where the fuel contacts the cladding
type = NodalVariableValue
variable = temp
nodeid = 771
execute_on = 'initial linear'
[]
[2_input_rod_power]
type = FunctionValuePostprocessor
function = power_history
[]
[clad_inner_vol]
type = InternalVolume
boundary = 7
execute_on = 'initial linear'
[]
[3_fuel_centerline_temp]
type = NodalVariableValue
variable = temp
nodeid = 1643
execute_on = 'initial timestep_end'
[]
[4_fuel_surface_temp]
type = NodalVariableValue
variable = temp
nodeid = 1671
execute_on = 'initial timestep_end'
[]
[5_clad_inner_surface_temp]
type = NodalVariableValue
variable = temp
nodeid = 496
execute_on = 'initial timestep_end'
[]
[6_clad_outer_surface_temp]
type = NodalVariableValue
variable = temp
nodeid = 509
execute_on = 'initial timestep_end'
[]
[clad_axial_elongation]
type = NodalVariableValue
variable = disp_y
nodeid = 900
execute_on = 'initial timestep_end'
[]
[fuel_axial_elongation]
type = NodalVariableValue
variable = disp_y
nodeid = 2311
execute_on = 'initial timestep_end'
[]
[clad_radial_elongation]
type = NodalVariableValue
variable = disp_x
nodeid = 496
execute_on = 'initial timestep_end'
[]
[fuel_radial_elongation]
type = NodalVariableValue
variable = disp_x
nodeid = 1671
execute_on = 'initial timestep_end'
[]
[clad_hoop_stress]
type = ElementalVariableValue
variable = hoop_stress
elementid = 149
execute_on = 'initial timestep_end'
[]
[clad_axial_stress]
type = ElementalVariableValue
variable = axial_stress
elementid = 149
execute_on = 'initial timestep_end'
[]
[total_hoop_strain]
type = ElementalVariableValue
variable = strain_zz
elementid = 149
execute_on = 'initial timestep_end'
[]
[total_axial_strain]
type = ElementalVariableValue
variable = strain_yy
elementid = 149
execute_on = 'initial timestep_end'
[]
[plastic_hoop_strain]
type = ElementalVariableValue
variable = plastic_strain_zz
elementid = 149
execute_on = 'initial timestep_end'
[]
[plastic_axial_strain]
type = ElementalVariableValue
variable = plastic_strain_yy
elementid = 149
execute_on = 'initial timestep_end'
[]
[elastic_hoop_strain]
type = ElementalVariableValue
variable = elastic_strain_zz
elementid = 149
execute_on = 'initial timestep_end'
[]
[elastic_axial_strain]
type = ElementalVariableValue
variable = elastic_strain_yy
elementid = 149
execute_on = 'initial timestep_end'
[]
############################
[gap_cond]
type = ElementalVariableValue
variable = gap_cond
elementid = 499
execute_on = 'initial timestep_end'
[]
[coolant_temp]
type = ElementalVariableValue
variable = coolant_temp
elementid = 149
execute_on = 'initial timestep_end'
[]
[clad_water_flux]
type = ElementalVariableValue
variable = clad_water_flux
elementid = 149
execute_on = 'initial timestep_end'
[]
[clad_water_htc]
type = ElementalVariableValue
variable = clad_water_htc
elementid = 149
execute_on = 'initial timestep_end'
[]
[qpoint_penetration]
type = ElementalVariableValue
variable = qpoint_penetration
elementid = 499
execute_on = 'initial timestep_end'
[]
[penetration]
type = NodalVariableValue
variable = penetration
nodeid = 1671
execute_on = 'initial timestep_end'
[]
[contact_pressure]
type = NodalVariableValue
variable = contact_pressure
nodeid = 1671
execute_on = 'initial timestep_end'
[]
[zz_fuel_OR]
type = FunctionValuePostprocessor
function = fuel_OR
execute_on = 'initial timestep_end'
[]
[zz_total_energy]
type = FunctionValuePostprocessor
function = total_energy
execute_on = 'initial timestep_end'
[]
[zz_FWMH]
type = FunctionValuePostprocessor
function = FWMH
execute_on = 'initial timestep_end'
[]
[zz_cp_factor]
type = FunctionValuePostprocessor
function = cp_factor
execute_on = 'initial timestep_end'
[]
[zzz_heat_generation]
type = FunctionValuePostprocessor
function = heat_generation
execute_on = 'initial timestep_end'
[]
[zzzz_power_ramp]
type = FunctionValuePostprocessor
function = power_ramp
execute_on = 'initial timestep_end'
[]
[zzzzz_RAE]
type = RadialAverageEnthalpy
vector_postprocessor = rad_temp
radial_direction = x
axial_direction = y
axial_position = 0.0709016
temperature_name = temp
execute_on = 'initial timestep_end'
[]
[peak_RAE]
type = TimeExtremeValue
postprocessor = zzzzz_RAE
[]
[]
[VectorPostprocessors]
[rad_temp]
type = NodalValueSampler
block = 3
sort_by = y
variable = temp
outputs = dummy
execute_on = 'initial timestep_end'
[]
[]
[StandardLWRFuelRodOutputs]
temperature = temp
rod_component = CLAD ## Request only clad components because fission gas models are not used in this input file
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
time_step_interval = 1
csv = true
exodus = true
color = false
[console]
type = Console
output_linear = true
max_rows = 10
[]
[dummy]
type = CSV
enable = false
[]
[chkfile]
type = CSV
show = 'plenum_temperature average_interior_clad_temperature plenum_volume peak_RAE'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/LOCA_Hardy_cladding_test/analysis/0pt7MPa/100C_sec/Hardy_Tube_Test_0pt7MPa.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
volumetric_locking_correction = false
displacements = 'disp_x disp_y'
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
group_variables = 'disp_x disp_y'
[]
[Mesh]
coord_type = RZ
patch_size = 10
patch_update_strategy = iteration
partitioner = centroid
centroid_partitioner_direction = y
[gen]
type = FuelPinMeshGenerator
include_fuel = false
include_clad = true
pellet_outer_radius = 0.0072527
clad_gap_width = 0.0
clad_top_gap_height = 0.0
clad_bot_gap_height = 0.0
clad_thickness = 0.38e-3
pellet_height = 0.5
pellet_quantity = 1
clad_mesh_density = customize
nx_c = 2
ny_c = 50
elem_type = QUAD8
[]
[]
[Variables]
[temperature]
initial_condition = 600.0
[]
[]
[AuxVariables]
[creep_rate_aux]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[total_hoop_strain]
order = CONSTANT
family = MONOMIAL
[]
[burst_stress]
order = CONSTANT
family = MONOMIAL
[]
[burst]
order = CONSTANT
family = MONOMIAL
[]
[]
[Functions]
[pressure_function]
type = PiecewiseLinear
x = '0 40'
y = '1 1'
[]
[temp_function]
type = PiecewiseLinear
y = '600 1600'
[]
[temperature_profile]
type = PiecewiseBilinear
y = '0 40'
x = '0 0.25224 0.50448'
z = '0.995 1.01 0.995 0.995 1.01 0.995'
axis = 1
[]
[inner_temperature]
type = CompositeFunction
functions = 'temp_function temperature_profile'
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[clad]
block = clad
add_variables = true
strain = FINITE
decomposition_method = EigenSolution
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz elastic_strain_xx elastic_strain_yy elastic_strain_zz
creep_strain_xx creep_strain_yy creep_strain_zz hoop_stress'
extra_vector_tags = 'ref'
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
extra_vector_tags = 'ref'
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
extra_vector_tags = 'ref'
[]
[]
[AuxKernels]
[creep_rate_aux]
type = MaterialRealAux
variable = creep_rate_aux
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[creep_rate]
type = MaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[total_hoop_strain]
type = RankTwoAux
rank_two_tensor = total_strain
variable = total_hoop_strain
index_i = 2
index_j = 2
execute_on = timestep_end
block = clad
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = clad_outside_right
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = clad_outside_right
execute_on = timestep_end
[]
[]
[BCs]
[Pressure]
[outer_surface]
boundary = 'clad_outside_bottom clad_outside_right clad_outside_top'
factor = 0.0
function = pressure_function
[]
[inner_surface]
boundary = 'clad_inside_right clad_inside_bottom clad_inside_top'
function = pressure_function
[]
[]
[u_bottom_fix]
type = DirichletBC
variable = disp_y
boundary = 1001
value = 0.0
[]
[x_fix]
type = DirichletBC
variable = disp_x
boundary = centerline
value = 0.0
[]
[temp_bc]
type = FunctionDirichletBC
function = inner_temperature
variable = temperature
boundary = 'clad_inside_bottom clad_inside_right clad_inside_top'
[]
[]
[Materials]
[clad_thermal]
type = ZryThermal
block = clad
zry_thermal_properties_model = MATPRO
temperature = temperature
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = clad
matpro_youngs_modulus = true
matpro_poissons_ratio = true
temperature = temperature
[]
[clad_stress]
type = ComputeMultipleInelasticStress
inelastic_models = 'clad_zrycreep'
block = clad
tangent_operator = nonlinear
[]
[clad_zrycreep]
type = ZryCreepLOCAUpdate
block = clad
temperature = temperature
model_irradiation_creep = false
model_primary_creep = true
model_thermal_creep = true
temperature_loca_creep_begin = 840 # values from the report
temperature_standard_thermal_creep_end = 975
[]
[thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = clad
temperature = temperature
stress_free_temperature = 600.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[clad_density]
type = Density
block = clad
density = 6550.0
[]
[phase]
type = ZrPhase
block = clad
temperature = temperature
numerical_method = 2
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = clad_outside_right
failure_criterion = combined_overstress_and_overstrain
hoop_stress = hoop_stress
hoop_creep_strain = creep_strain_zz
effective_strain_rate_creep = creep_rate_aux
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.0e-5
nl_abs_tol = 1.0e-8
start_time = 0
n_startup_steps = 1
end_time = 40
dtmax = 1
dtmin = 0.0000001
[TimeStepper]
type = IterationAdaptiveDT
timestep_limiting_postprocessor = material_timestep
dt = 1.0
[]
[]
[Postprocessors]
[ave_clad_temp]
type = SideAverageValue
boundary = clad_outside_right
variable = temperature
[]
[gas_volume]
type = InternalVolume
boundary = all_clad_interior
execute_on = 'initial linear'
[]
[max_clad_temp]
type = NodalExtremeValue
block = clad
value_type = max
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = clad
[]
[max_hoop_stress]
type = ElementExtremeValue
block = clad
value_type = max
variable = hoop_stress
[]
[vonmises_stress_clad]
type = ElementAverageValue
block = clad
variable = vonmises_stress
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = total_hoop_strain
[]
[max_disp_x]
type = NodalExtremeValue
block = clad
value_type = max
variable = disp_x
[]
[min_burst_stress]
type = ElementExtremeValue
block = clad
value_type = min
variable = burst_stress
[]
[burst]
type = ElementExtremeValue
block = clad
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = clad
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
[]
[PerformanceMetricOutputs]
[]
[Outputs]
color = false
perf_graph = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[csv]
type = CSV
[]
[chkfile]
type = CSV
show = 'max_disp_x max_hoop_stress vonmises_stress_clad'
execute_on = 'FINAL'
[]
[]
[UserObjects]
[terminator1]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '5'
include_fuel = false
[]
[]
(assessment/LWR/validation/LOCA_REBEKA_cladding_burst_tests/analysis/rebeka_2d_02MPa/rebeka_singlerod_2d_02MPa_aniso.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
order = SECOND
family = LAGRANGE
displacements = 'disp_x disp_y'
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = rebeka_singlerod.e
[]
[]
[Variables]
[temperature]
initial_condition = 573.0
[]
[]
[Functions]
[temperature_func]
type = PiecewiseLinear
x = '0. 700. '
y = '573. 1273.' # From 300 to 1000 C at 1 K/s
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 700. '
y = '2.e+06 2.e+06' # 10 bar
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 700. '
y = '1.e+05 1.e+05' # atmospheric pressure
[]
# Circumferential steady-state creep test and analysis of Zircaloy-4 fuel cladding
# Nuclear Engineering and Design, 53, 2312-2322 (2021)
[F]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.738 0.738 0.57'
[]
[G]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.174 0.174 0.45'
[]
[H]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.588 0.588 0.48'
[]
[L]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[M]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[N]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[clad]
block = cladding
add_variables = true
strain = FINITE
decomposition_method = TaylorExpansion
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz hoop_stress'
use_automatic_differentiation = true
[]
[]
[AuxVariables]
[creep_rate_aux]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[scale_thickness]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfract_total]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfgain_total]
order = CONSTANT
family = MONOMIAL
[]
[burst_stress]
order = CONSTANT
family = MONOMIAL
[]
[burst]
order = CONSTANT
family = MONOMIAL
[]
[]
[Kernels]
[heat]
type = ADHeatConduction
variable = temperature
[]
[heat_ie]
type = ADHeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate_aux]
type = ADMaterialRealAux
variable = creep_rate_aux
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = ADMaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = ADMaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[scl_thickness]
type = ADMaterialRealAux
variable = scale_thickness
property = oxide_scale_thickness
boundary = 2
[]
[ofract_total]
type = ADMaterialRealAux
variable = oxywtfract_total
property = current_oxygen_weight_frac_total
boundary = 2
[]
[ofgain_total]
type = ADMaterialRealAux
boundary = 2
variable = oxywtfgain_total
property = oxygen_weight_frac_gained_total
[]
[sigmaburst]
type = ADMaterialRealAux
variable = burst_stress
property = burst_stress
boundary = 2
[]
[hasburst]
type = ADMaterialRealAux
variable = burst
property = failed
boundary = 2
execute_on = timestep_end
[]
[]
[BCs]
[inner_temperature]
type = REBEKADirichletBC
variable = temperature
function_tempm = temperature_func
minimum_temperature = 573.
translation = 0.1625
boundary = 4
[]
[no_y_midsection]
type = ADDirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply steam pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 101 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[CoolantChannel]
[convective_clad_surface]
boundary = 2
variable = temperature
inlet_temperature = 473.
inlet_pressure = 1.e+05
inlet_massflux = 1.0 # kg/m^2-sec # almost stagnant steam
rod_diameter = 10.75e-03
rod_pitch = 1.26e-02 # default
oxide_thickness = scale_thickness
number_axial_zone = 15
use_ad = true
[]
[]
[Materials]
[thermal]
type = ADZryThermal
block = cladding
temperature = temperature
[]
[clad_elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
block = cladding
youngs_modulus = 1.0e11
poissons_ratio = 0.3
[]
[clad_stress]
type = ADComputeMultipleInelasticStress
inelastic_models = 'clad_zrycreep'
block = cladding
[]
[hill_constants]
type = ADHillConstants
hill_constants = "0.738 0.174 0.588 1.0 1.0 1.0"
function_names = "F G H L M N"
temperature = temperature
[]
[clad_zrycreep]
type = ADZryAnisoCreepLOCAUpdate
block = cladding
temperature = temperature
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
temperature_loca_creep_begin = 501
temperature_standard_thermal_creep_end = 500
fract_beta_phase_name = 'fract_beta_phase'
[]
[thermal_expansion]
type = ADZryThermalExpansionMATPROEigenstrain
block = cladding
temperature = temperature
stress_free_temperature = 573.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[density]
type = ADDensity
block = cladding
[]
[phase]
type = ADZrPhase
block = cladding
temperature = temperature
numerical_method = 2
[]
[oxidation]
type = ADZryOxidation
boundary = 2
temperature = temperature
clad_inner_radius = 0.00465
clad_outer_radius = 0.005375
normal_operating_temperature_model = epri_kwu_ce
high_temperature_model = leistikow
use_coolant_channel = true
[]
[clad_failure_criterion]
type = ADZryCladdingFailure
boundary = 2
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate_aux
temperature = temperature
fraction_beta_phase = fract_beta_phase
fraction_oxygen_gain = oxywtfgain_total
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = NEWTON
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-06
nl_abs_tol = 1.e-08
start_time = 0
n_startup_steps = 1
end_time = 700.
dtmax = 1.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[Postprocessors]
[ave_clad_exterior_temp]
type = SideAverageValue
boundary = 2
variable = temperature
[]
[max_clad_temp]
type = NodalExtremeValue
block = cladding
value_type = max
variable = temperature
[]
[min_clad_temp]
type = NodalExtremeValue
block = cladding
value_type = min
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = cladding
[]
[max_oxygen_fract]
type = ElementExtremeValue
block = cladding
value_type = max
variable = oxywtfract_total
[]
[max_betaph_fract]
type = ElementExtremeValue
block = cladding
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
block = cladding
value_type = max
variable = creep_rate_aux
[]
[max_creep_strain_mag]
type = ElementExtremeValue
block = cladding
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
block = cladding
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
block = cladding
value_type = max
variable = hoop_stress
[]
[vonmises_stress_clad]
type = ElementAverageValue
block = cladding
variable = vonmises_stress
[]
[min_burst_stress]
type = ElementExtremeValue
block = cladding
value_type = min
variable = burst_stress
[]
[burst]
type = ElementExtremeValue
block = cladding
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = cladding
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[top_disp_r_clad] # this is mid height
type = NodalVariableValue
variable = disp_x
nodeid = 0 #coords (0.005375, 0.1625)
[]
[top_disp_r_clad_slice] # this is mid height matched to the 1.5d
type = NodalVariableValue
variable = disp_x
nodeid = 3 #coords (0.005375, 0.1625)
[]
[top_disp_z_clad]
type = NodalVariableValue
variable = disp_y
nodeid = 0 #coords (0.005375, 0.1625)
[]
[stress_xx] # stess in the top Element
type = ElementalVariableValue
variable = stress_xx
elementid = 0
[]
[stress_yy] # stess in the top Element
type = ElementalVariableValue
variable = stress_yy
elementid = 0
[]
[stress_zz] # stess in the top Element
type = ElementalVariableValue
variable = stress_zz
elementid = 0
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = cladding
plenum_boundary_name = 4
external_clad_boundary_name = 2
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = rebeka_2d_02MPa_aniso_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
(assessment/LWR/validation/LOCA_Hardy_cladding_test/analysis/1pt4MPa/100C_sec/100C_sec_Hardy_Tube_Test_1pt4MPa.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
volumetric_locking_correction = false
displacements = 'disp_x disp_y'
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
group_variables = 'disp_x disp_y'
[]
[Mesh]
coord_type = RZ
patch_size = 10
patch_update_strategy = iteration
partitioner = centroid
centroid_partitioner_direction = y
[gen]
type = FuelPinMeshGenerator
include_fuel = false
include_clad = true
pellet_outer_radius = 0.0072527
clad_gap_width = 0.0
clad_top_gap_height = 0.0
clad_bot_gap_height = 0.0
clad_thickness = 0.38e-3
pellet_height = 0.5
pellet_quantity = 1
clad_mesh_density = customize
nx_c = 2
ny_c = 50
elem_type = QUAD8
[]
[]
[Variables]
[temperature]
initial_condition = 600.0
[]
[]
[AuxVariables]
[creep_rate_aux]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[total_hoop_strain]
order = CONSTANT
family = MONOMIAL
[]
[burst_stress]
order = CONSTANT
family = MONOMIAL
[]
[burst]
order = CONSTANT
family = MONOMIAL
[]
[]
[Functions]
[pressure_function]
type = PiecewiseLinear
x = '0 40'
y = '1 1'
[]
[temp_function]
type = PiecewiseLinear
y = '600 1600'
[]
[temperature_profile]
type = PiecewiseBilinear
y = '0 40'
x = '0 0.25224 0.50448'
z = '0.995 1.01 0.995 0.995 1.01 0.995'
axis = 1
[]
[inner_temperature]
type = CompositeFunction
functions = 'temp_function temperature_profile'
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[clad]
block = clad
add_variables = true
strain = FINITE
decomposition_method = EigenSolution
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz elastic_strain_xx elastic_strain_yy elastic_strain_zz
creep_strain_xx creep_strain_yy creep_strain_zz hoop_stress'
extra_vector_tags = 'ref'
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
extra_vector_tags = 'ref'
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
extra_vector_tags = 'ref'
[]
[]
[AuxKernels]
[creep_rate_aux]
type = MaterialRealAux
variable = creep_rate_aux
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[creep_rate]
type = MaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[total_hoop_strain]
type = RankTwoAux
rank_two_tensor = total_strain
variable = total_hoop_strain
index_i = 2
index_j = 2
execute_on = timestep_end
block = clad
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = clad_outside_right
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = clad_outside_right
execute_on = timestep_end
[]
[]
[BCs]
[Pressure]
[outer_surface]
boundary = 'clad_outside_bottom clad_outside_right clad_outside_top'
factor = 0.0
function = pressure_function
[]
[inner_surface]
boundary = 'clad_inside_right clad_inside_bottom clad_inside_top'
function = pressure_function
[]
[]
[u_bottom_fix]
type = DirichletBC
variable = disp_y
boundary = 1001
value = 0.0
[]
[x_fix]
type = DirichletBC
variable = disp_x
boundary = centerline
value = 0.0
[]
[temp_bc]
type = FunctionDirichletBC
function = inner_temperature
variable = temperature
boundary = 'clad_inside_bottom clad_inside_right clad_inside_top'
[]
[]
[Materials]
[clad_thermal]
type = ZryThermal
block = clad
zry_thermal_properties_model = MATPRO
temperature = temperature
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = clad
matpro_youngs_modulus = true
matpro_poissons_ratio = true
temperature = temperature
[]
[clad_stress]
type = ComputeMultipleInelasticStress
inelastic_models = 'clad_zrycreep'
block = clad
tangent_operator = nonlinear
[]
[clad_zrycreep]
type = ZryCreepLOCAUpdate
block = clad
temperature = temperature
model_irradiation_creep = false
model_primary_creep = true
model_thermal_creep = true
temperature_loca_creep_begin = 840 # values from the report
temperature_standard_thermal_creep_end = 975
[]
[thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = clad
temperature = temperature
stress_free_temperature = 600.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[clad_density]
type = Density
block = clad
density = 6550.0
[]
[phase]
type = ZrPhase
block = clad
temperature = temperature
numerical_method = 2
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = clad_outside_right
failure_criterion = combined_overstress_and_overstrain
hoop_stress = hoop_stress
hoop_creep_strain = creep_strain_zz
effective_strain_rate_creep = creep_rate_aux
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.0e-5
nl_abs_tol = 1.0e-8
start_time = 0
n_startup_steps = 1
end_time = 40
dtmax = 1
dtmin = 0.0000001
[TimeStepper]
type = IterationAdaptiveDT
timestep_limiting_postprocessor = material_timestep
dt = 1.0
[]
[]
[Postprocessors]
[ave_clad_temp]
type = SideAverageValue
boundary = clad_outside_right
variable = temperature
[]
[gas_volume]
type = InternalVolume
boundary = all_clad_interior
execute_on = 'initial linear'
[]
[max_clad_temp]
type = NodalExtremeValue
block = clad
value_type = max
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = clad
[]
[max_hoop_stress]
type = ElementExtremeValue
block = clad
value_type = max
variable = hoop_stress
[]
[vonmises_stress_clad]
type = ElementAverageValue
block = clad
variable = vonmises_stress
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = total_hoop_strain
[]
[max_disp_x]
type = NodalExtremeValue
block = clad
value_type = max
variable = disp_x
[]
[min_burst_stress]
type = ElementExtremeValue
block = clad
value_type = min
variable = burst_stress
[]
[burst]
type = ElementExtremeValue
block = clad
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = clad
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
[]
[PerformanceMetricOutputs]
[]
[Outputs]
color = false
perf_graph = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[csv]
type = CSV
[]
[chkfile]
type = CSV
show = 'max_disp_x max_hoop_stress vonmises_stress_clad'
execute_on = 'FINAL'
[]
[]
[UserObjects]
[terminator1]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '5'
include_fuel = false
[]
[]
(assessment/LWR/validation/LOCA_Hardy_cladding_test/analysis/0pt5MPa/25C_sec/25C_sec_Hardy_Tube_Test_0pt5MPa.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
volumetric_locking_correction = false
displacements = 'disp_x disp_y'
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
group_variables = 'disp_x disp_y'
[]
[Mesh]
coord_type = RZ
patch_size = 10
patch_update_strategy = iteration
partitioner = centroid
centroid_partitioner_direction = y
[gen]
type = FuelPinMeshGenerator
include_fuel = false
include_clad = true
pellet_outer_radius = 0.0072527
clad_gap_width = 0.0
clad_top_gap_height = 0.0
clad_bot_gap_height = 0.0
clad_thickness = 0.38e-3
pellet_height = 0.5
pellet_quantity = 1
clad_mesh_density = customize
nx_c = 2
ny_c = 50
elem_type = QUAD8
[]
[]
[Variables]
[temperature]
initial_condition = 600.0
[]
[]
[AuxVariables]
[creep_rate_aux]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[total_hoop_strain]
order = CONSTANT
family = MONOMIAL
[]
[burst_stress]
order = CONSTANT
family = MONOMIAL
[]
[burst]
order = CONSTANT
family = MONOMIAL
[]
[]
[Functions]
[pressure_function]
type = PiecewiseLinear
x = '0 40'
y = '1 1'
[]
[temp_function]
type = PiecewiseLinear
y = '600 1600'
[]
[temperature_profile]
type = PiecewiseBilinear
y = '0 40'
x = '0 0.25224 0.50448'
z = '0.995 1.01 0.995 0.995 1.01 0.995'
axis = 1
[]
[inner_temperature]
type = CompositeFunction
functions = 'temp_function temperature_profile'
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[clad]
block = clad
add_variables = true
strain = FINITE
decomposition_method = EigenSolution
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz elastic_strain_xx elastic_strain_yy elastic_strain_zz
creep_strain_xx creep_strain_yy creep_strain_zz hoop_stress'
extra_vector_tags = 'ref'
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
extra_vector_tags = 'ref'
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
extra_vector_tags = 'ref'
[]
[]
[AuxKernels]
[creep_rate_aux]
type = MaterialRealAux
variable = creep_rate_aux
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[creep_rate]
type = MaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[total_hoop_strain]
type = RankTwoAux
rank_two_tensor = total_strain
variable = total_hoop_strain
index_i = 2
index_j = 2
execute_on = timestep_end
block = clad
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = clad_outside_right
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = clad_outside_right
execute_on = timestep_end
[]
[]
[BCs]
[Pressure]
[outer_surface]
boundary = 'clad_outside_bottom clad_outside_right clad_outside_top'
factor = 0.0
function = pressure_function
[]
[inner_surface]
boundary = 'clad_inside_right clad_inside_bottom clad_inside_top'
function = pressure_function
[]
[]
[u_bottom_fix]
type = DirichletBC
variable = disp_y
boundary = 1001
value = 0.0
[]
[x_fix]
type = DirichletBC
variable = disp_x
boundary = centerline
value = 0.0
[]
[temp_bc]
type = FunctionDirichletBC
function = inner_temperature
variable = temperature
boundary = 'clad_inside_bottom clad_inside_right clad_inside_top'
[]
[]
[Materials]
[clad_thermal]
type = ZryThermal
block = clad
zry_thermal_properties_model = MATPRO
temperature = temperature
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = clad
matpro_youngs_modulus = true
matpro_poissons_ratio = true
temperature = temperature
[]
[clad_stress]
type = ComputeMultipleInelasticStress
inelastic_models = 'clad_zrycreep'
block = clad
tangent_operator = nonlinear
[]
[clad_zrycreep]
type = ZryCreepLOCAUpdate
block = clad
temperature = temperature
model_irradiation_creep = false
model_primary_creep = true
model_thermal_creep = true
temperature_loca_creep_begin = 840 # values from the report
temperature_standard_thermal_creep_end = 975
[]
[thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = clad
temperature = temperature
stress_free_temperature = 600.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[clad_density]
type = Density
block = clad
density = 6550.0
[]
[phase]
type = ZrPhase
block = clad
temperature = temperature
numerical_method = 2
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = clad_outside_right
failure_criterion = combined_overstress_and_overstrain
hoop_stress = hoop_stress
hoop_creep_strain = creep_strain_zz
effective_strain_rate_creep = creep_rate_aux
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.0e-5
nl_abs_tol = 1.0e-8
start_time = 0
n_startup_steps = 1
end_time = 40
dtmax = 1
dtmin = 0.0000001
[TimeStepper]
type = IterationAdaptiveDT
timestep_limiting_postprocessor = material_timestep
dt = 1.0
[]
[]
[Postprocessors]
[ave_clad_temp]
type = SideAverageValue
boundary = clad_outside_right
variable = temperature
[]
[gas_volume]
type = InternalVolume
boundary = all_clad_interior
execute_on = 'initial linear'
[]
[max_clad_temp]
type = NodalExtremeValue
block = clad
value_type = max
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = clad
[]
[max_hoop_stress]
type = ElementExtremeValue
block = clad
value_type = max
variable = hoop_stress
[]
[vonmises_stress_clad]
type = ElementAverageValue
block = clad
variable = vonmises_stress
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = total_hoop_strain
[]
[max_disp_x]
type = NodalExtremeValue
block = clad
value_type = max
variable = disp_x
[]
[min_burst_stress]
type = ElementExtremeValue
block = clad
value_type = min
variable = burst_stress
[]
[burst]
type = ElementExtremeValue
block = clad
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = clad
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
[]
[PerformanceMetricOutputs]
[]
[Outputs]
color = false
perf_graph = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[csv]
type = CSV
[]
[chkfile]
type = CSV
show = 'max_disp_x max_hoop_stress vonmises_stress_clad'
execute_on = 'FINAL'
[]
[]
[UserObjects]
[terminator1]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '5'
include_fuel = false
[]
[]
(assessment/LWR/validation/RIA_NSRR_FK/analysis/FK1/FK01.i)
# This file was created using BIF with the following inputs:
# FK01.var - md5sum: 123016ae8f3283a45bae816a366f93b1
# ../pulse_rev1.tpl - md5sum: 8d6b8b4bce1dd830dea2d8522009e514
[GlobalParams]
density = 10020.6066633
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
energy_per_fission = 3.2e-11
a_lower = 0.01822
a_upper = 0.12422
temperature = temp
volumetric_locking_correction = false
[]
[Mesh]
coord_type = RZ
[smeared_pellet_mesh]
type = FuelPinMeshGenerator
clad_mesh_density = customize
pellet_mesh_density = customize
elem_type = QUAD8
ny_p = 100
nx_c = 4
ny_c = 100
nx_p = 12
ny_cu = 3
ny_cl = 3
bx_p = 0.75
clad_bot_gap_height = 0.00152
bottom_clad_height = 0.0167
top_clad_height = 0.0167
clad_thickness = 0.00086
pellet_outer_radius = 0.00527
clad_top_gap_height = 0.04298
pellet_height = 0.106
clad_gap_width = 1e-05
pellet_quantity = 1
[]
patch_size = 5
patch_update_strategy = auto
partitioner = centroid
centroid_partitioner_direction = y
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
[]
[Variables]
[temp]
initial_condition = 293
[]
[]
[AuxVariables]
[BuTC]
[]
[gap]
order = CONSTANT
family = MONOMIAL
[]
[fast_neutron_flux]
block = 1
[]
[fast_neutron_fluence]
block = 1
[]
[buavg]
order = CONSTANT
family = MONOMIAL
[]
[fission_rate]
initial_condition = 0
[]
[grain_radius]
block = 3
initial_condition = 5.96e-6
[]
[integral_burnup]
order = CONSTANT
family = MONOMIAL
[]
[pellet_id]
order = CONSTANT
family = MONOMIAL
block = 3
[]
[gap_conductivity]
order = CONSTANT
family = MONOMIAL
[]
[porosity]
order = CONSTANT
family = MONOMIAL
initial_condition = 0.085711070864
[]
[SED]
order = CONSTANT
family = MONOMIAL
[]
[]
[Functions]
[linear_heat_rate_profile]
type = PiecewiseLinear
data_file = pulse.csv
format = columns
[]
[flux]
type = ConstantFunction
value = 0.0
[]
[axial_peaking_factors]
type = ConstantFunction
value = 1
[]
[coolant_pressure_ramp]
type = ConstantFunction
value = 101325
[]
[linear_heat_generation_rate]
type = CompositeFunction
functions = 'linear_heat_rate_profile axial_peaking_factors'
[]
[axial_flux]
type = CompositeFunction
functions = 'flux axial_peaking_factors'
[]
[burnup_thermal_conductivity]
type = ConstantFunction
value = 0.0473684210526 # should be burnup / 950
[]
[radial_power_profile]
type = PiecewiseBilinear
data_file = RadialPowerProfile.csv
axis = 0
[]
[radial_burnup_profile]
type = PiecewiseBilinear
data_file = RadialBurnupProfile.csv
axis = 0
[]
[initial_burnup]
type = CompositeFunction
functions = 'burnup_thermal_conductivity radial_burnup_profile'
[]
[]
[Burnup]
[burnup]
block = 3
rod_ave_lin_pow = linear_heat_rate_profile
axial_power_profile = axial_peaking_factors
rpf_input = radial_power_profile
num_radial = 80
num_axial = 49
fuel_inner_radius = 0.0
fuel_outer_radius = 0.00527
fuel_volume_ratio = 1.0
isotopes = 'U235 U238 Pu239 Pu240 Pu241 Pu242'
isotope_fractions = '0.039 0.961 0.0 0.0 0.0 0.0'
[]
[]
[Physics/SolidMechanics/QuasiStatic]
add_variables = true
[fuel]
block = 3
strain = FINITE
incremental = true
eigenstrain_names = 'fuel_thermal_eigenstrain
fuel_volumetric_swelling_eigenstrain'
extra_vector_tags = 'ref'
generate_output = 'vonmises_stress hydrostatic_stress elastic_strain_xx
elastic_strain_yy elastic_strain_zz stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz'
decomposition_method = EigenSolution
[]
[clad]
block = 1
strain = FINITE
incremental = true
eigenstrain_names = 'clad_thermal_eigenstrain'
extra_vector_tags = 'ref'
generate_output = 'vonmises_stress elastic_strain_xx
elastic_strain_yy elastic_strain_zz stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz creep_strain_xx creep_strain_yy creep_strain_zz'
decomposition_method = EigenSolution
[]
[]
[Kernels]
[gravity]
type = Gravity
variable = disp_y
value = -9.81
extra_vector_tags = 'ref'
[]
[heat]
type = HeatConduction
variable = temp
extra_vector_tags = 'ref'
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temp
extra_vector_tags = 'ref'
[]
[heat_source]
type = NeutronHeatSource
fission_rate = fission_rate
variable = temp
block = 3
extra_vector_tags = 'ref'
[]
[]
[AuxKernels]
[BuTC]
type = FunctionAux
block = 3
variable = BuTC
function = initial_burnup
[]
[pelletid]
type = PelletIdAux
block = 3
variable = pellet_id
number_pellets = 1
execute_on = initial
[]
[gap]
type = SpatialUserObjectAux
block = 3
variable = gap
execute_on = timestep_end
user_object = avg_gap
[]
[buavg]
type = SpatialUserObjectAux
block = 3
variable = buavg
execute_on = timestep_end
user_object = integral_burnup
[]
[fast_neutron_flux]
type = FastNeutronFluxAux
variable = fast_neutron_flux
function = axial_flux
block = 1
execute_on = timestep_begin
[]
[fast_neutron_fluence]
type = FastNeutronFluenceAux
variable = fast_neutron_fluence
block = 1
fast_neutron_flux = fast_neutron_flux
execute_on = timestep_begin
[]
[fuel_porosity]
type = PorosityAuxUO2
block = 3
variable = porosity
execute_on = timestep_begin
[]
[grain_radius]
type = GrainRadiusAux
block = 3
variable = grain_radius
temperature = temp
execute_on = timestep_begin
[]
[gap_conductance]
type = MaterialRealAux
property = gap_conductance
variable = gap_conductivity
boundary = 10
[]
[SED]
type = MaterialRealAux
variable = SED
property = strain_energy_density
execute_on = timestep_end
block = 1
[]
[]
[Contact]
[pellet_clad_mechanical]
primary = 5
secondary = 10
penalty = 1e14
normalize_penalty = true
model = frictionless
friction_coefficient = 2.5
normal_smoothing_distance = 0.1
formulation = penalty
[]
[]
[ThermalContact]
[thermal_contact]
type = GasGapHeatTransfer
variable = temp
primary = 5
secondary = 10
roughness_coef = 3.2
roughness_primary = 1.5e-6
roughness_secondary = 1.75e-6
jump_distance_model = LANNING
plenum_pressure = plenum_pressure
contact_pressure = contact_pressure
initial_moles = initial_moles
gas_released = fission_gas_released
tangential_tolerance = 1.0e-6
quadrature = true
[]
[]
[BCs]
[no_x_all]
type = DirichletBC
variable = disp_x
boundary = 12
value = 0.0
[]
[no_y_fuel_bottom]
type = DirichletBC
variable = disp_y
boundary = 20
value = 0.0
[]
[no_y_clad_bottom]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[]
[coolant_temp]
type = DirichletBC
boundary = '1 2 3'
variable = temp
value = 293
[]
[Pressure]
[coolantPressure]
boundary = '1 2 3'
factor = 1
function = coolant_pressure_ramp
[]
[]
[PlenumPressure]
[plenumPressure]
boundary = '10 5'
initial_pressure = 0.3e6
startup_time = 0
R = 8.314462
output_initial_moles = initial_moles
temperature = plenum_temperature
volume = plenum_volume
material_input = fission_gas_released
output = plenum_pressure
initial_temperature = 293
[]
[]
[]
[Materials]
[fuel_swelling]
type = UO2VolumetricSwellingEigenstrain
block = 3
burnup = burnup
initial_fuel_density = 10020.6066633
total_densification = 0.006
gas_swelling_model_type = SIFGRS
eigenstrain_name = 'fuel_volumetric_swelling_eigenstrain'
[]
[fuel_thermal]
type = UO2Thermal
thermal_conductivity_model = NFIR
block = 3
temperature = temp
burnup = BuTC
initial_porosity = 0.085711070864
[]
[fuel_elasticity_tensor]
type = UO2ElasticityTensor
block = 3
[]
[fuel_thermal_expansion]
type = UO2ThermalExpansionMartinEigenstrain
block = 3
stress_free_temperature = 293
eigenstrain_name = 'fuel_thermal_eigenstrain'
[]
[fuel_elastic_stress]
type = ComputeFiniteStrainElasticStress
block = 3
[]
[clad_thermal]
type = ZryThermal
block = 1
temperature = temp
[]
[clad_inelastic_stress]
type = ComputeMultipleInelasticStress
block = 1
tangent_operator = elastic
inelastic_models ='plasticity'
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = 1
fast_neutron_fluence = fast_neutron_fluence
initial_fast_fluence = 8.40e25
cold_work_factor = 0.01
matpro_youngs_modulus = true
matpro_poissons_ratio = true
[]
## TODO: Creep is not active, but is transfered from the SM version.
## Adding creep causes the Peak Hoop strain to best match the FALCON
## results given by R. Montgomery and D. Sunderland. Only retaining
## plasticity matches the results from Wenfeng Liu, John Alvis, Robert Montgomery, and Ken Yueh
[clad_creep_stress]
type = ZryCreepLimbackHoppeUpdate
block = 1
fast_neutron_flux = fast_neutron_flux
fast_neutron_fluence = fast_neutron_fluence
initial_fast_fluence = 8.40e25
[]
[clad_thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 293.0
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[plasticity]
type = ZryPlasticityUpdate
block = 1
initial_fast_fluence = 8.40e25
fast_neutron_flux = fast_neutron_flux
fast_neutron_fluence = fast_neutron_fluence
cold_work_factor = 0.01
plasticity_model_type = MATPRO
output_properties = yield_stress
outputs = all
zircaloy_alloy_type = 4
[]
[fission_gas_release]
type = UO2Sifgrs
block = 3
temperature = temp
fission_rate = fission_rate
grain_radius = grain_radius
gbs_model = true
burnup = BuTC
transient_option = MICROCRACKING
[]
[clad_density]
type = Density
block = 1
density = 6551
[]
[fuel_density]
type = Density
block = 3
[]
[strain_energy_density]
type = StrainEnergyDensity
block = 1
incremental = true
[]
[]
[UserObjects]
[avg_gap]
type = LayeredAverage
block = 3
variable = penetration
direction = y
num_layers = 48
[]
[pbz]
type = PelletBrittleZone
block = 3
pellet_id = pellet_id
temperature = temp
pellet_radius = 0.00527
number_pellets = 1
execute_on = timestep_begin
[]
[integral_burnup]
type = LayeredAverage
block = 3
variable = burnup
direction = y
num_layers = 1
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
l_max_its = 40
l_tol = 8e-3
nl_max_its = 40
nl_rel_tol = 1e-3
nl_abs_tol = 1e-10
dtmin = 0.00001
dtmax = 1.0
start_time = 0
end_time = 100
[TimeStepper]
type = IterationAdaptiveDT
dt = 0.0001
optimal_iterations = 200
linear_iteration_ratio = 100
timestep_limiting_function = linear_heat_rate_profile
max_function_change = 500000
force_step_every_function_point = true
[]
[]
[Dampers]
[limitT]
type = MaxIncrement
max_increment = 100.0
variable = temp
[]
[limitX]
type = MaxIncrement
max_increment = 1e-5
variable = disp_x
[]
[contactslip]
type = ContactSlipDamper
primary = 5
secondary = 8
min_damping_factor = 0.05
[]
[]
[Postprocessors]
[max_hoop_strain]
type = ElementExtremeValue
variable = strain_zz
block = 1
[]
[max_SED]
type = ElementExtremeValue
variable = SED
block = 1
[]
[average_grain_radius]
type = ElementAverageValue
block = 3
outputs = 'exodus'
variable = grain_radius
[]
[clad_inner_vol]
type = InternalVolume
boundary = 7
outputs = 'exodus'
execute_on = 'timestep_begin initial'
[]
[flux_from_clad]
type = SideDiffusiveFluxIntegral
variable = temp
boundary = 5
diffusivity = thermal_conductivity
outputs = 'exodus'
[]
[flux_from_fuel]
type = SideDiffusiveFluxIntegral
variable = temp
boundary = 10
diffusivity = thermal_conductivity
outputs = 'exodus'
[]
[rod_total_power]
type = ElementIntegralPower
variable = temp
fission_rate = fission_rate
block = 3
[]
[rod_input_power]
type = FunctionValuePostprocessor
function = linear_heat_rate_profile
scale_factor = 0.106
[]
[average_fission_rate]
type = ElementAverageValue
variable = fission_rate
block = '3'
[]
[RAE]
type = RadialAverageEnthalpy
vector_postprocessor = rad_temp
radial_direction = x
axial_direction = y
axial_position = 0.0503
temperature_name = temp
[]
[peak_RAE]
type = TimeExtremeValue
postprocessor = RAE
[]
[]
[VectorPostprocessors]
[rad_temp]
type = NodalValueSampler
block = 3
sort_by = y
variable = temp
execute_on = timestep_end
outputs = dummy
[]
[]
[StandardLWRFuelRodOutputs]
fuel_pellet_blocks = 3
cladding_blocks = 1
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[chkfile]
type = CSV
show = 'average_centerline_fuel_temperature average_fission_rate fission_gas_released_percentage peak_RAE rod_total_power'
execute_on = 'FINAL'
[]
[console]
type = Console
max_rows = 25
output_linear = true
[]
[dummy]
type = CSV
enable = false
[]
[]
(assessment/LWR/validation/LOCA_Hardy_cladding_test/analysis/0pt3MPa/25C_sec/25C_sec_Hardy_Tube_Test_0pt3MPa.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
volumetric_locking_correction = false
displacements = 'disp_x disp_y'
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
group_variables = 'disp_x disp_y'
[]
[Mesh]
coord_type = RZ
patch_size = 10
patch_update_strategy = iteration
partitioner = centroid
centroid_partitioner_direction = y
[gen]
type = FuelPinMeshGenerator
include_fuel = false
include_clad = true
pellet_outer_radius = 0.0072527
clad_gap_width = 0.0
clad_top_gap_height = 0.0
clad_bot_gap_height = 0.0
clad_thickness = 0.38e-3
pellet_height = 0.5
pellet_quantity = 1
clad_mesh_density = customize
nx_c = 2
ny_c = 50
elem_type = QUAD8
[]
[]
[Variables]
[temperature]
initial_condition = 600.0
[]
[]
[AuxVariables]
[creep_rate_aux]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[total_hoop_strain]
order = CONSTANT
family = MONOMIAL
[]
[burst_stress]
order = CONSTANT
family = MONOMIAL
[]
[burst]
order = CONSTANT
family = MONOMIAL
[]
[]
[Functions]
[pressure_function]
type = PiecewiseLinear
x = '0 40'
y = '1 1'
[]
[temp_function]
type = PiecewiseLinear
y = '600 1600'
[]
[temperature_profile]
type = PiecewiseBilinear
y = '0 40'
x = '0 0.25224 0.50448'
z = '0.995 1.01 0.995 0.995 1.01 0.995'
axis = 1
[]
[inner_temperature]
type = CompositeFunction
functions = 'temp_function temperature_profile'
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[clad]
block = clad
add_variables = true
strain = FINITE
decomposition_method = EigenSolution
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz elastic_strain_xx elastic_strain_yy elastic_strain_zz
creep_strain_xx creep_strain_yy creep_strain_zz hoop_stress'
extra_vector_tags = 'ref'
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
extra_vector_tags = 'ref'
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
extra_vector_tags = 'ref'
[]
[]
[AuxKernels]
[creep_rate_aux]
type = MaterialRealAux
variable = creep_rate_aux
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[creep_rate]
type = MaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[total_hoop_strain]
type = RankTwoAux
rank_two_tensor = total_strain
variable = total_hoop_strain
index_i = 2
index_j = 2
execute_on = timestep_end
block = clad
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = clad_outside_right
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = clad_outside_right
execute_on = timestep_end
[]
[]
[BCs]
[Pressure]
[outer_surface]
boundary = 'clad_outside_bottom clad_outside_right clad_outside_top'
factor = 0.0
function = pressure_function
[]
[inner_surface]
boundary = 'clad_inside_right clad_inside_bottom clad_inside_top'
function = pressure_function
[]
[]
[u_bottom_fix]
type = DirichletBC
variable = disp_y
boundary = 1001
value = 0.0
[]
[x_fix]
type = DirichletBC
variable = disp_x
boundary = centerline
value = 0.0
[]
[temp_bc]
type = FunctionDirichletBC
function = inner_temperature
variable = temperature
boundary = 'clad_inside_bottom clad_inside_right clad_inside_top'
[]
[]
[Materials]
[clad_thermal]
type = ZryThermal
block = clad
zry_thermal_properties_model = MATPRO
temperature = temperature
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = clad
matpro_youngs_modulus = true
matpro_poissons_ratio = true
temperature = temperature
[]
[clad_stress]
type = ComputeMultipleInelasticStress
inelastic_models = 'clad_zrycreep'
block = clad
tangent_operator = nonlinear
[]
[clad_zrycreep]
type = ZryCreepLOCAUpdate
block = clad
temperature = temperature
model_irradiation_creep = false
model_primary_creep = true
model_thermal_creep = true
temperature_loca_creep_begin = 840 # values from the report
temperature_standard_thermal_creep_end = 975
[]
[thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = clad
temperature = temperature
stress_free_temperature = 600.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[clad_density]
type = Density
block = clad
density = 6550.0
[]
[phase]
type = ZrPhase
block = clad
temperature = temperature
numerical_method = 2
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = clad_outside_right
failure_criterion = combined_overstress_and_overstrain
hoop_stress = hoop_stress
hoop_creep_strain = creep_strain_zz
effective_strain_rate_creep = creep_rate_aux
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.0e-5
nl_abs_tol = 1.0e-8
start_time = 0
n_startup_steps = 1
end_time = 40
dtmax = 1
dtmin = 0.0000001
[TimeStepper]
type = IterationAdaptiveDT
timestep_limiting_postprocessor = material_timestep
dt = 1.0
[]
[]
[Postprocessors]
[ave_clad_temp]
type = SideAverageValue
boundary = clad_outside_right
variable = temperature
[]
[gas_volume]
type = InternalVolume
boundary = all_clad_interior
execute_on = 'initial linear'
[]
[max_clad_temp]
type = NodalExtremeValue
block = clad
value_type = max
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = clad
[]
[max_hoop_stress]
type = ElementExtremeValue
block = clad
value_type = max
variable = hoop_stress
[]
[vonmises_stress_clad]
type = ElementAverageValue
block = clad
variable = vonmises_stress
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = total_hoop_strain
[]
[max_disp_x]
type = NodalExtremeValue
block = clad
value_type = max
variable = disp_x
[]
[min_burst_stress]
type = ElementExtremeValue
block = clad
value_type = min
variable = burst_stress
[]
[burst]
type = ElementExtremeValue
block = clad
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = clad
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
[]
[PerformanceMetricOutputs]
[]
[Outputs]
color = false
perf_graph = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[csv]
type = CSV
[]
[chkfile]
type = CSV
show = 'max_disp_x max_hoop_stress vonmises_stress_clad'
execute_on = 'FINAL'
[]
[]
[UserObjects]
[terminator1]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '5'
include_fuel = false
[]
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-11/puzry-11_aniso.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-11.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 1200. '
y = '1.e+05 1.e+05 1.534e+06' # Linear increase at 0.0717 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 1200. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
# Circumferential steady-state creep test and analysis of Zircaloy-4 fuel cladding
# Nuclear Engineering and Design, 53, 2312-2322 (2021)
[F]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.738 0.738 0.57'
[]
[G]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.174 0.174 0.45'
[]
[H]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.588 0.588 0.48'
[]
[L]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[M]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[N]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = TaylorExpansion
use_automatic_differentiation = true
[]
[]
[]
[]
[Kernels]
[heat]
type = ADHeatConduction
variable = temperature
[]
[heat_ie]
type = ADHeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = ADMaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = ADMaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = ADMaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = ADMaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = ADMaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = ADFunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = ADDirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = ADDirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ADZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1.e+11
poissons_ratio = 0.3
block = 1
[]
[hill_constants]
type = ADHillConstants
hill_constants = "0.738 0.174 0.588 1.0 1.0 1.0"
function_names = "F G H L M N"
temperature = temperature
[]
[creep_update]
type = ADZryAnisoCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 1.5e-05
temperature = temperature
temperature_standard_thermal_creep_end = 700
temperature_loca_creep_begin = 900.
fract_beta_phase_name = 'fract_beta_phase'
max_integration_error = 1000000.0
absolute_tolerance = 1e-13
relative_tolerance = 1e-11
[]
[creep]
type = ADComputeMultipleInelasticStress
block = 1
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ADZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = ADDensity
block = 1
[]
[phase]
type = ADZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ADZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = NEWTON
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0.
n_startup_steps = 1
end_time = 2500.
dtmax = 1.
dtmin = 1.0e-9
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-11_aniso_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/LOCA_Studsvik/analysis/rod_196/Studsvik_196_part1.i)
[GlobalParams]
density = 10431.0
initial_porosity = 0.05
order = SECOND
family = LAGRANGE
energy_per_fission = 3.2e-11 # J/fission
volumetric_locking_correction = false
displacements = 'disp_x disp_y'
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
[]
[Mesh]
coord_type = RZ
[smeared_mesh]
type = FuelPinMeshGenerator
clad_top_gap_height = 0.0248576
pellet_height = 0.2606424
pellet_quantity = 1
clad_bot_gap_height = 0.0145
pellet_outer_radius = 3.92e-3
clad_gap_width = 80e-6
clad_thickness = 0.57e-3
clad_mesh_density = customize
pellet_mesh_density = customize
nx_c = 5
ny_c = 50
nx_p = 11
ny_p = 60
elem_type = QUAD8
[]
patch_update_strategy = auto
patch_size = 10 # For contact algorithm
partitioner = centroid
centroid_partitioner_direction = y
[]
[Variables]
# Define dependent variables and initial conditions
[temperature]
initial_condition = 295.0 # set initial temp to coolant inlet
[]
[]
[AuxVariables]
# Define auxilary variables
[fast_neutron_flux]
block = clad
[]
[fast_neutron_fluence]
block = clad
[]
[grain_radius]
block = pellet
initial_condition = 10e-6
[]
[creep_strain_rate]
order = CONSTANT
family = MONOMIAL
[]
[effective_creep_strain]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[hoop_strain]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[scale_thickness] # ZrO2 scale thickness (m)
order = CONSTANT
family = MONOMIAL
[]
[oxywtfract_total] # Current oxigen weight fraction (oxide+metal) (/)
order = CONSTANT
family = MONOMIAL
[]
[oxywtfgain_total] # Gained oxygen weight fraction (oxide+metal) (/)
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[gap_cond]
order = CONSTANT
family = MONOMIAL
[]
[]
[Functions]
[power_history]
type = PiecewiseLinear
data_file = power_history.csv
format = columns
scale_factor = 1
[]
[axial_peaking_factors]
type = ParsedFunction
expression = 1
[]
[pressure_ramp] # reads and interpolates input data defining amplitude curve for fill gas pressure
type = PiecewiseLinear
x = '-200 0 86400 47386400 47472800 47559200 47645600 94945600 95032000'
y = '0.0065371 1 1 1 1 1 1 1 0.0065371'
scale_factor = 15.5e6
[]
[forced_times]
type = PiecewiseLinear
data_file = timestep_limiting.csv
scale_factor = 1
format = columns
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[fuel]
block = pellet
add_variables = true
strain = FINITE
eigenstrain_names = 'fuel_thermal_eigenstrain fuel_relocation_eigenstrain fuel_volumetric_eigenstrain'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz'
decomposition_method = EigenSolution
extra_vector_tags = 'ref'
temperature = temperature
[]
[clad]
block = clad
add_variables = true
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain clad_irradiation_eigenstrain'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz creep_strain_zz strain_zz'
extra_vector_tags = 'ref'
decomposition_method = EigenSolution
temperature = temperature
[]
[]
[Kernels]
[gravity]
type = Gravity
variable = disp_y
value = -9.81
[]
[heat]
type = HeatConduction
variable = temperature
extra_vector_tags = 'ref'
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
extra_vector_tags = 'ref'
[]
[heat_source]
type = NeutronHeatSource
variable = temperature
extra_vector_tags = 'ref'
block = pellet
burnup_function = burnup
[]
[]
[Burnup]
[burnup]
block = pellet
rod_ave_lin_pow = power_history # using the power function defined above
axial_power_profile = axial_peaking_factors # using the axial power profile function defined above
num_radial = 80
num_axial = 11
fuel_pin_geometry = fuel_pin_geometry
fuel_volume_ratio = 1.0 # for use with dished pellets (ratio of actual volume to cylinder volume)
order = CONSTANT
family = MONOMIAL
RPF = RPF
isotopes = 'U235 U238 Pu239 Pu240 Pu241 Pu242'
isotope_fractions = '0.05 0.95 0 0 0 0'
[]
[]
[AuxKernels]
# Define auxilliary kernels for each of the aux variables
[fast_neutron_flux]
type = FastNeutronFluxAux
variable = fast_neutron_flux
block = clad
rod_ave_lin_pow = power_history
axial_power_profile = axial_peaking_factors
factor = 3e13
execute_on = timestep_begin
[]
[fast_neutron_fluence]
type = FastNeutronFluenceAux
variable = fast_neutron_fluence
block = clad
fast_neutron_flux = fast_neutron_flux
execute_on = timestep_begin
[]
[grain_radius]
type = GrainRadiusAux
block = pellet
variable = grain_radius
temperature = temperature
execute_on = linear
[]
[creep_strain_rate]
type = MaterialRealAux
property = creep_rate
variable = creep_strain_rate
block = clad
[]
[effective_creep_strain]
type = MaterialRealAux
property = effective_creep_strain
variable = effective_creep_strain
block = clad
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
block = clad
variable = fract_beta_phase
property = fract_beta_phase
[]
[scl_thickness]
type = MaterialRealAux
boundary = 2
variable = scale_thickness
property = oxide_scale_thickness
[]
[ofract_total]
type = MaterialRealAux
boundary = 2
variable = oxywtfract_total
property = current_oxygen_weight_frac_total
[]
[ofgain_total]
type = MaterialRealAux
boundary = 2
variable = oxywtfgain_total
property = oxygen_weight_frac_gained_total
[]
[sigmaburst]
type = MaterialRealAux
boundary = 2
variable = burst_stress
property = burst_stress
[]
[hasburst]
type = MaterialRealAux
boundary = 2
variable = burst
property = failed
execute_on = timestep_end
[]
[conductance]
type = MaterialRealAux
property = gap_conductance
variable = gap_cond
boundary = 10
execute_on = 'linear'
[]
[]
[Contact]
[pellet_clad_mechanical]
primary = 5
secondary = 10
formulation = kinematic
model = frictionless
penalty = 1e7
[]
[]
[ThermalContact]
[thermal_contact]
type = GasGapHeatTransfer
variable = temperature
primary = 5
secondary = 10
initial_moles = initial_moles
gas_released = 'fission_gas_released he_prod'
released_gas_types = 'Kr Xe;
He'
released_fractions = '0.153 0.847;
1'
quadrature = true
contact_pressure = contact_pressure
refab_gas_types = He
refab_fractions = 1
refab_time = 95032000
refab_type = 0
[]
[]
[BCs]
[no_x_all]
type = DirichletBC
variable = disp_x
boundary = 12
value = 0.0
[]
[no_y_clad_bottom]
type = DirichletBC
variable = disp_y
boundary = '1'
value = 0.0
[]
[no_y_fuel_bottom]
type = DirichletBC
variable = disp_y
boundary = '1020'
value = 0.0
[]
[Pressure]
[coolantPressure]
boundary = '1 2 3'
function = pressure_ramp
[]
[]
[PlenumPressure]
[plenumPressure]
boundary = 9
initial_pressure = 3.44738e6
startup_time = 0
R = 8.3143
output_initial_moles = initial_moles
temperature = plenum_temp
volume = plenum_volume
material_input = 'fission_gas_released he_prod'
output = plenum_pressure
refab_time = 95032000
refab_pressure = 8.2e6
refab_temperature = 295.0
refab_volume = 1.04e-05
cladding_failure_status = burst
equilibrium_pressure = equilibrium_pressure
additional_volumes = additional_volume
temperature_of_additional_volumes = addition_temperature
[]
[]
[]
[UserObjects]
[fuel_pin_geometry]
type = FuelPinGeometry
[]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[]
[PlenumTemperature]
[plenum_temp]
boundary = 5
inner_surfaces = '5'
outer_surfaces = '10'
temperature = temperature
[]
[]
[CoolantChannel]
[convective_clad_surface] # apply convective boundary to clad outer surface
boundary = 2
variable = temperature
inlet_temperature = 580
inlet_pressure = 15.5e6 # Pa
inlet_massflux = 3800 # kg/m^2-sec
rod_diameter = 0.00914 # m
rod_pitch = 1.26e-2 # m
compute_enthalpy = false
linear_heat_rate = power_history
axial_power_profile = axial_peaking_factors
output_properties = 'coolant_channel_htype coolant_channel_hmode'
[]
[]
[Materials]
[uo2_pulverization]
type = UO2Pulverization
block = pellet
layered_average_contact_pressure = contact_pressure
temperature = temperature
burnup_function = burnup
output_properties = pulverized
outputs = all
[]
# Define material behavior models and input material property data
[fuel_thermal] # temperature and burnup dependent thermal properties of UO2 (BISON kernel)
type = UO2Thermal
block = pellet
thermal_conductivity_model = NFIR
temperature = temperature
burnup_function = burnup
[]
[fuel_elasticity_tensor]
type = UO2IsotropicDamageElasticityTensor
block = pellet
fragmentation_model = BARANI
temperature = temperature
rod_ave_lin_pow = power_history
[]
[fuel_elastic_stress]
type = ComputeMultipleInelasticStress
tangent_operator = elastic
inelastic_models = 'fuel_creep'
block = pellet
[]
[fuel_creep]
type = UO2CreepUpdate
block = pellet
temperature = temperature
fission_rate = fission_rate
initial_grain_radius = 10.0e-6
oxygen_to_metal_ratio = 2.0
[]
[fuel_relocation]
type = UO2RelocationEigenstrain
block = pellet
burnup_function = burnup
fuel_pin_geometry = fuel_pin_geometry
rod_ave_lin_pow = power_history
axial_power_profile = axial_peaking_factors
burnup_relocation_stop = 0.024
relocation_activation1 = 5000
relocation_model = ESCORE_modified
eigenstrain_name = fuel_relocation_eigenstrain
[]
[fuel_thermal_expansion]
type = ComputeThermalExpansionEigenstrain
block = pellet
thermal_expansion_coeff = 10.0e-6
temperature = temperature
stress_free_temperature = 295.0
eigenstrain_name = fuel_thermal_eigenstrain
[]
[fuel_volumetric_swelling]
type = UO2VolumetricSwellingEigenstrain
gas_swelling_model_type = SIFGRS
block = pellet
temperature = temperature
burnup_function = burnup
initial_fuel_density = 10431.0
eigenstrain_name = fuel_volumetric_eigenstrain
[]
[fission_gas_release]
type = UO2Sifgrs
block = pellet
temperature = temperature
burnup_function = burnup
grain_radius = grain_radius
gbs_model = true
[]
[clad_density]
type = Density
block = clad
density = 6550.
[]
[clad_thermal]
block = clad
type = ZryThermal
temperature = temperature
[]
[clad_thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = clad
temperature = temperature
stress_free_temperature = 295.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = clad
temperature = temperature
[]
[zry_thermal_creep]
type = ZryCreepLOCAUpdate
block = clad
temperature = temperature
model_irradiation_creep = true
model_primary_creep = true
model_thermal_creep = true
max_inelastic_increment = 5e-4
fast_neutron_flux = fast_neutron_flux
fast_neutron_fluence = fast_neutron_fluence
zircaloy_material_type = zirlo
[]
[clad_stress]
type = ComputeMultipleInelasticStress
tangent_operator = elastic
inelastic_models = 'zry_thermal_creep'
block = clad
[]
[clad_irradiation_growth]
type = ZryIrradiationGrowthEigenstrain
block = clad
fast_neutron_fluence = fast_neutron_fluence
zircaloy_material_type = zirlo
eigenstrain_name = clad_irradiation_eigenstrain
[]
[clad_phase]
type = ZrPhase
block = clad
temperature = temperature
numerical_method = 2
[]
[clad_oxidation]
type = ZryOxidation
boundary = 2
temperature = temperature
clad_inner_radius = 4.18e-03
clad_outer_radius = 4.75e-03
normal_operating_temperature_model = epri_kwu_ce
high_temperature_model = leistikow
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = 2
failure_criterion = overstrain
# effective_strain_rate_creep = creep_strain_rate
# failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = stress_zz
hoop_creep_strain = creep_strain_zz
fraction_beta_phase = fract_beta_phase
fraction_oxygen_gain = oxywtfract_total
temperature = temperature
[]
[fuel_density]
type = Density
block = pellet
[]
[]
[Dampers]
[limitT]
type = BoundingValueElementDamper
min_value = 290.0
max_value = 3000.0
variable = temperature
[]
[limitX]
type = MaxIncrement
max_increment = 1e-5
variable = disp_x
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
l_max_its = 50
l_tol = 8e-3
nl_max_its = 15
nl_rel_tol = 1e-4
nl_abs_tol = 1e-8
start_time = -10
n_startup_steps = 1
end_time = 95032000
dtmax = 1e6
dtmin = 1e-6
[TimeStepper]
type = IterationAdaptiveDT
timestep_limiting_postprocessor = material_timestep
dt = 10
optimal_iterations = 20
iteration_window = 4
linear_iteration_ratio = 100
growth_factor = 2
cutback_factor = .5
timestep_limiting_function = forced_times
force_step_every_function_point = true
[]
[Quadrature]
order = FIFTH
side_order = SEVENTH
[]
[]
[Postprocessors]
[ave_temp_interior]
type = SideAverageValue
boundary = 9
variable = temperature
execute_on = 'initial linear'
[]
[clad_inner_vol]
type = InternalVolume
boundary = 7
#outputs = exodus
execute_on = 'initial timestep_end'
[]
[fission_gas_produced] # fission gas produced (moles)
type = ElementIntegralFisGasGeneratedSifgrs
block = pellet
execute_on = 'linear'
[]
[fission_gas_grain]
type = ElementIntegralFisGasGrainSifgrs
block = pellet
outputs = exodus
execute_on = 'linear'
[]
[fission_gas_boundary]
type = ElementIntegralFisGasBoundarySifgrs
block = pellet
outputs = exodus
execute_on = 'linear'
[]
[flux_from_clad] # area integrated heat flux from the cladding
type = SideDiffusiveFluxIntegral
variable = temperature
boundary = 5
diffusivity = thermal_conductivity
[]
[flux_from_fuel] # area integrated heat flux from the fuel
type = SideDiffusiveFluxIntegral
variable = temperature
boundary = 10
diffusivity = thermal_conductivity
[]
[rod_total_power]
type = ElementIntegralPower
variable = temperature
burnup_function = burnup
block = pellet
[]
[rod_input_power]
type = FunctionValuePostprocessor
function = power_history
scale_factor = 0.1186 # rod height
[]
[max_fuel_temp]
type = NodalExtremeValue
block = pellet
value_type = max
variable = temperature
[]
[max_clad_temp]
type = NodalExtremeValue
block = clad
value_type = max
variable = temperature
[]
[max_clad_hoop_strain]
type = ElementExtremeValue
block = clad
value_type = max
variable = strain_zz
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = clad
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
block = clad
execute_on = 'initial timestep_end'
[]
[he_prod]
type = IFBAHeProduction
b10_load = 9.27165354e-5
b10_enrich = 0.5
burnup = average_burnup
zrb2_thick = 10e-6
fuel_out_rad = 9.32e-3
ifba_len = 0.3
u235_enrich = 0.05
[]
[volume_pulverized]
type = ElementIntegralMaterialProperty
mat_prop = pulverized
block = pellet
[]
[max_fuel_temp_periphery]
type = NodalExtremeValue
value_type = max
variable = temperature
boundary = 10
[]
[additional_volume]
type = FunctionValuePostprocessor
function = 8.5e-6
execute_on = 'initial linear'
[]
[addition_temperature]
type = FunctionValuePostprocessor
function = 300.0
execute_on = 'initial linear'
[]
[equilibrium_pressure]
type = FunctionValuePostprocessor
function = 101325.0
execute_on = 'initial linear'
[]
[]
[PerformanceMetricOutputs]
[]
[StandardLWRFuelRodOutputs]
temperature = temperature
fuel_pellet_blocks = 3
[]
[Outputs]
perf_graph = true
exodus = true
color = false
csv = true
[checkpoint]
type = Checkpoint
num_files = 2
[]
[chkfile]
type = CSV
execute_on = FINAL
show = 'volume_pulverized'
[]
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-20/puzry-20.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-20.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 2500. '
y = '1.e+05 1.e+05 3.475e+06' # Linear increase at 0.0225 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 2500. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = EigenSolution
[]
[]
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = MaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = FunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = DirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = DirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1.e+11
poissons_ratio = 0.3
block = 1
[]
[creep_update]
type = ZryCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 1.e-04
temperature = temperature
temperature_standard_thermal_creep_end = 700
temperature_loca_creep_begin = 900.
[]
[creep]
type = ComputeMultipleInelasticStress
block = 1
tangent_operator = elastic
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = Density
block = 1
[]
[phase]
type = ZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
active = 'smp'
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0.
n_startup_steps = 1
end_time = 2500.
dtmax = 1.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-20_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/RIA_NSRR_FK/analysis/FK7/FK07.i)
# This file was created using BIF with the following inputs:
# FK06/FK06.var - md5sum: 5a60c05af67ba840a89caacf70b852e2
# pulse.tpl - md5sum: 37e5a6b8a0c63ad020906dada3472585
# Other changes were added after that process.
[GlobalParams]
density = 10310.8809782
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
energy_per_fission = 3.2e-11
a_lower = 0.01822
a_upper = 0.12422
temperature = temp
volumetric_locking_correction = false
[]
[Mesh]
coord_type = RZ
[smeared_pellet_mesh]
type = FuelPinMeshGenerator
clad_mesh_density = customize
pellet_mesh_density = customize
elem_type = QUAD8
ny_p = 100
nx_c = 4
ny_c = 100
nx_p = 12
ny_cu = 3
ny_cl = 3
bx_p = 0.75
clad_bot_gap_height = 0.00152
bottom_clad_height = 0.0167
top_clad_height = 0.0167
clad_thickness = 0.00086
pellet_outer_radius = 0.00527
clad_top_gap_height = 0.05265
pellet_height = 0.106
clad_gap_width = 1e-05
pellet_quantity = 1
[]
patch_size = 5
patch_update_strategy = auto
partitioner = centroid
centroid_partitioner_direction = y
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
converge_on = 'disp_x disp_y temp'
[]
[Variables]
[temp]
initial_condition = 293
block = '1 3'
[]
[]
[AuxVariables]
[BuTC]
[]
[gap]
order = CONSTANT
family = MONOMIAL
[]
[fast_neutron_flux]
block = 1
[]
[fast_neutron_fluence]
block = 1
[]
[buavg]
order = CONSTANT
family = MONOMIAL
[]
[fission_rate]
initial_condition = 0
[]
[grain_radius]
block = 3
initial_condition = 5.96e-6
[]
[integral_burnup]
order = CONSTANT
family = MONOMIAL
[]
[pellet_id]
order = CONSTANT
family = MONOMIAL
block = 3
[]
[porosity]
order = CONSTANT
family = MONOMIAL
initial_condition = 0.0592261881186
[]
[SED]
order = CONSTANT
family = MONOMIAL
[]
[]
[Functions]
[linear_heat_rate_profile]
type = PiecewiseLinear
data_file = pulse.csv
format = columns
[]
[flux]
type = ConstantFunction
value = 0.0
[]
[axial_peaking_factors]
type = ConstantFunction
value = 1
[]
[coolant_pressure_ramp]
type = ConstantFunction
value = 101325
[]
[linear_heat_generation_rate]
type = CompositeFunction
functions = 'linear_heat_rate_profile axial_peaking_factors'
[]
[axial_flux]
type = CompositeFunction
functions = 'flux axial_peaking_factors'
[]
[burnup_thermal_conductivity]
type = ConstantFunction
value = 1 # should be burnup / 950
[]
[radial_power_profile]
type = PiecewiseLinear
data_file = RadialPowerProfile.csv
format = columns
axis = X
[]
[radial_burnup_profile]
type = PiecewiseLinear
data_file = RadialBurnupProfile.csv
format = columns
axis = X
[]
[initial_burnup]
type = CompositeFunction
functions = 'burnup_thermal_conductivity radial_burnup_profile'
[]
[]
[Burnup]
[burnup]
block = 3
rod_ave_lin_pow = linear_heat_rate_profile
axial_power_profile = axial_peaking_factors
rpf_input = radial_power_profile
num_radial = 80
num_axial = 49
fuel_inner_radius = 0.0
fuel_outer_radius = 0.00527
fuel_volume_ratio = 1.0
isotopes = 'U235 U238 Pu239 Pu240 Pu241 Pu242'
isotope_fractions = '0.045 0.955 0.0 0.0 0.0 0.0'
[]
[]
[Physics/SolidMechanics/QuasiStatic]
add_variables = true
[fuel]
block = 3
strain = FINITE
incremental = true
eigenstrain_names = 'fuel_thermal_eigenstrain
fuel_volumetric_swelling_eigenstrain'
extra_vector_tags = 'ref'
generate_output = 'vonmises_stress hydrostatic_stress elastic_strain_xx
elastic_strain_yy elastic_strain_zz stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz'
decomposition_method = EigenSolution
[]
[clad]
block = 1
strain = FINITE
incremental = true
eigenstrain_names = 'clad_thermal_eigenstrain'
extra_vector_tags = 'ref'
generate_output = 'vonmises_stress elastic_strain_xx
elastic_strain_yy elastic_strain_zz stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz creep_strain_xx creep_strain_yy creep_strain_zz'
decomposition_method = EigenSolution
[]
[]
[Kernels]
[gravity]
type = Gravity
variable = disp_y
value = -9.81
block = '1 3'
extra_vector_tags = 'ref'
[]
[heat]
type = HeatConduction
variable = temp
block = '1 3'
extra_vector_tags = 'ref'
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temp
block = '1 3'
extra_vector_tags = 'ref'
[]
[heat_source]
type = NeutronHeatSource
fission_rate = fission_rate
variable = temp
block = 3
extra_vector_tags = 'ref'
[]
[]
[AuxKernels]
[BuTC]
type = FunctionAux
block = 3
variable = BuTC
function = initial_burnup
[]
[pelletid]
type = PelletIdAux
block = 3
variable = pellet_id
number_pellets = 1
execute_on = initial
[]
[gap]
type = SpatialUserObjectAux
block = 3
variable = gap
execute_on = timestep_end
user_object = avg_gap
[]
[buavg]
type = SpatialUserObjectAux
block = 3
variable = buavg
execute_on = timestep_end
user_object = integral_burnup
[]
[fast_neutron_flux]
type = FastNeutronFluxAux
variable = fast_neutron_flux
function = axial_flux
block = 1
execute_on = timestep_begin
[]
[fast_neutron_fluence]
type = FastNeutronFluenceAux
variable = fast_neutron_fluence
block = 1
fast_neutron_flux = fast_neutron_flux
execute_on = timestep_begin
[]
[fuel_porosity]
type = PorosityAuxUO2
block = 3
variable = porosity
execute_on = timestep_begin
[]
[grain_radius]
type = GrainRadiusAux
block = 3
variable = grain_radius
temperature = temp
execute_on = timestep_begin
[]
[SED]
type = MaterialRealAux
variable = SED
property = strain_energy_density
execute_on = timestep_end
block = 1
[]
[]
[Contact]
[mechanical]
model = coulomb
formulation = mortar
primary = 5
secondary = 10
friction_coefficient = 0.4
c_normal = 1e+12
c_tangential = 1e+24
tangential_lm_scaling = 1.0e-16
normal_lm_scaling = 1.0e-10
[]
[]
[ThermalContactMortar]
[thermal_contact]
secondary_variable = temp
primary_boundary = '5'
secondary_boundary = '10'
layer_thickness = layer_thickness_action
roughness_coef = 3.2
roughness_primary = 1.5e-6
roughness_secondary = 1.75e-6
jump_distance_model = LANNING
plenum_pressure = plenum_pressure
initial_moles = initial_moles
initial_gas_types = 'He Ar'
initial_fractions = '0.25 0.75'
gas_released = fission_gas_released
contact_pressure = mechanical_normal_lm
thermal_lm_scaling = 1.0e-2
[]
[]
[BCs]
[no_x_all]
type = DirichletBC
variable = disp_x
boundary = 12
value = 0.0
[]
[no_y_fuel_bottom]
type = DirichletBC
variable = disp_y
boundary = 20
value = 0.0
[]
[no_y_clad_bottom]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[]
[coolant_temp]
type = DirichletBC
boundary = '1 2 3'
variable = temp
value = 293
[]
[Pressure]
[coolantPressure]
boundary = '1 2 3'
factor = 1
function = coolant_pressure_ramp
[]
[]
[PlenumPressure]
[plenumPressure]
boundary = '10 5'
initial_pressure = 0.1e6
startup_time = 0
R = 8.314462
output_initial_moles = initial_moles
temperature = plenum_temperature
volume = plenum_volume
material_input = fission_gas_released
output = plenum_pressure
initial_temperature = 293
[]
[]
[]
[Materials]
[fuel_swelling]
type = UO2VolumetricSwellingEigenstrain
block = 3
burnup = burnup
initial_fuel_density = 10310.8809782
total_densification = 0.006
gas_swelling_model_type = SIFGRS
eigenstrain_name = 'fuel_volumetric_swelling_eigenstrain'
[]
[fuel_thermal]
type = UO2Thermal
thermal_conductivity_model = NFIR
block = 3
temperature = temp
burnup = BuTC
initial_porosity = 0.0592261881186
[]
[fuel_elasticity_tensor]
type = UO2ElasticityTensor
block = 3
[]
[fuel_thermal_expansion]
type = UO2ThermalExpansionMartinEigenstrain
block = 3
stress_free_temperature = 293
eigenstrain_name = 'fuel_thermal_eigenstrain'
[]
[fuel_elastic_stress]
type = ComputeFiniteStrainElasticStress
block = '3'
[]
[clad_thermal]
type = ZryThermal
block = 1
temperature = temp
[]
[clad_inelastic_stress]
type = ComputeMultipleInelasticStress
block = 1
tangent_operator = elastic
inelastic_models ='plasticity'
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = 1
fast_neutron_fluence = fast_neutron_fluence
initial_fast_fluence = 1.30e26
cold_work_factor = 0.01
matpro_youngs_modulus = true
matpro_poissons_ratio = true
[]
## TODO: Creep is not active, but is transfered from the SM version.
## Adding creep causes the Peak Hoop strain to best match the FALCON
## results given by R. Montgomery and D. Sunderland. Only retaining
## plasticity matches the results from Wenfeng Liu, John Alvis, Robert Montgomery, and Ken Yueh
[clad_creep_stress]
type = ZryCreepLimbackHoppeUpdate
block = 1
fast_neutron_flux = fast_neutron_flux
fast_neutron_fluence = fast_neutron_fluence
initial_fast_fluence = 1.30e26
[]
[clad_thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 293.0
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[plasticity]
type = ZryPlasticityUpdate
block = 1
initial_fast_fluence = 1.30e26
fast_neutron_flux = fast_neutron_flux
fast_neutron_fluence = fast_neutron_fluence
cold_work_factor = .01
plasticity_model_type = MATPRO
output_properties = yield_stress
outputs = all
zircaloy_alloy_type = 4
[]
[fission_gas_release]
type = UO2Sifgrs
block = 3
temperature = temp
fission_rate = fission_rate
grain_radius = grain_radius
gbs_model = true
burnup = BuTC
transient_option = MICROCRACKING
[]
[clad_density]
type = Density
block = 1
density = 6551
[]
[fuel_density]
type = Density
block = 3
[]
[strain_energy_density]
type = StrainEnergyDensity
block = '1 3'
incremental = true
[]
[]
[UserObjects]
[avg_gap]
type = LayeredAverage
block = 3
variable = penetration
direction = y
num_layers = 48
[]
[pbz]
type = PelletBrittleZone
block = 3
pellet_id = pellet_id
temperature = temp
pellet_radius = 0.00527
number_pellets = 1
execute_on = timestep_begin
[]
[integral_burnup]
type = LayeredAverage
block = 3
variable = burnup
direction = y
num_layers = 1
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_converged_reason -ksp_converged_reason -snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package -mat_mffd_err -pc_factor_shift_type '
'-pc_factor_shift_amount'
petsc_options_value = 'lu superlu_dist 1e-5 NONZERO 1e-12'
line_search = 'none'
l_max_its = 40
l_tol = 8e-3
nl_max_its = 40
nl_rel_tol = 1e-3
nl_abs_tol = 1e-10
dtmin = 0.00001
dtmax = 1.0
start_time = 0
end_time = 100
[TimeStepper]
type = IterationAdaptiveDT
dt = 0.0001
optimal_iterations = 200
linear_iteration_ratio = 100
timestep_limiting_function = linear_heat_rate_profile
max_function_change = 500000
force_step_every_function_point = true
[]
[]
[Dampers]
[limitT]
type = MaxIncrement
max_increment = 200.0
variable = temp
[]
[limitX]
type = MaxIncrement
max_increment = 1e-4
variable = disp_x
[]
[]
[Postprocessors]
[max_hoop_strain]
type = ElementExtremeValue
variable = strain_zz
block = 1
[]
[max_SED]
type = ElementExtremeValue
variable = SED
block = 1
[]
[average_grain_radius]
type = ElementAverageValue
block = 3
outputs = 'exodus'
variable = grain_radius
[]
[clad_inner_vol]
type = InternalVolume
boundary = 7
outputs = 'exodus'
execute_on = 'timestep_begin initial'
[]
[flux_from_clad]
type = SideDiffusiveFluxIntegral
variable = temp
boundary = 5
diffusivity = thermal_conductivity
outputs = 'exodus'
[]
[flux_from_fuel]
type = SideDiffusiveFluxIntegral
variable = temp
boundary = 10
diffusivity = thermal_conductivity
outputs = 'exodus'
[]
[rod_total_power]
type = ElementIntegralPower
variable = temp
fission_rate = fission_rate
block = 3
[]
[rod_input_power]
type = FunctionValuePostprocessor
function = linear_heat_rate_profile
scale_factor = 0.106
[]
[average_fission_rate]
type = ElementAverageValue
variable = fission_rate
block = '3'
[]
[RAE]
type = RadialAverageEnthalpy
vector_postprocessor = rad_temp
radial_direction = x
axial_direction = y
axial_position = 0.0503
temperature_name = temp
[]
[peak_RAE]
type = TimeExtremeValue
postprocessor = RAE
[]
[]
[VectorPostprocessors]
[rad_temp]
type = NodalValueSampler
block = 3
sort_by = y
variable = temp
execute_on = timestep_end
outputs = dummy
[]
[]
[StandardLWRFuelRodOutputs]
fuel_pellet_blocks = 3
cladding_blocks = 1
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[chkfile]
type = CSV
show = 'average_centerline_fuel_temperature average_fission_rate fission_gas_released_percentage peak_RAE rod_total_power'
execute_on = 'FINAL'
[]
[console]
type = Console
max_rows = 25
output_linear = true
[]
[dummy]
type = CSV
enable = false
[]
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-22/puzry-22_aniso.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-22.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 6000. '
y = '1.e+05 1.e+05 7.5e+06' # Linear increase at 0.0148 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 6000. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
# Circumferential steady-state creep test and analysis of Zircaloy-4 fuel cladding
# Nuclear Engineering and Design, 53, 2312-2322 (2021)
[F]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.738 0.738 0.57'
[]
[G]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.174 0.174 0.45'
[]
[H]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.588 0.588 0.48'
[]
[L]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[M]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[N]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = TaylorExpansion
use_automatic_differentiation = true
[]
[]
[]
[]
[Kernels]
[heat]
type = ADHeatConduction
variable = temperature
[]
[heat_ie]
type = ADHeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = ADMaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = ADMaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = ADMaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = ADMaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = ADMaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = ADFunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = ADDirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = ADDirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ADZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1.e+11
poissons_ratio = 0.3
block = 1
[]
[hill_constants]
type = ADHillConstants
hill_constants = "0.738 0.174 0.588 1.0 1.0 1.0"
function_names = "F G H L M N"
temperature = temperature
[]
[creep_update]
type = ADZryAnisoCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 1.5e-05
temperature = temperature
temperature_standard_thermal_creep_end = 700
temperature_loca_creep_begin = 900.
fract_beta_phase_name = 'fract_beta_phase'
max_integration_error = 1000000.0
absolute_tolerance = 1e-13
relative_tolerance = 1e-11
[]
[creep]
type = ADComputeMultipleInelasticStress
block = 1
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ADZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = ADDensity
block = 1
[]
[phase]
type = ADZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ADZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = NEWTON
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-07
start_time = 0.
n_startup_steps = 1
end_time = 2500.
dtmax = 1.
dtmin = 1.0e-9
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-22_aniso_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-13/puzry-13.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-13.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 5000. '
y = '1.e+05 1.e+05 1.266e+07' # Linear increase at 0.0314 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 5000. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = EigenSolution
[]
[]
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = MaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = FunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = DirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = DirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1.e+11
poissons_ratio = 0.3
block = 1
[]
[creep_update]
type = ZryCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 1.e-04
temperature = temperature
temperature_standard_thermal_creep_end = 700
temperature_loca_creep_begin = 900.
[]
[creep]
type = ComputeMultipleInelasticStress
block = 1
tangent_operator = elastic
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = Density
block = 1
[]
[phase]
type = ZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
active = 'smp'
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0.
n_startup_steps = 1
end_time = 5000.
dtmax = 1.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-13_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/RIA_NSRR_FK/analysis/FK8/FK08.i)
# This file was created using BIF with the following inputs:
# FK06/FK06.var - md5sum: 5a60c05af67ba840a89caacf70b852e2
# pulse.tpl - md5sum: 37e5a6b8a0c63ad020906dada3472585
[GlobalParams]
density = 10310.8809782
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
energy_per_fission = 3.2e-11
a_lower = 0.01822
a_upper = 0.12422
temperature = temp
volumetric_locking_correction = false
[]
[Mesh]
coord_type = RZ
[smeared_pellet_mesh]
type = FuelPinMeshGenerator
clad_mesh_density = customize
pellet_mesh_density = customize
elem_type = QUAD8
ny_p = 100
nx_c = 4
ny_c = 100
nx_p = 12
ny_cu = 3
ny_cl = 3
bx_p = 0.75
clad_bot_gap_height = 0.00152
bottom_clad_height = 0.0167
top_clad_height = 0.0167
clad_thickness = 0.00086
pellet_outer_radius = 0.00527
clad_top_gap_height = 0.05265
pellet_height = 0.106
clad_gap_width = 1e-05
pellet_quantity = 1
[]
patch_size = 5
patch_update_strategy = auto
partitioner = centroid
centroid_partitioner_direction = y
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
converge_on = 'disp_x disp_y temp'
[]
[Variables]
[temp]
initial_condition = 293
block = '1 3'
[]
[]
[AuxVariables]
[BuTC]
[]
[gap]
order = CONSTANT
family = MONOMIAL
[]
[fast_neutron_flux]
block = 1
[]
[fast_neutron_fluence]
block = 1
[]
[buavg]
order = CONSTANT
family = MONOMIAL
[]
[fission_rate]
initial_condition = 0
[]
[grain_radius]
block = 3
initial_condition = 5.96e-6
[]
[integral_burnup]
order = CONSTANT
family = MONOMIAL
[]
[pellet_id]
order = CONSTANT
family = MONOMIAL
block = 3
[]
[porosity]
order = CONSTANT
family = MONOMIAL
initial_condition = 0.0592261881186
[]
[SED]
order = CONSTANT
family = MONOMIAL
[]
[]
[Functions]
[linear_heat_rate_profile]
type = PiecewiseLinear
data_file = pulse.csv
format = columns
[]
[flux]
type = ConstantFunction
value = 0.0
[]
[axial_peaking_factors]
type = ConstantFunction
value = 1
[]
[coolant_pressure_ramp]
type = ConstantFunction
value = 101325
[]
[linear_heat_generation_rate]
type = CompositeFunction
functions = 'linear_heat_rate_profile axial_peaking_factors'
[]
[axial_flux]
type = CompositeFunction
functions = 'flux axial_peaking_factors'
[]
[burnup_thermal_conductivity]
type = ConstantFunction
value = 1 # should be burnup / 950
[]
[radial_power_profile]
type = PiecewiseLinear
data_file = RadialPowerProfile.csv
format = columns
axis = X
[]
[radial_burnup_profile]
type = PiecewiseLinear
data_file = RadialBurnupProfile.csv
format = columns
axis = X
[]
[initial_burnup]
type = CompositeFunction
functions = 'burnup_thermal_conductivity radial_burnup_profile'
[]
[]
[Burnup]
[burnup]
block = 3
rod_ave_lin_pow = linear_heat_rate_profile
axial_power_profile = axial_peaking_factors
rpf_input = radial_power_profile
num_radial = 80
num_axial = 49
fuel_inner_radius = 0.0
fuel_outer_radius = 0.00527
fuel_volume_ratio = 1.0
isotopes = 'U235 U238 Pu239 Pu240 Pu241 Pu242'
isotope_fractions = '0.045 0.955 0.0 0.0 0.0 0.0'
[]
[]
[Physics/SolidMechanics/QuasiStatic]
add_variables = true
[fuel]
block = 3
strain = FINITE
incremental = true
eigenstrain_names = 'fuel_thermal_eigenstrain
fuel_volumetric_swelling_eigenstrain'
extra_vector_tags = 'ref'
generate_output = 'vonmises_stress hydrostatic_stress elastic_strain_xx
elastic_strain_yy '
'elastic_strain_zz stress_xx stress_yy stress_zz strain_xx
strain_yy '
'strain_zz'
decomposition_method = EigenSolution
[]
[clad]
block = 1
strain = FINITE
incremental = true
eigenstrain_names = 'clad_thermal_eigenstrain'
extra_vector_tags = 'ref'
generate_output = 'vonmises_stress elastic_strain_xx
elastic_strain_yy elastic_strain_zz '
'stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz '
'creep_strain_xx creep_strain_yy creep_strain_zz'
decomposition_method = EigenSolution
[]
[]
[Kernels]
[gravity]
type = Gravity
variable = disp_y
value = -9.81
block = '1 3'
extra_vector_tags = 'ref'
[]
[heat]
type = HeatConduction
variable = temp
block = '1 3'
extra_vector_tags = 'ref'
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temp
block = '1 3'
extra_vector_tags = 'ref'
[]
[heat_source]
type = NeutronHeatSource
fission_rate = fission_rate
variable = temp
block = 3
extra_vector_tags = 'ref'
[]
[]
[AuxKernels]
[BuTC]
type = FunctionAux
block = 3
variable = BuTC
function = initial_burnup
[]
[pelletid]
type = PelletIdAux
block = 3
variable = pellet_id
number_pellets = 1
execute_on = initial
[]
[gap]
type = SpatialUserObjectAux
block = 3
variable = gap
execute_on = timestep_end
user_object = avg_gap
[]
[buavg]
type = SpatialUserObjectAux
block = 3
variable = buavg
execute_on = timestep_end
user_object = integral_burnup
[]
[fast_neutron_flux]
type = FastNeutronFluxAux
variable = fast_neutron_flux
function = axial_flux
block = 1
execute_on = timestep_begin
[]
[fast_neutron_fluence]
type = FastNeutronFluenceAux
variable = fast_neutron_fluence
block = 1
fast_neutron_flux = fast_neutron_flux
execute_on = timestep_begin
[]
[fuel_porosity]
type = PorosityAuxUO2
block = 3
variable = porosity
execute_on = timestep_begin
[]
[grain_radius]
type = GrainRadiusAux
block = 3
variable = grain_radius
temperature = temp
execute_on = timestep_begin
[]
[SED]
type = MaterialRealAux
variable = SED
property = strain_energy_density
execute_on = timestep_end
block = 1
[]
[]
[Contact]
[mechanical]
model = coulomb
formulation = mortar
primary = 5
secondary = 10
friction_coefficient = 0.4
c_normal = 1e+12
c_tangential = 1e+24
tangential_lm_scaling = 1.0e-16
normal_lm_scaling = 1.0e-10
[]
[]
[ThermalContactMortar]
[thermal_contact]
secondary_variable = temp
primary_boundary = '5'
secondary_boundary = '10'
layer_thickness = layer_thickness_action
roughness_coef = 3.2
roughness_primary = 1.5e-6
roughness_secondary = 1.75e-6
jump_distance_model = LANNING
plenum_pressure = plenum_pressure
initial_moles = initial_moles
initial_gas_types = 'He Ar'
initial_fractions = '0.25 0.75'
gas_released = fission_gas_released
contact_pressure = mechanical_normal_lm
thermal_lm_scaling = 1.0e-2
[]
[]
[BCs]
[no_x_all]
type = DirichletBC
variable = disp_x
boundary = 12
value = 0.0
[]
[no_y_fuel_bottom]
type = DirichletBC
variable = disp_y
boundary = 20
value = 0.0
[]
[no_y_clad_bottom]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[]
[coolant_temp]
type = DirichletBC
boundary = '1 2 3'
variable = temp
value = 293
[]
[Pressure]
[coolantPressure]
boundary = '1 2 3'
factor = 1
function = coolant_pressure_ramp
[]
[]
[PlenumPressure]
[plenumPressure]
boundary = '10 5'
initial_pressure = 0.1e6
startup_time = 0
R = 8.314462
output_initial_moles = initial_moles
temperature = plenum_temperature
volume = plenum_volume
material_input = fission_gas_released
output = plenum_pressure
initial_temperature = 293
[]
[]
[]
[Materials]
[fuel_swelling]
type = UO2VolumetricSwellingEigenstrain
block = 3
burnup = burnup
initial_fuel_density = 10310.8809782
total_densification = 0.006
gas_swelling_model_type = SIFGRS
eigenstrain_name = 'fuel_volumetric_swelling_eigenstrain'
[]
[fuel_thermal]
type = UO2Thermal
thermal_conductivity_model = NFIR
block = 3
temperature = temp
burnup = BuTC
initial_porosity = 0.0592261881186
[]
[fuel_elasticity_tensor]
type = UO2ElasticityTensor
block = 3
[]
[fuel_thermal_expansion]
type = UO2ThermalExpansionMartinEigenstrain
block = 3
stress_free_temperature = 293
eigenstrain_name = 'fuel_thermal_eigenstrain'
[]
[fuel_elastic_stress]
type = ComputeFiniteStrainElasticStress
block = '3'
[]
[clad_thermal]
type = ZryThermal
block = 1
temperature = temp
[]
[clad_inelastic_stress]
type = ComputeMultipleInelasticStress
block = 1
tangent_operator = elastic
inelastic_models = 'plasticity'
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = 1
fast_neutron_fluence = fast_neutron_fluence
initial_fast_fluence = 1.30e26
cold_work_factor = 0.01
matpro_youngs_modulus = true
matpro_poissons_ratio = true
[]
## TODO: Creep is not active, but is transfered from the SM version.
## Adding creep causes the Peak Hoop strain to best match the FALCON
## results given by R. Montgomery and D. Sunderland. Only retaining
## plasticity matches the results from Wenfeng Liu, John Alvis, Robert Montgomery, and Ken Yueh
[clad_creep_stress]
type = ZryCreepLimbackHoppeUpdate
block = 1
fast_neutron_flux = fast_neutron_flux
fast_neutron_fluence = fast_neutron_fluence
initial_fast_fluence = 1.30e26
[]
[clad_thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 293.0
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[plasticity]
type = ZryPlasticityUpdate
block = 1
initial_fast_fluence = 1.30e26
fast_neutron_flux = fast_neutron_flux
fast_neutron_fluence = fast_neutron_fluence
cold_work_factor = .01
plasticity_model_type = MATPRO
output_properties = yield_stress
outputs = all
zircaloy_alloy_type = 4
[]
[fission_gas_release]
type = UO2Sifgrs
block = 3
temperature = temp
fission_rate = fission_rate
grain_radius = grain_radius
gbs_model = true
burnup = BuTC
transient_option = MICROCRACKING
[]
[clad_density]
type = Density
block = 1
density = 6551
[]
[fuel_density]
type = Density
block = 3
[]
[strain_energy_density]
type = StrainEnergyDensity
block = '1 3'
incremental = true
[]
[]
[UserObjects]
[avg_gap]
type = LayeredAverage
block = 3
variable = penetration
direction = y
num_layers = 48
[]
[pbz]
type = PelletBrittleZone
block = 3
pellet_id = pellet_id
temperature = temp
pellet_radius = 0.00527
number_pellets = 1
execute_on = timestep_begin
[]
[integral_burnup]
type = LayeredAverage
block = 3
variable = burnup
direction = y
num_layers = 1
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_converged_reason -ksp_converged_reason -snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package -mat_mffd_err -pc_factor_shift_type '
'-pc_factor_shift_amount'
petsc_options_value = 'lu superlu_dist 1e-5 NONZERO 1e-12'
line_search = 'none'
l_max_its = 40
l_tol = 8e-3
nl_max_its = 40
nl_rel_tol = 1e-3
nl_abs_tol = 1e-10
dtmin = 0.00001
dtmax = 1.0
start_time = 0
end_time = 100
[TimeStepper]
type = IterationAdaptiveDT
dt = 0.0001
optimal_iterations = 200
linear_iteration_ratio = 100
timestep_limiting_function = linear_heat_rate_profile
max_function_change = 500000
force_step_every_function_point = true
[]
[]
[Dampers]
[limitT]
type = MaxIncrement
max_increment = 100.0
variable = temp
[]
[limitX]
type = MaxIncrement
max_increment = 1e-4
variable = disp_x
[]
[]
[Postprocessors]
[max_hoop_strain]
type = ElementExtremeValue
variable = strain_zz
block = 1
[]
[max_SED]
type = ElementExtremeValue
variable = SED
block = 1
[]
[average_grain_radius]
type = ElementAverageValue
block = 3
outputs = 'exodus'
variable = grain_radius
[]
[clad_inner_vol]
type = InternalVolume
boundary = 7
outputs = 'exodus'
execute_on = 'timestep_begin initial'
[]
[flux_from_clad]
type = SideDiffusiveFluxIntegral
variable = temp
boundary = 5
diffusivity = thermal_conductivity
outputs = 'exodus'
[]
[flux_from_fuel]
type = SideDiffusiveFluxIntegral
variable = temp
boundary = 10
diffusivity = thermal_conductivity
outputs = 'exodus'
[]
[rod_total_power]
type = ElementIntegralPower
variable = temp
fission_rate = fission_rate
block = 3
[]
[rod_input_power]
type = FunctionValuePostprocessor
function = linear_heat_rate_profile
scale_factor = 0.106
[]
[average_fission_rate]
type = ElementAverageValue
variable = fission_rate
block = '3'
[]
[RAE]
type = RadialAverageEnthalpy
vector_postprocessor = rad_temp
radial_direction = x
axial_direction = y
axial_position = 0.0503
temperature_name = temp
[]
[peak_RAE]
type = TimeExtremeValue
postprocessor = RAE
[]
[]
[VectorPostprocessors]
[rad_temp]
type = NodalValueSampler
block = 3
sort_by = y
variable = temp
execute_on = timestep_end
outputs = dummy
[]
[]
[StandardLWRFuelRodOutputs]
fuel_pellet_blocks = 3
cladding_blocks = 1
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[chkfile]
type = CSV
show = 'average_centerline_fuel_temperature average_fission_rate fission_gas_released_percentage '
'peak_RAE rod_total_power'
execute_on = 'FINAL'
[]
[console]
type = Console
max_rows = 25
output_linear = true
[]
[dummy]
type = CSV
enable = false
[]
[]
(assessment/LWR/validation/LOCA_REBEKA_cladding_burst_tests/analysis/rebeka_2d_08MPa/rebeka_singlerod_2d_08MPa.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.0
order = SECOND
family = LAGRANGE
displacements = 'disp_x disp_y'
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = rebeka_singlerod.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 573.0
[]
[]
[Functions]
[temperature_func]
type = PiecewiseLinear
x = '0. 700. '
y = '573. 1273.' # From 300 to 1000 C at 1 K/s
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 700. '
y = '8.e+06 8.e+06' # 80 bar
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 700. '
y = '1.e+05 1.e+05' # atmospheric pressure
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[clad]
block = cladding
add_variables = false
strain = FINITE
decomposition_method = EigenSolution
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
eigenstrain_names = 'clad_thermal_eigenstrain'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz hoop_stress'
[]
[]
[AuxVariables]
[creep_rate_aux]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[scale_thickness]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfract_total]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfgain_total]
order = CONSTANT
family = MONOMIAL
[]
[burst_stress]
order = CONSTANT
family = MONOMIAL
[]
[burst]
order = CONSTANT
family = MONOMIAL
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate_aux]
type = MaterialRealAux
variable = creep_rate_aux
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[scl_thickness]
type = MaterialRealAux
variable = scale_thickness
property = oxide_scale_thickness
boundary = 2
[]
[ofract_total]
type = MaterialRealAux
variable = oxywtfract_total
property = current_oxygen_weight_frac_total
boundary = 2
[]
[ofgain_total]
type = MaterialRealAux
boundary = 2
variable = oxywtfgain_total
property = oxygen_weight_frac_gained_total
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = 2
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = 2
execute_on = timestep_end
[]
[]
[BCs]
[inner_temperature]
type = REBEKADirichletBC
variable = temperature
function_tempm = temperature_func
minimum_temperature = 573.
translation = 0.1625
boundary = 4
[]
[no_y_midsection]
type = DirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply steam pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 101 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[CoolantChannel]
[convective_clad_surface]
boundary = 2
variable = temperature
inlet_temperature = 473.
inlet_pressure = 1.e+05
inlet_massflux = 1.0 # kg/m^2-sec # almost stagnant steam
rod_diameter = 10.75e-03
rod_pitch = 1.26e-02 # default
number_axial_zone = 15
oxide_thickness = scale_thickness
[]
[]
[Materials]
[thermal]
type = ZryThermal
block = cladding
temperature = temperature
[]
[clad_elasticity_tensor]
type = ComputeIsotropicElasticityTensor
block = cladding
youngs_modulus = 1.0e11
poissons_ratio = 0.3
[]
[clad_stress]
type = ComputeMultipleInelasticStress
tangent_operator = elastic
inelastic_models = 'clad_zrycreep'
block = cladding
[]
[clad_zrycreep]
type = ZryCreepLOCAUpdate
block = cladding
temperature = temperature
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
temperature_loca_creep_begin = 501 # see Erbacher et al., 1982
temperature_standard_thermal_creep_end = 500
[]
[thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = cladding
temperature = temperature
stress_free_temperature = 573.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[density]
type = Density
block = cladding
[]
[phase]
type = ZrPhase
block = cladding
temperature = temperature
numerical_method = 2
[]
[oxidation]
type = ZryOxidation
boundary = 2
temperature = temperature
clad_inner_radius = 0.00465
clad_outer_radius = 0.005375
normal_operating_temperature_model = epri_kwu_ce
high_temperature_model = leistikow
use_coolant_channel = true
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = 2
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate_aux
temperature = temperature
fraction_beta_phase = fract_beta_phase
fraction_oxygen_gain = oxywtfgain_total
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0
n_startup_steps = 1
end_time = 700.
dtmax = 1.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average temperature of cladding exterior
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = cladding
[]
[max_clad_temp]
type = NodalExtremeValue
block = cladding
value_type = max
variable = temperature
[]
[max_oxygen_fract]
type = ElementExtremeValue
block = cladding
value_type = max
variable = oxywtfract_total
[]
[max_betaph_fract]
type = ElementExtremeValue
block = cladding
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
block = cladding
value_type = max
variable = creep_rate_aux
[]
[max_creep_strain_mag]
type = ElementExtremeValue
block = cladding
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
block = cladding
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
block = cladding
value_type = max
variable = hoop_stress
[]
[vonmises_stress_clad]
type = ElementAverageValue
block = cladding
variable = vonmises_stress
[]
[min_burst_stress]
type = ElementExtremeValue
block = cladding
value_type = min
variable = burst_stress
[]
[burst]
type = ElementExtremeValue
block = cladding
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = cladding
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = cladding
plenum_boundary_name = 4
external_clad_boundary_name = 2
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = rebeka_2d_08MPa_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-17/puzry-17.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-17.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 1500. '
y = '1.e+05 1.e+05 5.91e+06' # Linear increase at 0.1162 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 1500. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = EigenSolution
[]
[]
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = MaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = FunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = DirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = DirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1.0e+11
poissons_ratio = 0.3
block = 1
[]
[creep_update]
type = ZryCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 1.e-04
temperature = temperature
temperature_standard_thermal_creep_end = 700
temperature_loca_creep_begin = 900.
[]
[creep]
type = ComputeMultipleInelasticStress
block = 1
tangent_operator = elastic
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.0
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = Density
block = 1
[]
[phase]
type = ZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
active = 'smp'
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0.
n_startup_steps = 1
end_time = 1500.
dtmax = 1.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-17_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/LOCA_ANL_cladding_burst_tests/analysis/OCL5_8/OCL5_8.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
displacements = 'disp_x disp_y'
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
[]
[Mesh]
coord_type = RZ
[smeared_pellet_mesh]
type = FuelPinMeshGenerator
pellet_quantity = 1
pellet_height = 0.270
pellet_outer_radius = 4.78e-3
clad_bot_gap_height = 0.001
clad_top_gap_height = 0.013
clad_thickness = 0.71e-3
clad_gap_width = 0.1e-3
pellet_mesh_density = coarse
clad_mesh_density = coarse
elem_type = QUAD8
[]
patch_size = 10
patch_update_strategy = auto
partitioner = centroid
centroid_partitioner_direction = y
[]
[Variables]
[temperature]
initial_condition = 300.0
[]
[]
[Functions]
[temperature_func]
type = PiecewiseLinear
x = '0 496.02 520.74 528.12 545.94 551.28 671.52 885.3 1195.74 1410.36 1657.86 1680 1690 1700 1710 1720 1730 1740 1750 1760 1770 1780 1790 1800 1810 1820 1830 1840 1848'
y = '300 300 405.465 482.048 583.351 632.287 634.297 632.825 630.378 631.059 632.59 633 683 733 783 833 883 933 983 1033 1083 1133 1183 1233 1283 1333 1383 1433 1477'
[]
[temperature_profile]
type = PiecewiseBilinear
data_file = 'temp_profile.csv'
axis = 1
[]
[cladding_temperature]
type = CompositeFunction
functions = 'temperature_func temperature_profile'
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[pellets]
block = pellet
add_variables = true
strain = FINITE
eigenstrain_names = 'fuel_thermal_strain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
generate_output = 'vonmises_stress hydrostatic_stress stress_xx stress_yy
stress_zz strain_xx strain_yy strain_zz hoop_stress'
extra_vector_tags = 'ref'
[]
[clad]
block = clad
add_variables = true
strain = FINITE
decomposition_method = EigenSolution
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz hoop_stress'
extra_vector_tags = 'ref'
[]
[]
[AuxVariables]
[creep_rate_aux]
order = CONSTANT
family = MONOMIAL
block = clad
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
block = clad
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
block = clad
[]
[burst_stress]
order = CONSTANT
family = MONOMIAL
block = clad
[]
[burst]
order = CONSTANT
family = MONOMIAL
block = clad
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
extra_vector_tags = 'ref'
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
extra_vector_tags = 'ref'
[]
[]
[AuxKernels]
[creep_rate_aux]
type = MaterialRealAux
variable = creep_rate_aux
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
block = clad
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = clad_outside_right
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = clad_outside_right
execute_on = timestep_end
[]
[]
[ThermalContact]
[thermal_contact]
type = GapHeatTransfer
primary = 5
secondary = 10
variable = temperature
gap_conductivity = 0.15 # k of He per Netzsch
[]
[]
[BCs]
[clad_surface_temperature]
type = FunctionDirichletBC
variable = temperature
boundary = '2'
function = cladding_temperature
[]
[no_x_all]
type = DirichletBC
variable = disp_x
boundary = 12
value = 0.0
[]
[no_y_clad_bottom]
type = DirichletBC
variable = disp_y
boundary = '1'
value = 0.0
[]
[no_y_fuel_bottom]
type = DirichletBC
variable = disp_y
boundary = '1020'
value = 0.0
[]
[Pressure]
[outer_pressure]
boundary = '1 2 3'
factor = 101325
[]
[inner_pressure]
boundary = '4 5 6'
factor = 8.28e6
[]
[]
[]
[PlenumTemperature]
[plenum_temp]
boundary = 5
inner_surfaces = '5'
outer_surfaces = '10'
temperature = temperature
[]
[]
[Materials]
[fuel_thermal]
type = HeatConductionMaterial
block = pellet
thermal_conductivity = 3.5
specific_heat = 330.0
[]
[fuel_elasticity_tensor]
type = ComputeIsotropicElasticityTensor
block = pellet
youngs_modulus = 2.0e11
poissons_ratio = 0.345
[]
[fuel_elastic_stress]
type = ComputeFiniteStrainElasticStress
block = pellet
[]
[fuel_thermal_expansion]
type = ComputeThermalExpansionEigenstrain
block = pellet
thermal_expansion_coeff = 10.0e-6
temperature = temperature
stress_free_temperature = 300.0
eigenstrain_name = fuel_thermal_strain
[]
[fuel_density]
type = Density
block = pellet
density = 10980.0 #perfectly dense UO2
[]
[clad_thermal]
type = ZryThermal
block = clad
temperature = temperature
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = clad
matpro_youngs_modulus = false
matpro_poissons_ratio = false
[]
[clad_stress]
type = ComputeMultipleInelasticStress
inelastic_models = 'clad_zrycreep'
block = clad
tangent_operator = nonlinear
[]
[clad_zrycreep]
type = ZryCreepLOCAUpdate
block = clad
temperature = temperature
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
temperature_loca_creep_begin = 501
temperature_standard_thermal_creep_end = 500
[]
[thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = clad
temperature = temperature
stress_free_temperature = 300.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[clad_density]
type = Density
block = clad
density = 6550.0
[]
[phase]
type = ZrPhase
block = clad
temperature = temperature
numerical_method = 2
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = clad_outside_right
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate_aux
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
verbose = true
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.0e-04
nl_abs_tol = 1.0e-08
start_time = 0
n_startup_steps = 1
end_time = 1800.0
dtmax = 100
dtmin = 0.0001
[TimeStepper]
type = IterationAdaptiveDT
timestep_limiting_postprocessor = material_timestep
dt = 10.0
time_dt = '100 10'
time_t = '10 400'
[]
[]
[Postprocessors]
[ave_clad_temp]
type = SideAverageValue
boundary = clad_outside_right
variable = temperature
[]
[gas_volume]
type = InternalVolume
boundary = 9
execute_on = 'initial linear'
[]
[max_clad_temp]
type = NodalExtremeValue
block = clad
value_type = max
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = clad
[]
[max_hoop_stress]
type = ElementExtremeValue
block = clad
value_type = max
variable = hoop_stress
[]
[vonmises_stress_clad]
type = ElementAverageValue
block = clad
variable = vonmises_stress
[]
[min_burst_stress]
type = ElementExtremeValue
block = clad
value_type = min
variable = burst_stress
[]
[burst]
type = ElementExtremeValue
block = clad
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = clad
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
[]
[PerformanceMetricOutputs]
[]
[Outputs]
exodus = true
csv = true
color = false
perf_graph = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
show = 'max_clad_temp max_hoop_stress vonmises_stress_clad'
execute_on = 'FINAL'
[]
[]
[UserObjects]
[terminator1]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
[]
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-10/puzry-10_aniso.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-10.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 1200. '
y = '1.e+05 1.e+05 1.52e+06' # Linear increase at 0.0710 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 1200. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
# Circumferential steady-state creep test and analysis of Zircaloy-4 fuel cladding
# Nuclear Engineering and Design, 53, 2312-2322 (2021)
[F]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.738 0.738 0.57'
[]
[G]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.174 0.174 0.45'
[]
[H]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.588 0.588 0.48'
[]
[L]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[M]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[N]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = TaylorExpansion
use_automatic_differentiation = true
[]
[]
[]
[]
[Kernels]
[heat]
type = ADHeatConduction
variable = temperature
[]
[heat_ie]
type = ADHeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = ADMaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = ADMaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = ADMaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = ADMaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = ADMaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = ADFunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = ADDirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = ADDirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ADZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1.e+11
poissons_ratio = 0.3
block = 1
[]
[hill_constants]
type = ADHillConstants
hill_constants = "0.738 0.174 0.588 1.0 1.0 1.0"
function_names = "F G H L M N"
temperature = temperature
[]
[creep_update]
type = ADZryAnisoCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 1.5e-05
temperature = temperature
temperature_standard_thermal_creep_end = 700
temperature_loca_creep_begin = 900.
fract_beta_phase_name = 'fract_beta_phase'
max_integration_error = 1000000.0
absolute_tolerance = 1e-13
relative_tolerance = 1e-11
[]
[creep]
type = ADComputeMultipleInelasticStress
block = 1
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ADZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = ADDensity
block = 1
[]
[phase]
type = ADZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ADZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = NEWTON
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0.
n_startup_steps = 1
end_time = 2500.
dtmax = 1.
dtmin = 1.0e-9
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-10_aniso_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-14/puzry-14_aniso.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-14.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 2500. '
y = '1.e+05 1.e+05 1.795e+07' # Linear increase at 0.1190 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 2500. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
# Circumferential steady-state creep test and analysis of Zircaloy-4 fuel cladding
# Nuclear Engineering and Design, 53, 2312-2322 (2021)
[F]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.738 0.738 0.57'
[]
[G]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.174 0.174 0.45'
[]
[H]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.588 0.588 0.48'
[]
[L]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[M]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[N]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = TaylorExpansion
use_automatic_differentiation = true
[]
[]
[]
[]
[Kernels]
[heat]
type = ADHeatConduction
variable = temperature
[]
[heat_ie]
type = ADHeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = ADMaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = ADMaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = ADMaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = ADMaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = ADMaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = ADFunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = ADDirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = ADDirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ADZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1.e+11
poissons_ratio = 0.3
block = 1
[]
[hill_constants]
type = ADHillConstants
hill_constants = "0.738 0.174 0.588 1.0 1.0 1.0"
function_names = "F G H L M N"
temperature = temperature
[]
[creep_update]
type = ADZryAnisoCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 1.5e-05
temperature = temperature
temperature_standard_thermal_creep_end = 700
temperature_loca_creep_begin = 900.
fract_beta_phase_name = 'fract_beta_phase'
max_integration_error = 1000000.0
absolute_tolerance = 1e-13
relative_tolerance = 1e-11
[]
[creep]
type = ADComputeMultipleInelasticStress
block = 1
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ADZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = ADDensity
block = 1
[]
[phase]
type = ADZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ADZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-07
start_time = 0.
n_startup_steps = 1
end_time = 2500.
dtmax = 1.
dtmin = 1.0e-9
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-14_aniso_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/LOCA_ORNL_cladding_burst_tests/analysis/Zr2_2/ornl_zr2_2_ad.i)
# Simulation ORNL burst tests Zr2_2
[GlobalParams]
density = 6550.
order = SECOND
family = LAGRANGE
displacements = 'disp_x disp_y'
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = zr2_ornl_burst_test_mesh.e
[]
[]
[Variables]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func] # only 10 inches of the rod are within the heated zone (cf. Terrani email)
type = PiecewiseBilinear
data_file = temperature_ornl_zr2_2.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
data_file = pressure_inner_ornl_zr2_2.csv
scale_factor = 1.e+06
format = columns
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 700. '
y = '0.1 0.1 ' # atmospheric pressure
scale_factor = 1.e+06
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[clad]
use_automatic_differentiation = true
block = cladding
add_variables = true
strain = FINITE
decomposition_method = TaylorExpansion
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
eigenstrain_names = 'clad_thermal_eigenstrain'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz hoop_stress'
[]
[]
[AuxVariables]
[creep_rate_aux]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[scale_thickness]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfract_total]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfgain_total]
order = CONSTANT
family = MONOMIAL
[]
[burst_stress]
order = CONSTANT
family = MONOMIAL
[]
[burst]
order = CONSTANT
family = MONOMIAL
[]
[]
[Kernels]
[heat]
type = ADHeatConduction
variable = temperature
[]
[heat_ie]
type = ADHeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate_aux]
type = ADMaterialRealAux
variable = creep_rate_aux
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = ADMaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[scl_thickness]
type = ADMaterialRealAux
variable = scale_thickness
property = oxide_scale_thickness
boundary = 2
[]
[ofract_total]
type = ADMaterialRealAux
variable = oxywtfract_total
property = current_oxygen_weight_frac_total
boundary = 2
[]
[ofgain_total]
type = ADMaterialRealAux
boundary = 2
variable = oxywtfgain_total
property = oxygen_weight_frac_gained_total
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = 2
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = 2
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = ADFunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 4'
preset = false
[]
[no_y_top]
type = ADDirichletBC
variable = disp_y
boundary = 3
value = 0.
preset = false
[]
[Pressure]
[outer_pressure] # apply steam pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[mid_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 2 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
type = ADZryThermal
block = cladding
temperature = temperature
[]
[clad_elasticity_tensor]
type = ADZryElasticityTensor
block = cladding
matpro_youngs_modulus = false
matpro_poissons_ratio = false
[]
[clad_stress]
type = ADComputeMultipleInelasticStress
inelastic_models = 'clad_zrycreep'
block = cladding
[]
[hill_constants]
type = ADHillConstants
hill_constants = "0.5 0.5 0.5 1.0 1.0 1.0"
#hill_constants = "0.738 0.174 0.588 1.0 1.0 1.0"
#function_names = "F G H L M N"
[]
[clad_zrycreep]
type = ADZryAnisoCreepLOCAUpdate
block = cladding
temperature = temperature
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
temperature_loca_creep_begin = 301
temperature_standard_thermal_creep_end = 300
fract_beta_phase_name = 'ad_fract_beta_phase'
[]
[thermal_expansion]
type = ADZryThermalExpansionMATPROEigenstrain
block = cladding
temperature = temperature
stress_free_temperature = 300.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[density]
type = ADDensity
block = cladding
[]
[phase]
type = ZrPhase
block = cladding
temperature = temperature
numerical_method = 2
[]
[phase_converter]
type = MaterialADConverter
reg_props_in = 'fract_beta_phase'
ad_props_out = 'ad_fract_beta_phase'
[]
[oxidation]
type = ADZryOxidation
boundary = 2
temperature = temperature
clad_inner_radius = 0.004875
clad_outer_radius = 0.005580
normal_operating_temperature_model = epri_kwu_ce
high_temperature_model = leistikow
#use_coolant_channel = true
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = 2
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate_aux
temperature = temperature
fraction_beta_phase = fract_beta_phase
fraction_oxygen_gain = oxywtfgain_total
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = PJFNK
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0
n_startup_steps = 1
end_time = 700.
dtmax = 2.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 2.
[]
[]
[Postprocessors]
[pressure_inner]
type = FunctionValuePostprocessor
function = inner_pressure_func
execute_on = 'initial timestep_end'
[]
[pressure_outer]
type = FunctionValuePostprocessor
function = outer_pressure_func
execute_on = 'initial timestep_end'
[]
[ave_clad_temp]
type = SideAverageValue
boundary = 2
variable = temperature
execute_on = 'initial timestep_end'
[]
[max_clad_temp]
type = NodalExtremeValue
block = cladding
value_type = max
variable = temperature
execute_on = 'initial timestep_end'
[]
[min_clad_temp]
type = NodalExtremeValue
block = cladding
value_type = min
variable = temperature
execute_on = 'initial timestep_end'
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = cladding
[]
[max_oxygen_fract]
type = ElementExtremeValue
block = cladding
value_type = max
variable = oxywtfract_total
execute_on = 'initial timestep_end'
[]
[max_betaph_fract]
type = ElementExtremeValue
block = cladding
value_type = max
variable = fract_beta_phase
execute_on = 'initial timestep_end'
[]
[max_creep_rate]
type = ElementExtremeValue
block = cladding
value_type = max
variable = creep_rate_aux
execute_on = 'initial timestep_end'
[]
[max_creep_strain_mag]
type = ElementExtremeValue
block = cladding
value_type = max
variable = creep_strain_mag
execute_on = 'initial timestep_end'
[]
[max_hoop_strain]
type = ElementExtremeValue
block = cladding
value_type = max
variable = strain_zz
execute_on = 'initial timestep_end'
[]
[max_hoop_stress]
type = ElementExtremeValue
block = cladding
value_type = max
variable = hoop_stress
[]
[vonmises_stress_clad]
type = ElementAverageValue
block = cladding
variable = vonmises_stress
execute_on = 'initial timestep_end'
[]
[min_burst_stress]
type = ElementExtremeValue
block = cladding
value_type = min
variable = burst_stress
execute_on = 'initial timestep_end'
[]
[burst]
type = ElementExtremeValue
block = cladding
value_type = max
variable = burst
execute_on = 'initial timestep_end'
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = cladding
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[mid_disp_r_clad]
type = NodalVariableValue
variable = disp_x
nodeid = 22
[]
[stress_xx_midplane] # stress in the mid Element
type = ElementalVariableValue
variable = stress_xx
elementid = 19
[]
[stress_yy_midplane] # stress in the mid Element
type = ElementalVariableValue
variable = stress_yy
elementid = 19
[]
[stress_zz_midplane] # stress in the mid Element
type = ElementalVariableValue
variable = stress_zz
elementid = 19
[]
[strain_zz_midplane] # strain in the mid Element
type = ElementalVariableValue
variable = strain_zz
elementid = 19
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
plenum_boundary_name = 4
cladding_blocks = cladding
[]
[PerformanceMetricOutputs]
[]
[Outputs]
exodus = true
perf_graph = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 20
[]
[chkfile]
type = CSV
file_base = ornl_zr2_2_ad_chkfile
show = 'pressure_inner max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/LOCA_REBEKA_cladding_burst_tests/analysis/rebeka_2d_14MPa/rebeka_singlerod_2d_14MPa.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.0
order = SECOND
family = LAGRANGE
displacements = 'disp_x disp_y'
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = rebeka_singlerod.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 573.0
[]
[]
[Functions]
[temperature_func]
type = PiecewiseLinear
x = '0. 700. '
y = '573. 1273.' # From 300 to 1000 C at 1 K/s
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 700. '
y = '1.4e+07 1.4e+07' # 140 bar
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 700. '
y = '1.e+05 1.e+05' # atmospheric pressure
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[clad]
block = cladding
add_variables = false
strain = FINITE
decomposition_method = EigenSolution
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz hoop_stress'
[]
[]
[AuxVariables]
[creep_rate_aux]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[scale_thickness]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfract_total]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfgain_total]
order = CONSTANT
family = MONOMIAL
[]
[burst_stress]
order = CONSTANT
family = MONOMIAL
[]
[burst]
order = CONSTANT
family = MONOMIAL
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate_aux]
type = MaterialRealAux
variable = creep_rate_aux
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[scl_thickness]
type = MaterialRealAux
variable = scale_thickness
property = oxide_scale_thickness
boundary = 2
[]
[ofract_total]
type = MaterialRealAux
variable = oxywtfract_total
property = current_oxygen_weight_frac_total
boundary = 2
[]
[ofgain_total]
type = MaterialRealAux
boundary = 2
variable = oxywtfgain_total
property = oxygen_weight_frac_gained_total
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = 2
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = 2
execute_on = timestep_end
[]
[]
[BCs]
[inner_temperature]
type = REBEKADirichletBC
variable = temperature
function_tempm = temperature_func
minimum_temperature = 573.0
translation = 0.1625
boundary = 4
[]
[no_y_midsection]
type = DirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply steam pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 101 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[CoolantChannel]
[convective_clad_surface]
boundary = 2
variable = temperature
inlet_temperature = 473.
inlet_pressure = 1.e+05
inlet_massflux = 1.0 # kg/m^2-sec # almost stagnant steam
rod_diameter = 10.75e-03
rod_pitch = 1.26e-02 # default
number_axial_zone = 15
oxide_thickness = scale_thickness
[]
[]
[Materials]
[thermal]
type = ZryThermal
block = cladding
temperature = temperature
[]
[clad_elasticity_tensor]
type = ComputeIsotropicElasticityTensor
block = cladding
youngs_modulus = 1.0e11
poissons_ratio = 0.3
[]
[clad_stress]
type = ComputeMultipleInelasticStress
tangent_operator = elastic
inelastic_models = 'clad_zrycreep'
block = cladding
[]
[clad_zrycreep]
type = ZryCreepLOCAUpdate
block = cladding
temperature = temperature
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
temperature_loca_creep_begin = 501 # see Erbacher et al., 1982
temperature_standard_thermal_creep_end = 500
[]
[thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = cladding
temperature = temperature
stress_free_temperature = 573.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[density]
type = Density
block = cladding
[]
[phase]
type = ZrPhase
block = cladding
temperature = temperature
numerical_method = 2
[]
[oxidation]
type = ZryOxidation
boundary = 2
temperature = temperature
clad_inner_radius = 0.00465
clad_outer_radius = 0.005375
normal_operating_temperature_model = epri_kwu_ce
high_temperature_model = leistikow
use_coolant_channel = true
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = 2
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate_aux
temperature = temperature
fraction_beta_phase = fract_beta_phase
fraction_oxygen_gain = oxywtfgain_total
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0
n_startup_steps = 1
end_time = 700.
dtmax = 1.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average temperature of cladding exterior
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = cladding
[]
[max_clad_temp]
type = NodalExtremeValue
block = cladding
value_type = max
variable = temperature
[]
[max_oxygen_fract]
type = ElementExtremeValue
block = cladding
value_type = max
variable = oxywtfract_total
[]
[max_betaph_fract]
type = ElementExtremeValue
block = cladding
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
block = cladding
value_type = max
variable = creep_rate_aux
[]
[max_creep_strain_mag]
type = ElementExtremeValue
block = cladding
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
block = cladding
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
block = cladding
value_type = max
variable = hoop_stress
[]
[vonmises_stress_clad]
type = ElementAverageValue
block = cladding
variable = vonmises_stress
[]
[min_burst_stress]
type = ElementExtremeValue
block = cladding
value_type = min
variable = burst_stress
[]
[burst]
type = ElementExtremeValue
block = cladding
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = cladding
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = cladding
plenum_boundary_name = 4
external_clad_boundary_name = 2
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = rebeka_2d_14MPa_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
(assessment/LWR/validation/RIA_NSRR_FK/analysis/FK4/FK04.i)
# This file was created using BIF with the following inputs:
# FK04/FK04.var - md5sum: 789d603cfbdaaeb2625ea98056214f6f
# pulse.tpl - md5sum: 37e5a6b8a0c63ad020906dada3472585
[GlobalParams]
density = 10310.8809782
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
energy_per_fission = 3.2e-11
a_lower = 0.01822
a_upper = 0.12422
temperature = temp
volumetric_locking_correction = false
[]
[Mesh]
coord_type = RZ
[smeared_pellet_mesh]
type = FuelPinMeshGenerator
clad_mesh_density = customize
pellet_mesh_density = customize
elem_type = QUAD8
ny_p = 100
nx_c = 4
ny_c = 100
nx_p = 12
ny_cu = 3
ny_cl = 3
bx_p = 0.75
clad_bot_gap_height = 0.00152
bottom_clad_height = 0.0167
top_clad_height = 0.0167
clad_thickness = 0.00086
pellet_outer_radius = 0.00527
clad_top_gap_height = 0.053182
pellet_height = 0.106
clad_gap_width = 1e-05
pellet_quantity = 1
[]
patch_size = 5
patch_update_strategy = auto
partitioner = centroid
centroid_partitioner_direction = y
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
converge_on = 'disp_x disp_y temp'
[]
[Variables]
[temp]
block = '1 3'
initial_condition = 293
[]
[]
[AuxVariables]
[BuTC]
[]
[gap]
order = CONSTANT
family = MONOMIAL
[]
[fast_neutron_flux]
block = 1
[]
[fast_neutron_fluence]
block = 1
[]
[buavg]
order = CONSTANT
family = MONOMIAL
[]
[fission_rate]
initial_condition = 0
[]
[grain_radius]
block = 3
initial_condition = 5.96e-6
[]
[integral_burnup]
order = CONSTANT
family = MONOMIAL
[]
[pellet_id]
order = CONSTANT
family = MONOMIAL
block = 3
[]
[porosity]
order = CONSTANT
family = MONOMIAL
initial_condition = 0.0592261881186
[]
[SED]
order = CONSTANT
family = MONOMIAL
[]
[]
[Functions]
[linear_heat_rate_profile]
type = PiecewiseLinear
data_file = pulse.csv
format = columns
[]
[flux]
type = ConstantFunction
value = 0.0
[]
[axial_peaking_factors]
type = ConstantFunction
value = 1
[]
[coolant_pressure_ramp]
type = ConstantFunction
value = 101325
[]
[linear_heat_generation_rate]
type = CompositeFunction
functions = 'linear_heat_rate_profile axial_peaking_factors'
[]
[axial_flux]
type = CompositeFunction
functions = 'flux axial_peaking_factors'
[]
[burnup_thermal_conductivity]
type = ConstantFunction
value = 1 # should be burnup / 950
[]
[radial_power_profile]
type = PiecewiseLinear
data_file = RadialPowerProfile.csv
format = columns
axis = X
[]
[radial_burnup_profile]
type = PiecewiseLinear
data_file = RadialBurnupProfile.csv
format = columns
axis = X
[]
[initial_burnup]
type = CompositeFunction
functions = 'burnup_thermal_conductivity radial_burnup_profile'
[]
[]
[Burnup]
[burnup]
block = 3
rod_ave_lin_pow = linear_heat_rate_profile
axial_power_profile = axial_peaking_factors
rpf_input = radial_power_profile
num_radial = 80
num_axial = 49
fuel_inner_radius = 0.0
fuel_outer_radius = 0.00527
fuel_volume_ratio = 1.0
isotopes = 'U235 U238 Pu239 Pu240 Pu241 Pu242'
isotope_fractions = '0.045 0.955 0.0 0.0 0.0 0.0'
[]
[]
[Physics/SolidMechanics/QuasiStatic]
add_variables = true
[fuel]
block = 3
strain = FINITE
incremental = true
eigenstrain_names = 'fuel_thermal_eigenstrain
fuel_volumetric_swelling_eigenstrain'
extra_vector_tags = 'ref'
generate_output = 'vonmises_stress hydrostatic_stress elastic_strain_xx
elastic_strain_yy elastic_strain_zz stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz'
decomposition_method = EigenSolution
[]
[clad]
block = 1
strain = FINITE
incremental = true
eigenstrain_names = 'clad_thermal_eigenstrain'
extra_vector_tags = 'ref'
generate_output = 'vonmises_stress elastic_strain_xx
elastic_strain_yy elastic_strain_zz stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz creep_strain_xx creep_strain_yy creep_strain_zz'
decomposition_method = EigenSolution
[]
[]
[Kernels]
[gravity]
type = Gravity
variable = disp_y
value = -9.81
block = '1 3'
extra_vector_tags = 'ref'
[]
[heat]
type = HeatConduction
variable = temp
block = '1 3'
extra_vector_tags = 'ref'
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temp
block = '1 3'
extra_vector_tags = 'ref'
[]
[heat_source]
type = NeutronHeatSource
fission_rate = fission_rate
variable = temp
block = 3
extra_vector_tags = 'ref'
[]
[]
[AuxKernels]
[BuTC]
type = FunctionAux
block = 3
variable = BuTC
function = initial_burnup
[]
[pelletid]
type = PelletIdAux
block = 3
variable = pellet_id
number_pellets = 1
execute_on = initial
[]
[gap]
type = SpatialUserObjectAux
block = 3
variable = gap
execute_on = timestep_end
user_object = avg_gap
[]
[buavg]
type = SpatialUserObjectAux
block = 3
variable = buavg
execute_on = timestep_end
user_object = integral_burnup
[]
[fast_neutron_flux]
type = FastNeutronFluxAux
variable = fast_neutron_flux
function = axial_flux
block = 1
execute_on = timestep_begin
[]
[fast_neutron_fluence]
type = FastNeutronFluenceAux
variable = fast_neutron_fluence
block = 1
fast_neutron_flux = fast_neutron_flux
execute_on = timestep_begin
[]
[fuel_porosity]
type = PorosityAuxUO2
block = 3
variable = porosity
execute_on = timestep_begin
[]
[grain_radius]
type = GrainRadiusAux
block = 3
variable = grain_radius
temperature = temp
execute_on = timestep_begin
[]
[SED]
type = MaterialRealAux
variable = SED
property = strain_energy_density
execute_on = timestep_end
block = 1
[]
[]
[Contact]
[mechanical]
model = coulomb
formulation = mortar
primary = 5
secondary = 10
friction_coefficient = 0.4
c_normal = 1e+12
c_tangential = 1e+24
tangential_lm_scaling = 1.0e-16
normal_lm_scaling = 1.0e-10
[]
[]
[ThermalContactMortar]
[thermal_contact]
secondary_variable = temp
primary_boundary = '5'
secondary_boundary = '10'
layer_thickness = layer_thickness_action
roughness_coef = 3.2
roughness_primary = 1.5e-6
roughness_secondary = 1.75e-6
jump_distance_model = LANNING
plenum_pressure = plenum_pressure
initial_moles = initial_moles
gas_released = fission_gas_released
contact_pressure = mechanical_normal_lm
thermal_lm_scaling = 1.0e-2
[]
[]
[BCs]
[no_x_all]
type = DirichletBC
variable = disp_x
boundary = 12
value = 0.0
[]
[no_y_fuel_bottom]
type = DirichletBC
variable = disp_y
boundary = 20
value = 0.0
[]
[no_y_clad_bottom]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[]
[coolant_temp]
type = DirichletBC
boundary = '1 2 3'
variable = temp
value = 293
[]
[Pressure]
[coolantPressure]
boundary = '1 2 3'
factor = 1
function = coolant_pressure_ramp
[]
[]
[PlenumPressure]
[plenumPressure]
boundary = '10 5'
initial_pressure = 0.5e6
startup_time = 0
R = 8.314462
output_initial_moles = initial_moles
temperature = plenum_temperature
volume = plenum_volume
material_input = fission_gas_released
output = plenum_pressure
initial_temperature = 293
[]
[]
[]
[Materials]
[fuel_swelling]
type = UO2VolumetricSwellingEigenstrain
block = 3
burnup = burnup
initial_fuel_density = 10310.8809782
total_densification = 0.006
gas_swelling_model_type = SIFGRS
eigenstrain_name = 'fuel_volumetric_swelling_eigenstrain'
[]
[fuel_thermal]
type = UO2Thermal
thermal_conductivity_model = NFIR
block = 3
temperature = temp
burnup = BuTC
initial_porosity = 0.0592261881186
[]
[fuel_elasticity_tensor]
type = UO2ElasticityTensor
block = 3
[]
[fuel_thermal_expansion]
type = UO2ThermalExpansionMartinEigenstrain
block = 3
stress_free_temperature = 293
eigenstrain_name = 'fuel_thermal_eigenstrain'
[]
[fuel_elastic_stress]
type = ComputeFiniteStrainElasticStress
block = '3'
[]
[clad_thermal]
type = ZryThermal
block = 1
temperature = temp
[]
[clad_inelastic_stress]
type = ComputeMultipleInelasticStress
block = 1
tangent_operator = elastic
inelastic_models ='plasticity'
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = 1
fast_neutron_fluence = fast_neutron_fluence
initial_fast_fluence = 1.20e26
cold_work_factor = 0.01
matpro_youngs_modulus = true
matpro_poissons_ratio = true
[]
## TODO: Creep is not active, but is transfered from the SM version.
## Adding creep causes the Peak Hoop strain to best match the FALCON
## results given by R. Montgomery and D. Sunderland. Only retaining
## plasticity matches the results from Wenfeng Liu, John Alvis, Robert Montgomery, and Ken Yueh
[clad_creep_stress]
type = ZryCreepLimbackHoppeUpdate
block = 1
fast_neutron_flux = fast_neutron_flux
fast_neutron_fluence = fast_neutron_fluence
initial_fast_fluence = 1.20e26
[]
[clad_thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 293.0
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[plasticity]
type = ZryPlasticityUpdate
block = 1
initial_fast_fluence = 1.20e26
fast_neutron_flux = fast_neutron_flux
fast_neutron_fluence = fast_neutron_fluence
cold_work_factor = .01
plasticity_model_type = MATPRO
output_properties = yield_stress
outputs = all
zircaloy_alloy_type = 4
[]
[fission_gas_release]
type = UO2Sifgrs
block = 3
temperature = temp
fission_rate = fission_rate
grain_radius = grain_radius
gbs_model = true
burnup = BuTC
transient_option = MICROCRACKING
[]
[clad_density]
type = Density
block = 1
density = 6551
[]
[fuel_density]
type = Density
block = 3
[]
[strain_energy_density]
type = StrainEnergyDensity
block = '1 3'
incremental = true
[]
[]
[UserObjects]
[avg_gap]
type = LayeredAverage
block = 3
variable = penetration
direction = y
num_layers = 48
[]
[pbz]
type = PelletBrittleZone
block = 3
pellet_id = pellet_id
temperature = temp
pellet_radius = 0.00527
number_pellets = 1
execute_on = timestep_begin
[]
[integral_burnup]
type = LayeredAverage
block = 3
variable = burnup
direction = y
num_layers = 1
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_converged_reason -ksp_converged_reason -snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package -mat_mffd_err -pc_factor_shift_type '
'-pc_factor_shift_amount'
petsc_options_value = 'lu superlu_dist 1e-5 NONZERO 1e-12'
line_search = 'none'
l_max_its = 40
l_tol = 8e-3
nl_max_its = 40
nl_rel_tol = 1e-3
nl_abs_tol = 1e-10
dtmin = 0.00001
dtmax = 1.0
start_time = 0
end_time = 100
[TimeStepper]
type = IterationAdaptiveDT
dt = 0.0001
optimal_iterations = 200
linear_iteration_ratio = 100
timestep_limiting_function = linear_heat_rate_profile
max_function_change = 500000
force_step_every_function_point = true
[]
[]
[Dampers]
[limitT]
type = MaxIncrement
max_increment = 200.0
variable = temp
[]
[limitX]
type = MaxIncrement
max_increment = 1e-4
variable = disp_x
[]
[]
[Postprocessors]
[max_hoop_strain]
type = ElementExtremeValue
variable = strain_zz
block = 1
[]
[max_SED]
type = ElementExtremeValue
variable = SED
block = 1
[]
[average_grain_radius]
type = ElementAverageValue
block = 3
outputs = 'exodus'
variable = grain_radius
[]
[clad_inner_vol]
type = InternalVolume
boundary = 7
outputs = 'exodus'
execute_on = 'timestep_begin initial'
[]
[flux_from_clad]
type = SideDiffusiveFluxIntegral
variable = temp
boundary = 5
diffusivity = thermal_conductivity
outputs = 'exodus'
[]
[flux_from_fuel]
type = SideDiffusiveFluxIntegral
variable = temp
boundary = 10
diffusivity = thermal_conductivity
outputs = 'exodus'
[]
[rod_total_power]
type = ElementIntegralPower
variable = temp
fission_rate = fission_rate
block = 3
[]
[rod_input_power]
type = FunctionValuePostprocessor
function = linear_heat_rate_profile
scale_factor = 0.106
[]
[average_fission_rate]
type = ElementAverageValue
variable = fission_rate
block = '3'
[]
[RAE]
type = RadialAverageEnthalpy
vector_postprocessor = rad_temp
radial_direction = x
axial_direction = y
axial_position = 0.0503
temperature_name = temp
[]
[peak_RAE]
type = TimeExtremeValue
postprocessor = RAE
[]
[]
[VectorPostprocessors]
[rad_temp]
type = NodalValueSampler
block = 3
sort_by = y
variable = temp
execute_on = timestep_end
outputs = dummy
[]
[]
[StandardLWRFuelRodOutputs]
fuel_pellet_blocks = 3
cladding_blocks = 1
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[chkfile]
type = CSV
show = 'average_centerline_fuel_temperature average_fission_rate fission_gas_released_percentage peak_RAE rod_total_power'
execute_on = 'FINAL'
[]
[console]
type = Console
max_rows = 25
output_linear = true
[]
[dummy]
type = CSV
enable = false
[]
[]
(assessment/LWR/validation/LOCA_REBEKA_cladding_burst_tests/analysis/rebeka_2d_02MPa/rebeka_singlerod_2d_02MPa.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.0
order = SECOND
family = LAGRANGE
displacements = 'disp_x disp_y'
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = rebeka_singlerod.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 573.0
[]
[]
[Functions]
[temperature_func]
type = PiecewiseLinear
x = '0. 700. '
y = '573. 1273.' # From 300 to 1000 C at 1 K/s
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 700. '
y = '2.e+06 2.e+06' # 20 bar
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 700. '
y = '1.e+05 1.e+05' # atmospheric pressure
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[clad]
block = cladding
add_variables = false
strain = FINITE
decomposition_method = EigenSolution
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz hoop_stress'
[]
[]
[AuxVariables]
[creep_rate_aux]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[scale_thickness]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfract_total]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfgain_total]
order = CONSTANT
family = MONOMIAL
[]
[burst_stress]
order = CONSTANT
family = MONOMIAL
[]
[burst]
order = CONSTANT
family = MONOMIAL
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate_aux]
type = MaterialRealAux
variable = creep_rate_aux
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[scl_thickness]
type = MaterialRealAux
variable = scale_thickness
property = oxide_scale_thickness
boundary = 2
[]
[ofract_total]
type = MaterialRealAux
variable = oxywtfract_total
property = current_oxygen_weight_frac_total
boundary = 2
[]
[ofgain_total]
type = MaterialRealAux
boundary = 2
variable = oxywtfgain_total
property = oxygen_weight_frac_gained_total
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = 2
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = 2
execute_on = timestep_end
[]
[]
[BCs]
[inner_temperature]
type = REBEKADirichletBC
variable = temperature
function_tempm = temperature_func
minimum_temperature = 573.
translation = 0.1625
boundary = 4
[]
[no_y_midsection]
type = DirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply steam pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 101 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[CoolantChannel]
[convective_clad_surface]
boundary = 2
variable = temperature
inlet_temperature = 473.
inlet_pressure = 1.e+05
inlet_massflux = 1.0 # kg/m^2-sec # almost stagnant steam
rod_diameter = 10.75e-03
rod_pitch = 1.26e-02 # default
number_axial_zone = 15
oxide_thickness = scale_thickness
[]
[]
[Materials]
[thermal]
type = ZryThermal
block = cladding
temperature = temperature
[]
[clad_elasticity_tensor]
type = ComputeIsotropicElasticityTensor
block = cladding
youngs_modulus = 1.0e11
poissons_ratio = 0.3
[]
[clad_stress]
type = ComputeMultipleInelasticStress
tangent_operator = elastic
inelastic_models = 'clad_zrycreep'
block = cladding
[]
[clad_zrycreep]
type = ZryCreepLOCAUpdate
block = cladding
temperature = temperature
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
temperature_loca_creep_begin = 501 # see Erbacher et al., 1982
temperature_standard_thermal_creep_end = 500
[]
[thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = cladding
temperature = temperature
stress_free_temperature = 573.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[density]
type = Density
block = cladding
[]
[phase]
type = ZrPhase
block = cladding
temperature = temperature
numerical_method = 2
[]
[oxidation]
type = ZryOxidation
boundary = 2
temperature = temperature
clad_inner_radius = 0.00465
clad_outer_radius = 0.005375
normal_operating_temperature_model = epri_kwu_ce
high_temperature_model = leistikow
use_coolant_channel = true
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = 2
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate_aux
temperature = temperature
fraction_beta_phase = fract_beta_phase
fraction_oxygen_gain = oxywtfgain_total
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0
n_startup_steps = 1
end_time = 700.
dtmax = 1.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average temperature of cladding exterior
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = cladding
[]
[max_clad_temp]
type = NodalExtremeValue
block = cladding
value_type = max
variable = temperature
[]
[max_oxygen_fract]
type = ElementExtremeValue
block = cladding
value_type = max
variable = oxywtfract_total
[]
[max_betaph_fract]
type = ElementExtremeValue
block = cladding
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
block = cladding
value_type = max
variable = creep_rate_aux
[]
[max_creep_strain_mag]
type = ElementExtremeValue
block = cladding
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
block = cladding
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
block = cladding
value_type = max
variable = hoop_stress
[]
[vonmises_stress_clad]
type = ElementAverageValue
block = cladding
variable = vonmises_stress
[]
[min_burst_stress]
type = ElementExtremeValue
block = cladding
value_type = min
variable = burst_stress
[]
[burst]
type = ElementExtremeValue
block = cladding
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = cladding
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = cladding
plenum_boundary_name = 4
external_clad_boundary_name = 2
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = rebeka_2d_02MPa_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-12/puzry-12_aniso.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-12.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 1200. '
y = '1.e+05 1.e+05 1.546e+06' # Linear increase at 0.0723 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 1200. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
# Circumferential steady-state creep test and analysis of Zircaloy-4 fuel cladding
# Nuclear Engineering and Design, 53, 2312-2322 (2021)
[F]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.738 0.738 0.57'
[]
[G]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.174 0.174 0.45'
[]
[H]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.588 0.588 0.48'
[]
[L]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[M]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[N]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = TaylorExpansion
use_automatic_differentiation = true
[]
[]
[]
[]
[Kernels]
[heat]
type = ADHeatConduction
variable = temperature
[]
[heat_ie]
type = ADHeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = ADMaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = ADMaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = ADMaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = ADMaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = ADMaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = ADFunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = ADDirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = ADDirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ADZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1.e+11
poissons_ratio = 0.3
block = 1
[]
[hill_constants]
type = ADHillConstants
hill_constants = "0.738 0.174 0.588 1.0 1.0 1.0"
function_names = "F G H L M N"
temperature = temperature
[]
[creep_update]
type = ADZryAnisoCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 2.5e-05
temperature = temperature
temperature_standard_thermal_creep_end = 700
temperature_loca_creep_begin = 900.
fract_beta_phase_name = 'fract_beta_phase'
max_integration_error = 1000000.0
absolute_tolerance = 1e-07
relative_tolerance = 1e-07
[]
[creep]
type = ADComputeMultipleInelasticStress
block = 1
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ADZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = ADDensity
block = 1
[]
[phase]
type = ADZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ADZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = NEWTON
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0.
n_startup_steps = 1
end_time = 2500.
dtmax = 1.
dtmin = 1.0e-9
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-12_aniso_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/LOCA_ORNL_cladding_burst_tests/analysis/Zr2_1/ornl_zr2_1.i)
# Simulation ORNL burst tests Zr2_1
[GlobalParams]
density = 6550.
order = SECOND
family = LAGRANGE
displacements = 'disp_x disp_y'
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = zr2_ornl_burst_test_mesh.e
[]
[]
[Variables]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func] # only 10 inches of the rod are within the heated zone (cf. Terrani email)
type = PiecewiseBilinear
data_file = temperature_ornl_zr2_1.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
data_file = pressure_inner_ornl_zr2_1.csv
scale_factor = 1.e+06
format = columns
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 400. '
y = '0.1 0.1 ' # atmospheric pressure
scale_factor = 1.e+06
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[clad]
block = cladding
add_variables = true
strain = FINITE
decomposition_method = EigenSolution
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
eigenstrain_names = 'clad_thermal_eigenstrain'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz hoop_stress'
[]
[]
[AuxVariables]
[creep_rate_aux]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[scale_thickness]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfract_total]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfgain_total]
order = CONSTANT
family = MONOMIAL
[]
[burst_stress]
order = CONSTANT
family = MONOMIAL
[]
[burst]
order = CONSTANT
family = MONOMIAL
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate_aux]
type = MaterialRealAux
variable = creep_rate_aux
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[scl_thickness]
type = MaterialRealAux
variable = scale_thickness
property = oxide_scale_thickness
boundary = 2
[]
[ofract_total]
type = MaterialRealAux
variable = oxywtfract_total
property = current_oxygen_weight_frac_total
boundary = 2
[]
[ofgain_total]
type = MaterialRealAux
boundary = 2
variable = oxywtfgain_total
property = oxygen_weight_frac_gained_total
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = 2
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = 2
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = FunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 4'
preset = false
[]
[no_y_top]
type = DirichletBC
variable = disp_y
boundary = 3
value = 0.
preset = false
[]
[Pressure]
[outer_pressure] # apply steam pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[mid_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 2 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
type = ZryThermal
block = cladding
temperature = temperature
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = cladding
matpro_youngs_modulus = false
matpro_poissons_ratio = false
[]
[clad_stress]
type = ComputeMultipleInelasticStress
tangent_operator = elastic
inelastic_models = 'clad_zrycreep'
block = cladding
[]
[clad_zrycreep]
type = ZryCreepLOCAUpdate
block = cladding
temperature = temperature
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
temperature_loca_creep_begin = 301
temperature_standard_thermal_creep_end = 300
[]
[thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = cladding
temperature = temperature
stress_free_temperature = 300.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[density]
type = Density
block = cladding
[]
[phase]
type = ZrPhase
block = cladding
temperature = temperature
numerical_method = 2
[]
[oxidation]
type = ZryOxidation
boundary = 2
temperature = temperature
clad_inner_radius = 0.004875
clad_outer_radius = 0.005580
normal_operating_temperature_model = epri_kwu_ce
high_temperature_model = leistikow
#use_coolant_channel = true
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = 2
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate_aux
temperature = temperature
fraction_beta_phase = fract_beta_phase
fraction_oxygen_gain = oxywtfgain_total
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0
n_startup_steps = 1
end_time = 400.
dtmax = 1.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[Postprocessors]
[pressure_inner]
type = FunctionValuePostprocessor
function = inner_pressure_func
execute_on = 'initial timestep_end'
[]
[pressure_outer]
type = FunctionValuePostprocessor
function = outer_pressure_func
execute_on = 'initial timestep_end'
[]
[ave_clad_temp]
type = SideAverageValue
boundary = 2
variable = temperature
execute_on = 'initial timestep_end'
[]
[max_clad_temp]
type = NodalExtremeValue
block = cladding
value_type = max
variable = temperature
execute_on = 'initial timestep_end'
[]
[min_clad_temp]
type = NodalExtremeValue
block = cladding
value_type = min
variable = temperature
execute_on = 'initial timestep_end'
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = cladding
[]
[max_oxygen_fract]
type = ElementExtremeValue
block = cladding
value_type = max
variable = oxywtfract_total
execute_on = 'initial timestep_end'
[]
[max_betaph_fract]
type = ElementExtremeValue
block = cladding
value_type = max
variable = fract_beta_phase
execute_on = 'initial timestep_end'
[]
[max_creep_rate]
type = ElementExtremeValue
block = cladding
value_type = max
variable = creep_rate_aux
execute_on = 'initial timestep_end'
[]
[max_creep_strain_mag]
type = ElementExtremeValue
block = cladding
value_type = max
variable = creep_strain_mag
execute_on = 'initial timestep_end'
[]
[max_hoop_strain]
type = ElementExtremeValue
block = cladding
value_type = max
variable = strain_zz
execute_on = 'initial timestep_end'
[]
[max_hoop_stress]
type = ElementExtremeValue
block = cladding
value_type = max
variable = hoop_stress
[]
[vonmises_stress_clad]
type = ElementAverageValue
block = cladding
variable = vonmises_stress
execute_on = 'initial timestep_end'
[]
[min_burst_stress]
type = ElementExtremeValue
block = cladding
value_type = min
variable = burst_stress
execute_on = 'initial timestep_end'
[]
[burst]
type = ElementExtremeValue
block = cladding
value_type = max
variable = burst
execute_on = 'initial timestep_end'
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = cladding
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[mid_disp_r_clad]
type = NodalVariableValue
variable = disp_x
nodeid = 22
[]
[stress_xx_midplane] # stress in the mid Element
type = ElementalVariableValue
variable = stress_xx
elementid = 19
[]
[stress_yy_midplane] # stress in the mid Element
type = ElementalVariableValue
variable = stress_yy
elementid = 19
[]
[stress_zz_midplane] # stress in the mid Element
type = ElementalVariableValue
variable = stress_zz
elementid = 19
[]
[strain_zz_midplane] # strain in the mid Element
type = ElementalVariableValue
variable = strain_zz
elementid = 19
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
plenum_boundary_name = 4
cladding_blocks = cladding
[]
[PerformanceMetricOutputs]
[]
[Outputs]
exodus = true
perf_graph = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 20
[]
[chkfile]
type = CSV
file_base = ornl_zr2_1_chkfile
show = 'pressure_inner max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/LOCA_Hardy_cladding_test/analysis/1pt0MPa/25C_sec/25C_sec_Hardy_Tube_Test_1pt0MPa.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
volumetric_locking_correction = false
displacements = 'disp_x disp_y'
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
group_variables = 'disp_x disp_y'
[]
[Mesh]
coord_type = RZ
patch_size = 10
patch_update_strategy = iteration
partitioner = centroid
centroid_partitioner_direction = y
[gen]
type = FuelPinMeshGenerator
include_fuel = false
include_clad = true
pellet_outer_radius = 0.0072527
clad_gap_width = 0.0
clad_top_gap_height = 0.0
clad_bot_gap_height = 0.0
clad_thickness = 0.38e-3
pellet_height = 0.5
pellet_quantity = 1
clad_mesh_density = customize
nx_c = 2
ny_c = 50
elem_type = QUAD8
[]
[]
[Variables]
[temperature]
initial_condition = 600.0
[]
[]
[AuxVariables]
[creep_rate_aux]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[total_hoop_strain]
order = CONSTANT
family = MONOMIAL
[]
[burst_stress]
order = CONSTANT
family = MONOMIAL
[]
[burst]
order = CONSTANT
family = MONOMIAL
[]
[]
[Functions]
[pressure_function]
type = PiecewiseLinear
x = '0 40'
y = '1 1'
[]
[temp_function]
type = PiecewiseLinear
y = '600 1600'
[]
[temperature_profile]
type = PiecewiseBilinear
y = '0 40'
x = '0 0.25224 0.50448'
z = '0.995 1.01 0.995 0.995 1.01 0.995'
axis = 1
[]
[inner_temperature]
type = CompositeFunction
functions = 'temp_function temperature_profile'
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[clad]
block = clad
add_variables = true
strain = FINITE
decomposition_method = EigenSolution
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz elastic_strain_xx elastic_strain_yy elastic_strain_zz
creep_strain_xx creep_strain_yy creep_strain_zz hoop_stress'
extra_vector_tags = 'ref'
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
extra_vector_tags = 'ref'
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
extra_vector_tags = 'ref'
[]
[]
[AuxKernels]
[creep_rate_aux]
type = MaterialRealAux
variable = creep_rate_aux
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[creep_rate]
type = MaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[total_hoop_strain]
type = RankTwoAux
rank_two_tensor = total_strain
variable = total_hoop_strain
index_i = 2
index_j = 2
execute_on = timestep_end
block = clad
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = clad_outside_right
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = clad_outside_right
execute_on = timestep_end
[]
[]
[BCs]
[Pressure]
[outer_surface]
boundary = 'clad_outside_bottom clad_outside_right clad_outside_top'
factor = 0.0
function = pressure_function
[]
[inner_surface]
boundary = 'clad_inside_right clad_inside_bottom clad_inside_top'
function = pressure_function
[]
[]
[u_bottom_fix]
type = DirichletBC
variable = disp_y
boundary = 1001
value = 0.0
[]
[x_fix]
type = DirichletBC
variable = disp_x
boundary = centerline
value = 0.0
[]
[temp_bc]
type = FunctionDirichletBC
function = inner_temperature
variable = temperature
boundary = 'clad_inside_bottom clad_inside_right clad_inside_top'
[]
[]
[Materials]
[clad_thermal]
type = ZryThermal
block = clad
zry_thermal_properties_model = MATPRO
temperature = temperature
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = clad
matpro_youngs_modulus = true
matpro_poissons_ratio = true
temperature = temperature
[]
[clad_stress]
type = ComputeMultipleInelasticStress
inelastic_models = 'clad_zrycreep'
block = clad
tangent_operator = nonlinear
[]
[clad_zrycreep]
type = ZryCreepLOCAUpdate
block = clad
temperature = temperature
model_irradiation_creep = false
model_primary_creep = true
model_thermal_creep = true
temperature_loca_creep_begin = 840 # values from the report
temperature_standard_thermal_creep_end = 975
[]
[thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = clad
temperature = temperature
stress_free_temperature = 600.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[clad_density]
type = Density
block = clad
density = 6550.0
[]
[phase]
type = ZrPhase
block = clad
temperature = temperature
numerical_method = 2
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = clad_outside_right
failure_criterion = combined_overstress_and_overstrain
hoop_stress = hoop_stress
hoop_creep_strain = creep_strain_zz
effective_strain_rate_creep = creep_rate_aux
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.0e-5
nl_abs_tol = 1.0e-8
start_time = 0
n_startup_steps = 1
end_time = 40
dtmax = 1
dtmin = 0.0000001
[TimeStepper]
type = IterationAdaptiveDT
timestep_limiting_postprocessor = material_timestep
dt = 1.0
[]
[]
[Postprocessors]
[ave_clad_temp]
type = SideAverageValue
boundary = clad_outside_right
variable = temperature
[]
[gas_volume]
type = InternalVolume
boundary = all_clad_interior
execute_on = 'initial linear'
[]
[max_clad_temp]
type = NodalExtremeValue
block = clad
value_type = max
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = clad
[]
[max_hoop_stress]
type = ElementExtremeValue
block = clad
value_type = max
variable = hoop_stress
[]
[vonmises_stress_clad]
type = ElementAverageValue
block = clad
variable = vonmises_stress
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = total_hoop_strain
[]
[max_disp_x]
type = NodalExtremeValue
block = clad
value_type = max
variable = disp_x
[]
[min_burst_stress]
type = ElementExtremeValue
block = clad
value_type = min
variable = burst_stress
[]
[burst]
type = ElementExtremeValue
block = clad
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = clad
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
[]
[PerformanceMetricOutputs]
[]
[Outputs]
color = false
perf_graph = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[csv]
type = CSV
[]
[chkfile]
type = CSV
show = 'max_disp_x max_hoop_stress vonmises_stress_clad'
execute_on = 'FINAL'
[]
[]
[UserObjects]
[terminator1]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '5'
include_fuel = false
[]
[]
(assessment/LWR/validation/RIA_CABRI_REP_Na/analysis/REP_Na_3/REP_Na_3_RIA.i)
# REP Na 3 Rodlet RIA
[GlobalParams]
density = 10394.075 # assumed TD = 10970
displacements = 'disp_x disp_y'
temperature = temp
order = SECOND
family = LAGRANGE
energy_per_fission = 3.2e-11
volumetric_locking_correction = false
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
acceptable_iterations = 30
acceptable_multiplier = 10
restart_file_base = 'recover_files_cp/LATEST'
[]
[Mesh]
coord_type = RZ
[smeared_pellet_mesh]
type = FuelPinMeshGenerator
clad_mesh_density = customize
pellet_mesh_density = customize
nx_p = 11
ny_p = 128
ny_cu = 3
ny_c = 130
ny_cl = 3
nx_c = 4
clad_thickness = 0.000596
pellet_outer_radius = 0.0040956
pellet_quantity = 32
pellet_height = 0.0135890
clad_top_gap_height = 0.0298168
clad_bot_gap_height = 0.003
clad_gap_width = 82.0e-6
bottom_clad_height = 0.0015
top_clad_height = 0.0015
elem_type = QUAD8
[]
patch_size = 40
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temp]
[]
[]
[AuxVariables]
[fast_neutron_flux]
block = 1
[]
[fast_neutron_fluence]
block = 1
[]
[grain_radius]
block = 3
[]
[gap_cond]
order = CONSTANT
family = MONOMIAL
[]
[fuel_cond]
order = CONSTANT
family = MONOMIAL
[]
[swelling_strain]
order = CONSTANT
family = MONOMIAL
block = 3
[]
[total_hoop_strain]
order = CONSTANT
family = MONOMIAL
[]
[total_axial_strain]
order = CONSTANT
family = MONOMIAL
[]
[clad_coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[coolant_temp]
order = CONSTANT
family = MONOMIAL
[]
[clad_coolant_flux]
order = CONSTANT
family = MONOMIAL
[]
[coolant_channel_hmode]
order = CONSTANT
family = MONOMIAL
[]
[coolant_channel_htype]
order = CONSTANT
family = MONOMIAL
[]
[critical_heat_flux]
order = CONSTANT
family = MONOMIAL
[]
[oxide_thickness]
order = CONSTANT
family = MONOMIAL
[]
[SED]
order = CONSTANT
family = MONOMIAL
block = 1
[]
[oxywtfract_total]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfgain_total]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[]
[Functions]
[power_profile]
type = PiecewiseLinear
data_file = REPNa3_power_history_Full.csv
format = columns
[]
[axial_peaking_factors]
type = PiecewiseBilinear
data_file = REPNa3_axial_peaking_Full.csv
axis = 1
[]
[pressure_ramp]
type = PiecewiseLinear
xy_data = '0 101325
8640 15499970
17280 15499970
25920 15499970
34560 15499970
43200 15499970
51840 15499970
98798400 15499970
99273600 101325
99273610 101325
99273650 500008
99273700 500008
99273900 500008
99274000 101325
99274100 101325'
[]
[temp_ramp]
type = PiecewiseLinear
xy_data = '0 293.15
8640 583.15
17280 583.15
25920 583.15
34560 583.15
43200 583.15
51840 583.15
98798400 583.15
99273600 293.15
99273610 293.15
99273650 553.15
99273700 553.15
99273900 553.15
99274000 293.15
99274100 293.15'
[]
[Fuel_CTE_function] #Fuel CTE as a function of temp from MATPRO data
type = PiecewiseLinear
xy_data = ' 0 1.000E-05
300 1.000E-05
350 1.000E-05
400 1.000E-05
450 1.000E-05
500 1.001E-05
550 1.002E-05
600 1.003E-05
650 1.005E-05
700 1.008E-05
750 1.011E-05
800 1.015E-05
850 1.020E-05
900 1.026E-05
950 1.032E-05
1000 1.039E-05
1050 1.046E-05
1100 1.053E-05
1150 1.061E-05
1200 1.069E-05
1250 1.077E-05
1300 1.085E-05
1350 1.094E-05
1400 1.102E-05
1450 1.111E-05
1500 1.119E-05
1550 1.127E-05
1600 1.135E-05
1650 1.143E-05
1700 1.151E-05
1750 1.158E-05
1800 1.166E-05
1850 1.173E-05
1900 1.180E-05
1950 1.187E-05
2000 1.193E-05
2050 1.199E-05
2100 1.205E-05
2150 1.211E-05
2200 1.217E-05
2250 1.222E-05
2300 1.227E-05
2350 1.232E-05
2400 1.237E-05
2450 1.242E-05
2500 1.246E-05
2550 1.250E-05
2600 1.254E-05
2650 1.258E-05
2700 1.262E-05
2750 1.265E-05
2800 1.268E-05
2850 1.271E-05
2900 1.274E-05
2950 1.277E-05
3000 1.280E-05
3050 1.282E-05
3100 1.285E-05'
[]
[burnup_GWd]
type = ParsedFunction
expression = bu*950
symbol_names = 'bu'
symbol_values = 'average_burnup_EAV'
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[fuel]
block = 3
strain = FINITE
incremental = true
eigenstrain_names = 'fuel_relocation_eigenstrain fuel_thermal_eigenstrain
fuel_volumetric_swelling_eigenstrain'
extra_vector_tags = 'ref'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz'
[]
[clad]
block = 1
strain = FINITE
incremental = true
eigenstrain_names = 'clad_irradiation_growth_eigenstrain
clad_thermal_eigenstrain'
extra_vector_tags = 'ref'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz plastic_strain_xx plastic_strain_yy plastic_strain_zz
creep_strain_xx creep_strain_yy creep_strain_zz elastic_strain_xx
elastic_strain_yy elastic_strain_zz hoop_stress'
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temp
extra_vector_tags = 'ref'
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temp
extra_vector_tags = 'ref'
[]
[heat_source_fuel]
type = NeutronHeatSource
variable = temp
block = 3
burnup_function = burnup
extra_vector_tags = 'ref'
[]
[]
[Burnup]
[burnup]
block = 3
rod_ave_lin_pow = power_profile
axial_power_profile = axial_peaking_factors
num_radial = 80
num_axial = 33
a_upper = 0.4393480
a_lower = 0.0045
fuel_inner_radius = 0
fuel_outer_radius = 0.0040956
fuel_volume_ratio = 1
isotopes = 'U235 U238 Pu239 Pu240 Pu241 Pu242'
isotope_fractions = '0.045 0.955 0 0 0 0'
RPF = RPF
order = CONSTANT
family = MONOMIAL
[]
[]
[AuxKernels]
[fast_neutron_flux]
type = FastNeutronFluxAux
variable = fast_neutron_flux
block = 1
axial_power_profile = axial_peaking_factors
rod_ave_lin_pow = power_profile
factor = 3e13 #n/m2-s
execute_on = timestep_begin
[]
[fast_neutron_fluence]
type = FastNeutronFluenceAux
variable = fast_neutron_fluence
fast_neutron_flux = fast_neutron_flux
block = 1
execute_on = timestep_begin
[]
[grain_radius]
type = GrainRadiusAux
block = 3
variable = grain_radius
temperature = temp
execute_on = linear
[]
[gap_conductance]
type = MaterialRealAux
property = gap_conductance
variable = gap_cond
boundary = 10
[]
[fuel_conductance]
type = MaterialRealAux
property = thermal_conductivity
variable = fuel_cond
block = 3
[]
[swelling_strain]
type = MaterialRealAux
property = volumetric_swelling_strain
variable = swelling_strain
block = 3
[]
[total_hoop_strain]
type = RankTwoScalarAux
rank_two_tensor = total_strain
variable = total_hoop_strain
scalar_type = HoopStress
execute_on = timestep_end
block = 1
[]
[total_axial_strain]
type = RankTwoScalarAux
rank_two_tensor = total_strain
variable = total_axial_strain
scalar_type = AxialStress
execute_on = timestep_end
block = 1
[]
[clad_coolant_htc]
type = MaterialRealAux
property = coolant_channel_htc
variable = clad_coolant_htc
boundary = 2
[]
[coolant_temp]
type = MaterialRealAux
property = coolant_temperature
variable = coolant_temp
boundary = 2
[]
[clad_coolant_flux]
type = MaterialRealAux
property = output_heat_flux
variable = clad_coolant_flux
boundary = 2
[]
[coolant_channel_hmode]
type = MaterialRealAux
property = coolant_channel_hmode
variable = coolant_channel_hmode
boundary = 2
[]
[coolant_channel_htype]
type = MaterialRealAux
property = coolant_channel_htype
variable = coolant_channel_htype
boundary = 2
[]
[critical_heat_flux]
type = MaterialRealAux
property = critical_heat_flux
variable = critical_heat_flux
boundary = 2
[]
[oxide]
type = MaterialRealAux
property = oxide_scale_thickness
variable = oxide_thickness
boundary = 2
[]
[SED]
type = MaterialRealAux
variable = SED
property = strain_energy_density
execute_on = timestep_end
[]
[ofract_total]
type = MaterialRealAux
variable = oxywtfract_total
property = current_oxygen_weight_frac_total
execute_on = timestep_end
boundary = 2
[]
[ofgain_total]
type = MaterialRealAux
variable = oxywtfgain_total
property = oxygen_weight_frac_gained_total
execute_on = timestep_end
boundary = 2
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
block = 1
[]
[]
[Contact]
[pellet_clad_mechanical]
primary = 5
secondary = 10
penalty = 1e10
formulation = penalty
normalize_penalty = false
model = frictionless
normal_smoothing_distance = 0.1
[]
[]
[ThermalContact]
[thermal_contact]
type = GasGapHeatTransfer
variable = temp
primary = 5
secondary = 10
initial_moles = initial_moles
gas_released = fission_gas_released
jump_distance_model = LANNING
plenum_pressure = plenum_pressure
contact_pressure = contact_pressure
roughness_primary = 1.0e-6
roughness_secondary = 0.5e-6
roughness_coef = 3.2
normal_smoothing_distance = 0.1
quadrature = true
contact_coef = 20
emissivity_primary = 1
emissivity_secondary = 1
refab_time = 99187200
refab_gas_types = He
refab_fractions = 1
[]
[]
[BCs]
[no_x_all]
type = DirichletBC
variable = disp_x
boundary = 12
value = 0.0
[]
[no_y_clad_bottom]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[]
[no_y_fuel_bottom]
type = DirichletBC
variable = disp_y
boundary = 20
value = 0.0
[]
[Pressure]
[coolantPressure]
boundary = '1 2 3'
function = pressure_ramp
[]
[]
[PlenumPressure]
[plenumPressure]
boundary = 9
initial_temperature = 293.15
initial_pressure = 2.60e6
startup_time = 0
R = 8.3143
output_initial_moles = initial_moles
temperature = plenum_temperature
volume = plenum_volume
material_input = fission_gas_released
output = plenum_pressure
refab_time = 99187200
refab_pressure = 0.31e6
refab_temperature = 293.15
refab_volume = 2.0e-6
[]
[]
[]
[CoolantChannel]
[convective_clad_surface]
boundary = '1 2 3'
variable = temp
inlet_temperature = temp_ramp # K
inlet_pressure = pressure_ramp # Pa
inlet_massflux = 3533 # kg/m^2-sec Based on flow rate provided and flow area and estimated density of 885.1 kg/m^3
flow_area = 8.74855e-5 #m^2
heated_diameter = 1.172526e-2 #m
hydraulic_diameter = 4.7e-3 #m
heated_perimeter = 2.984513e-2 #m
coolant_material = 'sodium'
compute_enthalpy = true
heat_transfer_mode = 0
#oxide_thickness = oxide_thickness # coupled oxide_thickness
number_axial_zone = 50
rod_pitch = 1.26e-2 # m
rod_diameter = 0.0095 # m
[]
[]
[Materials]
[swelling]
type = UO2VolumetricSwellingEigenstrain
block = 3
burnup_function = burnup
initial_fuel_density = 10394.075
include_solid_swelling = true
include_densification = true
total_densification = 0.00675
initial_porosity = 0.0525
eigenstrain_name = 'fuel_volumetric_swelling_eigenstrain'
[]
[fuel_thermal]
type = UO2Thermal
block = 3
thermal_conductivity_model = NFIR
temperature = temp
burnup_function = burnup
initial_porosity = 0.0525
[]
[fuel_elastic_stress]
type = ComputeFiniteStrainElasticStress
block = 3
[]
[fuel_elasticity_tensor]
type = UO2ElasticityTensor
block = 3
[]
[fuel_thermal_expansion]
type = ComputeInstantaneousThermalExpansionFunctionEigenstrain
block = 3
stress_free_temperature = 293.15
thermal_expansion_function = Fuel_CTE_function
eigenstrain_name = 'fuel_thermal_eigenstrain'
[]
[fuel_relocation]
type = UO2RelocationEigenstrain
block = 3
burnup_function = burnup
diameter = 0.0081912 #Fuel pellet diameter in m
rod_ave_lin_pow = power_profile
axial_power_profile = axial_peaking_factors
diametral_gap =164.0e-6
burnup_relocation_stop = 0.0
relocation_activation1 = 5000
eigenstrain_name = 'fuel_relocation_eigenstrain'
[]
[clad_thermal]
type = ZryThermal
block = 1
temperature = temp
[]
[clad_zrycreep]
type = ZryCreepLimbackHoppeUpdate
block = 1
fast_neutron_flux = fast_neutron_flux
fast_neutron_fluence = fast_neutron_fluence
zircaloy_material_type = stress_relief_annealed
max_inelastic_increment = 1.0e-4
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = 1
fast_neutron_fluence = fast_neutron_fluence
cold_work_factor = 0.5
oxygen_concentration = 0.02135
matpro_poissons_ratio = true
matpro_youngs_modulus = true
[]
[clad_inelastic_stress]
type = ComputeMultipleInelasticStress
block = 1
tangent_operator = elastic
inelastic_models = 'plasticity' #only use plasticity
[]
[clad_thermal_eigenstrain]
type = ZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 293.15
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[clad_irradiation_eigenstrain]
type = ZryIrradiationGrowthEigenstrain
block = 1
fast_neutron_fluence = fast_neutron_fluence
zircaloy_material_type = stress_relief_annealed
eigenstrain_name = 'clad_irradiation_growth_eigenstrain'
[]
[plasticity]
type = ZryPlasticityUpdate
block = 1
cold_work_factor = 0.5
fast_neutron_fluence = fast_neutron_fluence
fast_neutron_flux = fast_neutron_flux
plasticity_model_type = MATPRO
oxygen_concentration = 0.0
max_inelastic_increment = 1.0e-4
[]
[density_clad]
type = Density
block = 1
density = 6550
[]
[density_fuel]
type = Density
block = 3
[]
[fission_gas_release]
type = UO2Sifgrs
block = 3
temperature = temp
burnup_function = burnup
initial_porosity = 0.0525
grain_radius_const = 5.0e-6
gbs_model = false
transient_option = MICROCRACKING_BURNUP
[]
[ZryOxidation]
type = ZryOxidation
boundary = 2
clad_inner_radius = 0.0041178
clad_outer_radius = 0.0047549
use_coolant_channel = true
fast_neutron_flux = fast_neutron_flux
[]
[phase]
type = ZrPhase
block = 1
numerical_method = 2
[]
[strain_energy_density]
type = StrainEnergyDensity
incremental = true
[]
[]
[Dampers]
[BoundingValueNodalDamper]
type = BoundingValueNodalDamper
max_value = 3200
min_value = 200
variable = temp
[]
[contact_slip]
type = ContactSlipDamper
primary = 5
secondary = 10
min_damping_factor = 0.05
[]
[]
[Preconditioning]
[SMP]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-3
nl_max_its = 40
nl_rel_tol = 1e-4
nl_abs_tol = 1e-10
#start_time = 0
end_time = 99274100
dtmax = 10
dtmin = 1e-7
[TimeStepper]
type = IterationAdaptiveDT
dt = 10
optimal_iterations = 20
iteration_window = 4
linear_iteration_ratio = 100
timestep_limiting_function = power_profile
max_function_change = 1e5
force_step_every_function_point = true
timestep_limiting_postprocessor = material_timestep_control
time_t = '99273610 99273620 99273630 99273640 99273650 99273660 99273670 99273680'
time_dt = '10 10 10 10 10 10 10 10'
[]
[Quadrature]
order = FIFTH
side_order = SEVENTH
[]
[]
[Postprocessors]
[fis_gas_grain]
type = ElementIntegralFisGasGrainSifgrs
block = 3
outputs = exodus
[]
[fis_gas_boundary]
type = ElementIntegralFisGasBoundarySifgrs
block = 3
outputs = exodus
[]
[rod_input_power]
type = FunctionValuePostprocessor
function = power_profile
[]
[average_burnup_EAV]
type = ElementAverageValue
block = 3
variable = burnup
[]
[burnup_GWd]
type = FunctionValuePostprocessor
function = burnup_GWd
[]
#######################################
[penetration]
type = NodalVariableValue
variable = penetration
nodeid = 4415
use_displaced_mesh = 1
[]
[contact_pressure]
type = NodalVariableValue
variable = contact_pressure
nodeid = 4415
use_displaced_mesh = 1
[]
[gap_cond]
type = ElementalVariableValue
variable = gap_cond
elementid = 1324
use_displaced_mesh = 1
[]
[creep_hoop_strain]
type = ElementalVariableValue
variable = creep_strain_zz
elementid = 292
use_displaced_mesh = 1
[]
[elastic_hoop_strain]
type = ElementalVariableValue
variable = elastic_strain_zz
elementid = 292
use_displaced_mesh = 1
[]
[plastic_hoop_strain]
type = ElementalVariableValue
variable = plastic_strain_zz
elementid = 292
use_displaced_mesh = 1
[]
[total_hoop_strain]
type = ElementalVariableValue
variable = total_hoop_strain
elementid = 292
use_displaced_mesh = 1
[]
[clad_hoop_stress]
type = ElementalVariableValue
variable = hoop_stress
elementid = 292
use_displaced_mesh = 1
[]
[clad_axial_elongation]
type = NodalVariableValue
variable = disp_y
nodeid = 2031
use_displaced_mesh = 1
[]
[clad_oxide_thickness]
type = ElementalVariableValue
variable = oxide_thickness
elementid = 292
use_displaced_mesh = 1
[]
[clad_coolant_htc]
type = ElementalVariableValue
variable = clad_coolant_htc
elementid = 292
use_displaced_mesh = 1
[]
[coolant_temp]
type = ElementalVariableValue
variable = coolant_temp
elementid = 292
use_displaced_mesh = 1
[]
[fuel_centerline_temp]
type = NodalVariableValue
variable = temp
nodeid = 4384
[]
[fuel_surface_temp]
type = NodalVariableValue
variable = temp
nodeid = 4415
[]
[clad_inner_surface_temp]
type = NodalVariableValue
variable = temp
nodeid = 1027
[]
[clad_outer_surface_temp]
type = NodalVariableValue
variable = temp
nodeid = 1037
[]
[fuel_axial_elongation]
type = NodalVariableValue
variable = disp_y
nodeid = 6655
[]
[clad_radial_elongation]
type = NodalVariableValue
variable = disp_x
nodeid = 1037
[]
[fuel_radial_elongation]
type = NodalVariableValue
variable = disp_x
nodeid = 4415
[]
[SED_PPN_O]
type = ElementalVariableValue
variable = SED
elementid = 292
use_displaced_mesh = 1
[]
[SED_PPN_I]
type = ElementalVariableValue
variable = SED
elementid = 289
use_displaced_mesh = 1
[]
[OFract_PPN_O]
type = ElementalVariableValue
variable = oxywtfract_total
elementid = 292
use_displaced_mesh = 1
[]
[OGain_PPN_O]
type = ElementalVariableValue
variable = oxywtfgain_total
elementid = 292
use_displaced_mesh = 1
[]
#######################################
[max_fuel_temp]
type = NodalExtremeValue
block = 3
variable = temp
[]
[max_clad_temp]
type = NodalExtremeValue
block = 1
variable = temp
[]
[max_clad_SED]
type = ElementExtremeValue
block = 1
variable = SED
value_type = max
[]
[RAE]
type = RadialAverageEnthalpy
vector_postprocessor = rad_temp
radial_direction = x
axial_direction = y
axial_position = 0.22
temperature_name = temp
[]
[material_timestep_control]
type = MaterialTimeStepPostprocessor
block = 1
[]
[peak_RAE]
type = TimeExtremeValue
postprocessor = RAE
[]
[]
[VectorPostprocessors]
[ox_thick]
type = SideValueSampler
variable = oxide_thickness
boundary = 2
sort_by = y
outputs = 'outfile_oxide_thickness'
[]
[rad_temp]
type = NodalValueSampler
block = 3
sort_by = y
variable = temp
execute_on = timestep_end
outputs = 'outfile_radial_temp'
[]
[]
[StandardLWRFuelRodOutputs]
fuel_pellet_blocks = 3
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
csv = true
color = true
[outfile_oxide_thickness]
type = CSV
sync_times = '99273600 99274100'
sync_only = true
[]
[outfile_radial_temp]
type = CSV
enable = false
[]
[console]
type = Console
output_linear = true
max_rows = 10
[]
[chkfile]
type = CSV
show = 'plenum_temperature fission_gas_released_percentage
average_centerline_fuel_temperature average_burnup peak_RAE'
execute_on = 'FINAL'
[]
[exodus]
type = Exodus
time_step_interval = 4
end_time = 99273700
[]
[exodus_RIA]
type = Exodus
time_step_interval = 2
start_time = 99273695
[]
[]
(examples/multiapp/pin2.i)
## In this example the multiapp system is called to run another BISON simulation.
## (input1.i calls input2.i) An application of this might be multiple fuel pins
## in an assembly. This example also demonstrates the internal mesh maker.
[GlobalParams]
density = 10200
displacements = 'disp_x disp_y'
order = FIRST
family = LAGRANGE
energy_per_fission = 3.2e-11 # J/fission
a_lower = 0.06951
a_upper = 3.72711
initial_porosity = 0.04
[]
# ==================================================== #
# Mesh (and Geometry, internally-meshed)
# ==================================================== #
[Mesh]
coord_type = RZ
[smeared_pellet_mesh]
type = FuelPinMeshGenerator
clad_mesh_density = customize
pellet_mesh_density = customize
clad_thickness = 0.0005
pellet_outer_radius = 0.0041
clad_bot_gap_height = 0.00152
clad_top_gap_height = 0.16
pellet_quantity = 1
pellet_height = 3.6576
clad_gap_width = 8.0e-05
bottom_clad_height = 0.0167
top_clad_height = 0.0167
nx_p = 6 # number of radial elements in the fuel
ny_p = 48 # number of axial elements in the fuel
nx_c = 3 # number of elements in the clad thickness
ny_c = 48 # number of elements in the axially in the clad
ny_cu = 1
ny_cl = 1
intervals = '0.03866 0.08211 0.08211 0.08211 0.08212 0.08211 0.08211 0.08211 0.0381 0.08065 0.08065 0.08065 0.08065 0.08065 0.08065 0.0381 0.08065 0.08065 0.08065 0.08065 0.08065 0.08065 0.0381 0.08065 0.08065 0.08065 0.08065 0.08065 0.08065 0.0381 0.08065 0.08065 0.08065 0.08065 0.08065 0.08065 0.0381 0.08065 0.08065 0.08065 0.08065 0.08065 0.08065 0.0381 0.079212 0.079212 0.079212 0.079212 0.079212'
elem_type = QUAD4
[]
partitioner = centroid
centroid_partitioner_direction = y
patch_size = 10
patch_update_strategy = auto
[]
[DefaultElementQuality]
aspect_ratio_upper_bound = 493
[]
# ==================================================== #
# Dimensions and Primary Variables
# ==================================================== #
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
group_variables = 'disp_x disp_y'
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temp]
initial_condition = 3.000000e+02
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[pellets]
block = 3
add_variables = false
strain = FINITE
eigenstrain_names = 'fuel_relocation_strain fuel_thermal_strain fuel_volumetric_strain'
generate_output = 'vonmises_stress hydrostatic_stress stress_xx stress_yy stress_zz strain_xx strain_yy strain_zz'
extra_vector_tags = 'ref'
[]
[clad]
block = 1
add_variables = false
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain clad_irradiation_strain'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz creep_strain_xx creep_strain_yy creep_strain_xy creep_strain_zz strain_xx strain_yy strain_zz'
extra_vector_tags = 'ref'
[]
[]
# ==================================================== #
# Auxiliary Variables
# ==================================================== #
[AuxVariables]
# ================================================== #
# Nodal Quantities
# ================================================== #
[htcl]
initial_condition = 500.0
[]
[htcv]
initial_condition = 0.0
[]
[Tl]
initial_condition = 565.0
[]
[Tv]
initial_condition = 565.0
[]
[burnup]
block = 3
[]
[fast_neutron_flux]
block = 1
[]
[fast_neutron_fluence]
block = 1
[]
[grain_radius]
block = 3
initial_condition = 5.240000e-06
[]
# ================================================== #
# Constant Monomial Quantities (Non-Mechanics)
# ================================================== #
[pellet_id]
order = CONSTANT
family = MONOMIAL
block = 3
[]
[axial_fission_rate]
order = CONSTANT
family = MONOMIAL
[]
[axial_burnup]
order = CONSTANT
family = MONOMIAL
[]
[axial_temperature]
order = CONSTANT
family = MONOMIAL
[]
[gap_conductivity]
order = CONSTANT
family = MONOMIAL
[]
[porosity]
order = CONSTANT
family = MONOMIAL
initial_condition = 0.04
[]
[]
# ==================================================== #
# Time- and Space-Dependent Source and BCs
# ==================================================== #
[Functions]
[linear_heat_rate_profile]
type = PiecewiseLinear
x = '-100 0 5000'
y = '0 0 25000'
scale_factor = 1
[]
[axial_peaking_factors]
type = ParsedFunction
expression = 1
[]
[coolant_temperature]
type = PiecewiseLinear
x = '-100 0'
y = '293 565'
axis = y
[]
[coolant_pressure_ramp]
# used in coolantPressure BC
type = PiecewiseLinear
scale_factor = 1
x = '0 10000.0'
y = '0 1.0'
[]
[]
# ==================================================== #
# Burnup Equation Set
# ==================================================== #
[Burnup]
[burnup]
block = 3
rod_ave_lin_pow = linear_heat_rate_profile
axial_power_profile = axial_peaking_factors
num_radial = 80
num_axial = 49
fuel_inner_radius = 0.0
fuel_outer_radius = 0.0041
fuel_volume_ratio = 1.0
isotopes = 'U235 U238'
isotope_fractions = '3.100e-02 9.690e-01'
RPF = RPF
[]
[]
# ==================================================== #
# Primary Kernels used in Heat Transfer
# ==================================================== #
[Kernels]
[gravity]
type = Gravity
variable = disp_y
value = -9.81
[]
[heat]
# gradient term in heat conduction equation
type = HeatConduction
variable = temp
extra_vector_tags = 'ref'
[]
[heat_ie]
# time term in heat conduction equation
type = HeatConductionTimeDerivative
variable = temp
extra_vector_tags = 'ref'
[]
[heat_source]
type = NeutronHeatSource
fission_rate = fission_rate
variable = temp
extra_vector_tags = 'ref'
block = 3
[]
[]
[AuxKernels]
# ================================================== #
# Pre-Defined Types
# ================================================== #
[pelletid]
type = PelletIdAux
block = 3
variable = pellet_id
number_pellets = 1
execute_on = initial
[]
[fast_neutron_flux]
type = FastNeutronFluxAux
variable = fast_neutron_flux
block = 1
rod_ave_lin_pow = linear_heat_rate_profile
axial_power_profile = axial_peaking_factors
factor = 1.27e+14 # (n/m2-s per W/m)
execute_on = timestep_begin
[]
[fast_neutron_fluence]
type = FastNeutronFluenceAux
variable = fast_neutron_fluence
block = 1
fast_neutron_flux = fast_neutron_flux
execute_on = timestep_begin
[]
[fuel_porosity]
type = PorosityAuxUO2
block = 3
variable = porosity
execute_on = linear
[]
[grain_radius]
type = GrainRadiusAux
block = 3
variable = grain_radius
temperature = temp
execute_on = linear
[]
[gap_conductance]
type = MaterialRealAux
property = gap_conductance
variable = gap_conductivity
boundary = 10
execute_on = linear
[]
[conductance]
type = MaterialRealAux
property = gap_conductance
variable = gap_conductivity
boundary = 10
execute_on = linear
[]
# ================================================== #
# Other General Types
# ================================================== #
[axial_burnup]
type = SpatialUserObjectAux
block = 3
variable = axial_burnup
user_object = axial_burnup
execute_on = timestep_begin
[]
[axial_temperature]
type = SpatialUserObjectAux
block = 3
variable = axial_temperature
user_object = axial_temperature
execute_on = timestep_begin
[]
[]
# ==================================================== #
# Mechanical and Thermal Contact
# ==================================================== #
[Contact]
[pellet_clad_mechanical]
primary = 5
secondary = 10
penalty = 1e14
normalize_penalty = true
normal_smoothing_distance = 0.1
model = frictionless
formulation = Kinematic
[]
[]
[ThermalContact]
[thermal_contact]
type = GasGapHeatTransfer
variable = temp
primary = 5
secondary = 10
roughness_coef = 3.200000e+00
roughness_primary = 1.8e-06
roughness_secondary = 8e-07
jump_distance_model = LANNING
plenum_pressure = plenum_pressure
contact_pressure = contact_pressure
initial_moles = initial_moles
gas_released = fission_gas_released
tangential_tolerance = 0.0001
normal_smoothing_distance = 0.1
order = FIRST
[]
[]
[BCs]
[no_x_all]
type = DirichletBC
variable = disp_x
boundary = 12
value = 0.0
[]
[no_y_fuel_bottom]
type = DirichletBC
variable = disp_y
boundary = 20
value = 0.0
[]
[no_y_clad_bottom]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[]
[convective_clad_surface_bottom]
type = ConvectiveFluxBC
boundary = '1 2 3'
variable = temp
rate = 38200.0 #convection coefficient (h)
initial = 565.0
final = 585.0
duration = 1.0e4 #duration of initial power ramp
[]
[Pressure]
[coolantPressure]
boundary = '1 2 3'
factor = 1.55132e+07
function = coolant_pressure_ramp
[]
[]
[PlenumPressure]
# apply plenum pressure on clad inner walls and pellet surfaces
[plenumPressure]
boundary = 9
initial_pressure = 1.99948e+06
startup_time = 0
R = 8.314462
output_initial_moles = initial_moles
temperature = ave_temp_interior
volume = gas_volume
material_input = fission_gas_released
output = plenum_pressure
[]
[]
[]
# ==================================================== #
# Specification of Material Properties
# ==================================================== #
[Materials]
[fuel_thermal]
type = UO2Thermal
thermal_conductivity_model = NFIR
block = 3
temperature = temp
burnup = burnup
[]
[fuel_elasticity_tensor]
type = ComputeIsotropicElasticityTensor
block = 3
youngs_modulus = 2.0e11
poissons_ratio = 0.345
[]
[fuel_elastic_stress]
type = ComputeFiniteStrainElasticStress
block = 3
[]
[fuel_thermal_expansion]
type = ComputeThermalExpansionEigenstrain
block = 3
thermal_expansion_coeff = 10.0e-6
temperature = temp
stress_free_temperature = 300.0
eigenstrain_name = fuel_thermal_strain
[]
[fuel_relocation]
type = UO2RelocationEigenstrain
block = 3
burnup = burnup
rod_ave_lin_pow = linear_heat_rate_profile
axial_power_profile = axial_peaking_factors
relocation_activation1 = 5000
relocation_model = ESCORE_modified
eigenstrain_name = fuel_relocation_strain
diameter = 0.008192
diametral_gap =0.000168
# Average burnup at which fuel comes into contact with clad at 25kW/m
burnup_relocation_stop = 0.0315
[]
[fuel_volumetric_swelling]
type = UO2VolumetricSwellingEigenstrain
gas_swelling_model_type = SIFGRS
block = 3
temperature = temp
burnup = burnup
initial_fuel_density = 10200.0
eigenstrain_name = fuel_volumetric_strain
total_densification = 0.01
[]
[fission_gas_release]
type = UO2Sifgrs
axial_power_profile = axial_peaking_factors
block = 3
burnup = burnup
fission_rate = fission_rate
hydrostatic_stress = hydrostatic_stress
grain_radius = grain_radius
pellet_brittle_zone = pbz
pellet_id = pellet_id
rod_ave_lin_pow = linear_heat_rate_profile
temperature = temp
[]
[fuel_density]
type = Density
block = 3
[]
[clad_thermal]
type = ZryThermal
block = 1
temperature = temp
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = 1
[]
[clad_stress]
type = ComputeMultipleInelasticStress
tangent_operator = elastic
inelastic_models = 'clad_zrycreep'
block = 1
[]
[clad_zrycreep]
type = ZryCreepLimbackHoppeUpdate
block = 1
temperature = temp
fast_neutron_flux = fast_neutron_flux
fast_neutron_fluence = fast_neutron_fluence
model_irradiation_creep = true
model_primary_creep = true
model_thermal_creep = true
[]
[thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = 1
temperature = temp
stress_free_temperature = 300.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[irradiation_swelling]
type = ZryIrradiationGrowthEigenstrain
block = 1
fast_neutron_fluence = fast_neutron_fluence
zircaloy_material_type = stress_relief_annealed
eigenstrain_name = clad_irradiation_strain
[]
[clad_density]
type = Density
block = 1
density = 7833
[]
[]
# ==================================================== #
# User Objects for Output Processing
# ==================================================== #
[UserObjects]
[pbz]
type = PelletBrittleZone
block = 3
pellet_id = pellet_id
temperature = temp
pellet_radius = 0.0041
number_pellets = 1
execute_on = linear
[]
[averagefissionrate]
type = LayeredAverage
block = 3
variable = fission_rate
direction = y
num_layers = 49
execute_on = timestep_begin
[]
[average_temp]
type = LayeredAverage
block = 3
variable = temp
direction = y
num_layers = 49
execute_on = timestep_begin
[]
[averagebu]
type = LayeredAverage
block = 3
variable = burnup
direction = y
num_layers = 49
execute_on = timestep_begin
[]
[casl_average_fission_rate]
variable = fission_rate
type = LayeredAverage
block = 3
direction = y
bounds = '0.01822 0.05688 0.13899 0.2211 0.30321 0.38533 0.46744 0.54955 0.63166 0.66976 0.75041 0.83106 0.91171 0.99236 1.07301 1.15366 1.19176 1.27241 1.35306 1.43371 1.51436 1.59501 1.67566 1.71376 1.79441 1.87506 1.95571 2.03636 2.11701 2.19766 2.23576 2.31641 2.39706 2.47771 2.55836 2.63901 2.71966 2.75776 2.83841 2.91906 2.99971 3.08036 3.16101 3.24166 3.27976 3.35897 3.43818 3.5174 3.59661 3.67582'
execute_on = timestep_begin
[]
[surface_temp]
type = LayeredSideAverage
boundary = 2
variable = temp
direction = y
bounds = '0.01822 0.05688 0.13899 0.2211 0.30321 0.38533 0.46744 0.54955 0.63166 0.66976 0.75041 0.83106 0.91171 0.99236 1.07301 1.15366 1.19176 1.27241 1.35306 1.43371 1.51436 1.59501 1.67566 1.71376 1.79441 1.87506 1.95571 2.03636 2.11701 2.19766 2.23576 2.31641 2.39706 2.47771 2.55836 2.63901 2.71966 2.75776 2.83841 2.91906 2.99971 3.08036 3.16101 3.24166 3.27976 3.35897 3.43818 3.5174 3.59661 3.67582'
use_displaced_mesh = 0
execute_on = timestep_begin
[]
[axial_temperature]
type = LayeredAverage
block = 3
variable = temp
direction = y
bounds = '0.01822 0.05688 0.13899 0.2211 0.30321 0.38533 0.46744 0.54955 0.63166 0.66976 0.75041 0.83106 0.91171 0.99236 1.07301 1.15366 1.19176 1.27241 1.35306 1.43371 1.51436 1.59501 1.67566 1.71376 1.79441 1.87506 1.95571 2.03636 2.11701 2.19766 2.23576 2.31641 2.39706 2.47771 2.55836 2.63901 2.71966 2.75776 2.83841 2.91906 2.99971 3.08036 3.16101 3.24166 3.27976 3.35897 3.43818 3.5174 3.59661 3.67582'
execute_on = timestep_begin
[]
[axial_burnup]
type = LayeredAverage
block = 3
variable = burnup
direction = y
bounds = '0.01822 0.05688 0.13899 0.2211 0.30321 0.38533 0.46744 0.54955 0.63166 0.66976 0.75041 0.83106 0.91171 0.99236 1.07301 1.15366 1.19176 1.27241 1.35306 1.43371 1.51436 1.59501 1.67566 1.71376 1.79441 1.87506 1.95571 2.03636 2.11701 2.19766 2.23576 2.31641 2.39706 2.47771 2.55836 2.63901 2.71966 2.75776 2.83841 2.91906 2.99971 3.08036 3.16101 3.24166 3.27976 3.35897 3.43818 3.5174 3.59661 3.67582'
execute_on = timestep_begin
[]
[integral_temperature]
type = LayeredAverage
block = 3
variable = temp
direction = y
num_layers = 1
execute_on = timestep_begin
[]
[integral_burnup]
type = LayeredAverage
block = 3
variable = burnup
direction = y
num_layers = 1
execute_on = timestep_begin
[]
[average]
type = LayeredAverage
block = 3
variable = temp
direction = y
bounds = '0.01822 0.05688 0.13899 0.2211 0.30321 0.38533 0.46744 0.54955 0.63166 0.66976 0.75041 0.83106 0.91171 0.99236 1.07301 1.15366 1.19176 1.27241 1.35306 1.43371 1.51436 1.59501 1.67566 1.71376 1.79441 1.87506 1.95571 2.03636 2.11701 2.19766 2.23576 2.31641 2.39706 2.47771 2.55836 2.63901 2.71966 2.75776 2.83841 2.91906 2.99971 3.08036 3.16101 3.24166 3.27976 3.35897 3.43818 3.5174 3.59661 3.67582'
execute_on = timestep_begin
[]
[axial_surface_temperature]
type = LayeredSideAverage
boundary = 2
variable = temp
direction = y
bounds = '0.01822 0.05688 0.13899 0.2211 0.30321 0.38533 0.46744 0.54955 0.63166 0.66976 0.75041 0.83106 0.91171 0.99236 1.07301 1.15366 1.19176 1.27241 1.35306 1.43371 1.51436 1.59501 1.67566 1.71376 1.79441 1.87506 1.95571 2.03636 2.11701 2.19766 2.23576 2.31641 2.39706 2.47771 2.55836 2.63901 2.71966 2.75776 2.83841 2.91906 2.99971 3.08036 3.16101 3.24166 3.27976 3.35897 3.43818 3.5174 3.59661 3.67582'
use_displaced_mesh = 0
execute_on = timestep_begin
[]
[rod_avg_fast_fluence]
type = LayeredSideAverage
boundary = 2
variable = fast_neutron_fluence
direction = y
num_layers = 1
use_displaced_mesh = 0
execute_on = timestep_begin
[]
[casl_clad_surface_heat_flux]
type = LayeredSideDiffusiveFluxAverage
variable = temp
boundary = 2
direction = y
bounds = '0.01822 0.05688 0.13899 0.2211 0.30321 0.38533 0.46744 0.54955 0.63166 0.66976 0.75041 0.83106 0.91171 0.99236 1.07301 1.15366 1.19176 1.27241 1.35306 1.43371 1.51436 1.59501 1.67566 1.71376 1.79441 1.87506 1.95571 2.03636 2.11701 2.19766 2.23576 2.31641 2.39706 2.47771 2.55836 2.63901 2.71966 2.75776 2.83841 2.91906 2.99971 3.08036 3.16101 3.24166 3.27976 3.35897 3.43818 3.5174 3.59661 3.67582'
diffusivity = thermal_conductivity
execute_on = timestep_begin
[]
[]
[Dampers]
[BoundingValueNodalDamper]
type = BoundingValueNodalDamper
variable = temp
max_value = 3200
min_value = 293
[]
[]
# ==================================================== #
# Solver Options
# ==================================================== #
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package -ksp_gmres_restart'
petsc_options_value = 'lu superlu_dist 51'
verbose = true
line_search = 'none'
# controls for linear iterations
l_max_its = 100
l_tol = 8e-3
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-6
nl_abs_tol = 1e-10
# ================================================== #
# Time Step Control
# ================================================== #
start_time = -100
end_time = 5e6
dtmin = 0.1
dtmax = 1e6
dt = 10
[TimeStepper]
type = IterationAdaptiveDT
dt = 1.0e2
optimal_iterations = 1000
time_t = '0 1.0e4 53200 1.0e5'
time_dt = '1.0e3 1.0e3 1.0e3 1.0e5'
[]
[]
[Postprocessors]
# ================================================== #
# Required for Fission Gas Release Models
# ================================================== #
[ave_temp_interior]
# used to compute temperature of plenum
type = SideAverageValue
boundary = 9
variable = temp
outputs = exodus
execute_on = 'initial linear'
[]
[fission_gas_released]
type = ElementIntegralFisGasReleasedSifgrs
block = 3
outputs = exodus
execute_on = linear
[]
[gas_volume]
type = InternalVolume
boundary = 9
outputs = exodus
execute_on = 'initial linear'
[]
[fis_gas_grain]
type = ElementIntegralFisGasGrainSifgrs
block = 3
outputs = exodus
execute_on = linear
[]
[fis_gas_boundary]
type = ElementIntegralFisGasBoundarySifgrs
block = 3
outputs = exodus
execute_on = linear
[]
[_dt]
type = TimestepSize
execute_on = timestep_end
[]
[num_lin_it]
type = NumLinearIterations
[]
[num_nonlin_it]
type = NumNonlinearIterations
[]
[tot_lin_it]
type = CumulativeValuePostprocessor
postprocessor = num_lin_it
[]
[tot_nonlin_it]
type = CumulativeValuePostprocessor
postprocessor = num_nonlin_it
[]
[alive_time]
type = PerfGraphData
section_name = Root
data_type = TOTAL
[]
[]
# ==================================================== #
# Location and format of output
# ==================================================== #
[Outputs]
perf_graph = true
exodus = true
file_base = pin2_output
time_step_interval = 1
[console]
type = Console
max_rows = 25
output_linear = true
[]
[]
(assessment/LWR/validation/RIA_CABRI_REP_Na/analysis/REP_Na_5/REP_Na_5_RIA.i)
# REP Na 5 Rodlet RIA
[GlobalParams]
density = 10476.35 # assumed TD = 10970
displacements = 'disp_x disp_y'
temperature = temp
order = SECOND
family = LAGRANGE
energy_per_fission = 3.2e-11
volumetric_locking_correction = false
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
acceptable_iterations = 30
acceptable_multiplier = 10
restart_file_base = 'recover_files_cp/LATEST'
[]
[Mesh]
coord_type = RZ
[smeared_pellet_mesh]
type = FuelPinMeshGenerator
clad_mesh_density = customize
pellet_mesh_density = customize
nx_p = 11
ny_p = 164
ny_cu = 3
ny_c = 170
ny_cl = 3
nx_c = 4
clad_thickness = 0.00057825
pellet_outer_radius = 0.0040959
pellet_quantity = 41
pellet_height = 0.0137414
clad_top_gap_height = 0.04081553
clad_bot_gap_height = 0.003
clad_gap_width = 82.0e-6
bottom_clad_height = 0.0015
top_clad_height = 0.0015
elem_type = QUAD8
[]
patch_size = 40
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temp]
[]
[]
[AuxVariables]
[fast_neutron_flux]
block = 1
[]
[fast_neutron_fluence]
block = 1
[]
[grain_radius]
block = 3
[]
[gap_cond]
order = CONSTANT
family = MONOMIAL
[]
[fuel_cond]
order = CONSTANT
family = MONOMIAL
[]
[swelling_strain]
order = CONSTANT
family = MONOMIAL
block = 3
[]
[total_hoop_strain]
order = CONSTANT
family = MONOMIAL
[]
[total_axial_strain]
order = CONSTANT
family = MONOMIAL
[]
[clad_coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[coolant_temp]
order = CONSTANT
family = MONOMIAL
[]
[clad_coolant_flux]
order = CONSTANT
family = MONOMIAL
[]
[coolant_channel_hmode]
order = CONSTANT
family = MONOMIAL
[]
[coolant_channel_htype]
order = CONSTANT
family = MONOMIAL
[]
[critical_heat_flux]
order = CONSTANT
family = MONOMIAL
[]
[oxide_thickness]
order = CONSTANT
family = MONOMIAL
[]
[SED]
order = CONSTANT
family = MONOMIAL
block = 1
[]
[oxywtfract_total]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfgain_total]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[]
[Functions]
[power_profile]
type = PiecewiseLinear
data_file = REPNa5_power_history_Full.csv
format = columns
[]
[axial_peaking_factors]
type = PiecewiseBilinear
data_file = REPNa5_axial_peaking_Full.csv
axis = 1
[]
[pressure_ramp]
type = PiecewiseLinear
xy_data = '0 101325
8640 15499970
124675200 15499970
124718400 101325
125193600 101325
125193610 101325
125193650 500008
125193700 500008
125193900 500008
125194000 101325
125194100 101325'
[]
[temp_ramp]
type = PiecewiseLinear
xy_data = '0 293.15
8640 560.15
124675200 560.15
124761600 293.15
125193600 293.15
125193610 293.15
125193650 553.15
125193700 553.15
125193900 553.15
125194000 293.15
125194100 293.15'
[]
[Fuel_CTE_function] #Fuel CTE as a function of temp from MATPRO data
type = PiecewiseLinear
xy_data = ' 0 1.000E-05
300 1.000E-05
350 1.000E-05
400 1.000E-05
450 1.000E-05
500 1.001E-05
550 1.002E-05
600 1.003E-05
650 1.005E-05
700 1.008E-05
750 1.011E-05
800 1.015E-05
850 1.020E-05
900 1.026E-05
950 1.032E-05
1000 1.039E-05
1050 1.046E-05
1100 1.053E-05
1150 1.061E-05
1200 1.069E-05
1250 1.077E-05
1300 1.085E-05
1350 1.094E-05
1400 1.102E-05
1450 1.111E-05
1500 1.119E-05
1550 1.127E-05
1600 1.135E-05
1650 1.143E-05
1700 1.151E-05
1750 1.158E-05
1800 1.166E-05
1850 1.173E-05
1900 1.180E-05
1950 1.187E-05
2000 1.193E-05
2050 1.199E-05
2100 1.205E-05
2150 1.211E-05
2200 1.217E-05
2250 1.222E-05
2300 1.227E-05
2350 1.232E-05
2400 1.237E-05
2450 1.242E-05
2500 1.246E-05
2550 1.250E-05
2600 1.254E-05
2650 1.258E-05
2700 1.262E-05
2750 1.265E-05
2800 1.268E-05
2850 1.271E-05
2900 1.274E-05
2950 1.277E-05
3000 1.280E-05
3050 1.282E-05
3100 1.285E-05'
[]
[burnup_GWd]
type = ParsedFunction
expression = bu*950
symbol_names = 'bu'
symbol_values = 'average_burnup_EAV'
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[fuel]
block = 3
strain = FINITE
incremental = true
eigenstrain_names = 'fuel_relocation_eigenstrain fuel_thermal_eigenstrain
fuel_volumetric_swelling_eigenstrain'
extra_vector_tags = 'ref'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz'
[]
[clad]
block = 1
strain = FINITE
incremental = true
eigenstrain_names = 'clad_irradiation_growth_eigenstrain
clad_thermal_eigenstrain'
extra_vector_tags = 'ref'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz plastic_strain_xx plastic_strain_yy plastic_strain_zz
creep_strain_xx creep_strain_yy creep_strain_zz elastic_strain_xx
elastic_strain_yy elastic_strain_zz hoop_stress'
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temp
extra_vector_tags = 'ref'
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temp
extra_vector_tags = 'ref'
[]
[heat_source_fuel]
type = NeutronHeatSource
variable = temp
block = 3
burnup_function = burnup
extra_vector_tags = 'ref'
[]
[]
[Burnup]
[burnup]
block = 3
rod_ave_lin_pow = power_profile
axial_power_profile = axial_peaking_factors
num_radial = 80
num_axial = 42
a_upper = 0.5678974
a_lower = 0.0045
fuel_inner_radius = 0
fuel_outer_radius = 0.0040959
fuel_volume_ratio = 1
isotopes = 'U235 U238 Pu239 Pu240 Pu241 Pu242'
isotope_fractions = '0.0449 0.9551 0 0 0 0'
RPF = RPF
order = CONSTANT
family = MONOMIAL
[]
[]
[AuxKernels]
[fast_neutron_flux]
type = FastNeutronFluxAux
variable = fast_neutron_flux
block = 1
axial_power_profile = axial_peaking_factors
rod_ave_lin_pow = power_profile
factor = 3e13 #n/m2-s
execute_on = timestep_begin
[]
[fast_neutron_fluence]
type = FastNeutronFluenceAux
variable = fast_neutron_fluence
fast_neutron_flux = fast_neutron_flux
block = 1
execute_on = timestep_begin
[]
[grain_radius]
type = GrainRadiusAux
block = 3
variable = grain_radius
temperature = temp
execute_on = linear
[]
[gap_conductance]
type = MaterialRealAux
property = gap_conductance
variable = gap_cond
boundary = 10
[]
[fuel_conductance]
type = MaterialRealAux
property = thermal_conductivity
variable = fuel_cond
block = 3
[]
[swelling_strain]
type = MaterialRealAux
property = volumetric_swelling_strain
variable = swelling_strain
block = 3
[]
[total_hoop_strain]
type = RankTwoScalarAux
rank_two_tensor = total_strain
variable = total_hoop_strain
scalar_type = HoopStress
execute_on = timestep_end
block = 1
[]
[total_axial_strain]
type = RankTwoScalarAux
rank_two_tensor = total_strain
variable = total_axial_strain
scalar_type = AxialStress
execute_on = timestep_end
block = 1
[]
[clad_coolant_htc]
type = MaterialRealAux
property = coolant_channel_htc
variable = clad_coolant_htc
boundary = 2
[]
[coolant_temp]
type = MaterialRealAux
property = coolant_temperature
variable = coolant_temp
boundary = 2
[]
[clad_coolant_flux]
type = MaterialRealAux
property = output_heat_flux
variable = clad_coolant_flux
boundary = 2
[]
[coolant_channel_hmode]
type = MaterialRealAux
property = coolant_channel_hmode
variable = coolant_channel_hmode
boundary = 2
[]
[coolant_channel_htype]
type = MaterialRealAux
property = coolant_channel_htype
variable = coolant_channel_htype
boundary = 2
[]
[critical_heat_flux]
type = MaterialRealAux
property = critical_heat_flux
variable = critical_heat_flux
boundary = 2
[]
[oxide]
type = MaterialRealAux
property = oxide_scale_thickness
variable = oxide_thickness
boundary = 2
[]
[SED]
type = MaterialRealAux
variable = SED
property = strain_energy_density
execute_on = timestep_end
[]
[ofract_total]
type = MaterialRealAux
variable = oxywtfract_total
property = current_oxygen_weight_frac_total
execute_on = timestep_end
boundary = 2
[]
[ofgain_total]
type = MaterialRealAux
variable = oxywtfgain_total
property = oxygen_weight_frac_gained_total
execute_on = timestep_end
boundary = 2
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
block = 1
[]
[]
[Contact]
[pellet_clad_mechanical]
primary = 5
secondary = 10
penalty = 1e10
formulation = penalty
normalize_penalty = false
model = frictionless
normal_smoothing_distance = 0.1
[]
[]
[ThermalContact]
[thermal_contact]
type = GasGapHeatTransfer
variable = temp
primary = 5
secondary = 10
initial_moles = initial_moles
gas_released = fission_gas_released
jump_distance_model = LANNING
plenum_pressure = plenum_pressure
contact_pressure = contact_pressure
roughness_primary = 0.1e-6 #2.0e-6
roughness_secondary = 0.1e-6 #0.5e-6
roughness_coef = 3.2
normal_smoothing_distance = 0.1
quadrature = true
contact_coef = 20
emissivity_primary = 1
emissivity_secondary = 1
refab_time = 125107200
refab_gas_types = He
refab_fractions = 1
[]
[]
[BCs]
[no_x_all]
type = DirichletBC
variable = disp_x
boundary = 12
value = 0.0
[]
[no_y_clad_bottom]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[]
[no_y_fuel_bottom]
type = DirichletBC
variable = disp_y
boundary = 20
value = 0.0
[]
[Pressure]
[coolantPressure]
boundary = '1 2 3'
function = pressure_ramp
[]
[]
[PlenumPressure]
[plenumPressure]
boundary = 9
initial_temperature = 293.15
initial_pressure = 2.60e6
startup_time = 0
R = 8.3143
output_initial_moles = initial_moles
temperature = plenum_temperature
volume = plenum_volume
material_input = fission_gas_released
output = plenum_pressure
refab_time = 125107200
refab_pressure = 0.302e6
refab_temperature = 293.15
refab_volume = 2.4e-6
[]
[]
[]
[CoolantChannel]
[convective_clad_surface]
boundary = '1 2 3'
variable = temp
inlet_temperature = temp_ramp # K
inlet_pressure = pressure_ramp # Pa
inlet_massflux = 3533 # kg/m^2-sec Based on flow rate provided and flow area and estimated density of 885.1 kg/m^3
flow_area = 8.74855e-5 #m^2
heated_diameter = 1.172526e-2 #m
hydraulic_diameter = 4.7e-3 #m
heated_perimeter = 2.984513e-2 #m
coolant_material = 'sodium'
compute_enthalpy = true
heat_transfer_mode = 0
#oxide_thickness = oxide_thickness # coupled oxide_thickness
number_axial_zone = 50
rod_pitch = 1.26e-2 # m
rod_diameter = 0.0095 # m
[]
[]
[Materials]
[swelling]
type = UO2VolumetricSwellingEigenstrain
block = 3
burnup_function = burnup
initial_fuel_density = 10476.35
include_solid_swelling = true
include_densification = true
total_densification = 0.00675
initial_porosity = 0.045
eigenstrain_name = 'fuel_volumetric_swelling_eigenstrain'
[]
[fuel_thermal]
type = UO2Thermal
block = 3
thermal_conductivity_model = NFIR
temperature = temp
burnup_function = burnup
initial_porosity = 0.045
[]
[fuel_elastic_stress]
type = ComputeFiniteStrainElasticStress
block = 3
[]
[fuel_elasticity_tensor]
type = UO2ElasticityTensor
block = 3
[]
[fuel_thermal_expansion]
type = ComputeInstantaneousThermalExpansionFunctionEigenstrain
block = 3
stress_free_temperature = 293.15
thermal_expansion_function = Fuel_CTE_function
eigenstrain_name = 'fuel_thermal_eigenstrain'
[]
[fuel_relocation]
type = UO2RelocationEigenstrain
block = 3
burnup_function = burnup
diameter = 0.00819179 #Fuel pellet diameter in m
rod_ave_lin_pow = power_profile
axial_power_profile = axial_peaking_factors
diametral_gap =164.0e-6
burnup_relocation_stop = 0.0
relocation_activation1 = 5000
eigenstrain_name = 'fuel_relocation_eigenstrain'
[]
[clad_thermal]
type = ZryThermal
block = 1
temperature = temp
[]
[clad_zrycreep]
type = ZryCreepLimbackHoppeUpdate
block = 1
fast_neutron_flux = fast_neutron_flux
fast_neutron_fluence = fast_neutron_fluence
zircaloy_material_type = stress_relief_annealed
max_inelastic_increment = 1.0e-4
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = 1
fast_neutron_fluence = fast_neutron_fluence
cold_work_factor = 0.5
oxygen_concentration = 0.0
matpro_poissons_ratio = true
matpro_youngs_modulus = true
[]
[clad_inelastic_stress]
type = ComputeMultipleInelasticStress
block = 1
tangent_operator = elastic
inelastic_models = 'plasticity' #only use plasticity
[]
[clad_thermal_eigenstrain]
type = ZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 293.15
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[clad_irradiation_eigenstrain]
type = ZryIrradiationGrowthEigenstrain
block = 1
fast_neutron_fluence = fast_neutron_fluence
zircaloy_material_type = stress_relief_annealed
eigenstrain_name = 'clad_irradiation_growth_eigenstrain'
[]
[plasticity]
type = ZryPlasticityUpdate
block = 1
cold_work_factor = 0.5
fast_neutron_fluence = fast_neutron_fluence
fast_neutron_flux = fast_neutron_flux
plasticity_model_type = MATPRO
oxygen_concentration = 0.0
max_inelastic_increment = 1.0e-4
[]
[density_clad]
type = Density
block = 1
density = 6550
[]
[density_fuel]
type = Density
block = 3
[]
[fission_gas_release]
type = UO2Sifgrs
block = 3
temperature = temp
burnup_function = burnup
initial_porosity = 0.045
grain_radius_const = 5.0e-6
gbs_model = false
transient_option = MICROCRACKING_BURNUP
[]
[ZryOxidation]
type = ZryOxidation
boundary = 2
clad_inner_radius = 0.0041178
clad_outer_radius = 0.0047549
use_coolant_channel = true
fast_neutron_flux = fast_neutron_flux
[]
[phase]
type = ZrPhase
block = 1
numerical_method = 2
[]
[strain_energy_density]
type = StrainEnergyDensity
incremental = true
[]
[]
[Dampers]
[BoundingValueNodalDamper]
type = BoundingValueNodalDamper
max_value = 3200
min_value = 200
variable = temp
[]
[contact_slip]
type = ContactSlipDamper
primary = 5
secondary = 10
min_damping_factor = 0.05
[]
[]
[Preconditioning]
[SMP]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-3
nl_max_its = 40
nl_rel_tol = 1e-4
nl_abs_tol = 1e-10
#start_time = 0
end_time = 125194100
dtmax = 10
dtmin = 1e-7
[TimeStepper]
type = IterationAdaptiveDT
dt = 10
optimal_iterations = 20
iteration_window = 4
linear_iteration_ratio = 100
timestep_limiting_function = power_profile
max_function_change = 1e5
force_step_every_function_point = true
timestep_limiting_postprocessor = material_timestep_control
time_t = '125193610 125193620 125193630 125193640 125193650 125193660 125193670 125193680'
time_dt = '10 10 10 10 10 10 10 10'
[]
[Quadrature]
order = FIFTH
side_order = SEVENTH
[]
[]
[Postprocessors]
[fis_gas_grain]
type = ElementIntegralFisGasGrainSifgrs
block = 3
outputs = exodus
[]
[fis_gas_boundary]
type = ElementIntegralFisGasBoundarySifgrs
block = 3
outputs = exodus
[]
[rod_input_power]
type = FunctionValuePostprocessor
function = power_profile
[]
[average_burnup_EAV]
type = ElementAverageValue
block = 3
variable = burnup
[]
[burnup_GWd]
type = FunctionValuePostprocessor
function = burnup_GWd
[]
#######################################
[penetration]
type = NodalVariableValue
variable = penetration
nodeid = 5780
use_displaced_mesh = 1
[]
[contact_pressure]
type = NodalVariableValue
variable = contact_pressure
nodeid = 5780
use_displaced_mesh = 1
[]
[gap_cond]
type = ElementalVariableValue
variable = gap_cond
elementid = 1737
use_displaced_mesh = 1
[]
[creep_hoop_strain]
type = ElementalVariableValue
variable = creep_strain_zz
elementid = 388
use_displaced_mesh = 1
[]
[elastic_hoop_strain]
type = ElementalVariableValue
variable = elastic_strain_zz
elementid = 388
use_displaced_mesh = 1
[]
[plastic_hoop_strain]
type = ElementalVariableValue
variable = plastic_strain_zz
elementid = 388
use_displaced_mesh = 1
[]
[total_hoop_strain]
type = ElementalVariableValue
variable = total_hoop_strain
elementid = 388
use_displaced_mesh = 1
[]
[clad_hoop_stress]
type = ElementalVariableValue
variable = hoop_stress
elementid = 388
use_displaced_mesh = 1
[]
[clad_axial_elongation]
type = NodalVariableValue
variable = disp_y
nodeid = 2591
use_displaced_mesh = 1
[]
[clad_oxide_thickness]
type = ElementalVariableValue
variable = oxide_thickness
elementid = 388
use_displaced_mesh = 1
[]
[clad_coolant_htc]
type = ElementalVariableValue
variable = clad_coolant_htc
elementid = 388
use_displaced_mesh = 1
[]
[coolant_temp]
type = ElementalVariableValue
variable = coolant_temp
elementid = 388
use_displaced_mesh = 1
[]
[fuel_centerline_temp]
type = NodalVariableValue
variable = temp
nodeid = 5749
[]
[fuel_surface_temp]
type = NodalVariableValue
variable = temp
nodeid = 5780
[]
[clad_inner_surface_temp]
type = NodalVariableValue
variable = temp
nodeid = 1349
[]
[clad_outer_surface_temp]
type = NodalVariableValue
variable = temp
nodeid = 1359
[]
[fuel_axial_elongation]
type = NodalVariableValue
variable = disp_y
nodeid = 8475
[]
[clad_radial_elongation]
type = NodalVariableValue
variable = disp_x
nodeid = 1359
[]
[fuel_radial_elongation]
type = NodalVariableValue
variable = disp_x
nodeid = 5780
[]
[SED_PPN_O]
type = ElementalVariableValue
variable = SED
elementid = 388
use_displaced_mesh = 1
[]
[SED_PPN_I]
type = ElementalVariableValue
variable = SED
elementid = 385
use_displaced_mesh = 1
[]
[OFract_PPN_O]
type = ElementalVariableValue
variable = oxywtfract_total
elementid = 388
use_displaced_mesh = 1
[]
[OGain_PPN_O]
type = ElementalVariableValue
variable = oxywtfgain_total
elementid = 388
use_displaced_mesh = 1
[]
#######################################
[max_fuel_temp]
type = NodalExtremeValue
block = 3
variable = temp
[]
[max_clad_temp]
type = NodalExtremeValue
block = clad
variable = temp
[]
[max_clad_SED]
type = ElementExtremeValue
block = clad
variable = SED
value_type = max
[]
[RAE]
type = RadialAverageEnthalpy
vector_postprocessor = rad_temp
radial_direction = x
axial_direction = y
axial_position = 0.3
temperature_name = temp
[]
[material_timestep_control]
type = MaterialTimeStepPostprocessor
block = 1
[]
[peak_RAE]
type = TimeExtremeValue
postprocessor = RAE
[]
[]
[VectorPostprocessors]
[ox_thick]
type = SideValueSampler
variable = oxide_thickness
boundary = 2
sort_by = y
outputs = 'outfile_oxide_thickness'
[]
[rad_temp]
type = NodalValueSampler
block = 3
sort_by = y
variable = temp
execute_on = timestep_end
outputs = 'outfile_radial_temp'
[]
[]
[StandardLWRFuelRodOutputs]
fuel_pellet_blocks = 3
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
csv = true
color = true
[outfile_oxide_thickness]
type = CSV
sync_times = '125193600 125194100'
sync_only = true
[]
[outfile_radial_temp]
type = CSV
enable = false
[]
[console]
type = Console
output_linear = true
max_rows = 10
[]
[chkfile]
type = CSV
show = 'plenum_temperature fission_gas_released_percentage
average_centerline_fuel_temperature average_burnup peak_RAE'
execute_on = 'FINAL'
[]
[exodus]
type = Exodus
time_step_interval = 4
end_time = 125193700
[]
[exodus_RIA]
type = Exodus
time_step_interval = 2
start_time = 125193695
[]
[]
(assessment/LWR/validation/RIA_CABRI_REP_Na/analysis/REP_Na_5/REP_Na_5.i)
# REP Na 5 Rodlet Base Irradiation
[GlobalParams]
density = 10476.35 # assumed TD = 10970
displacements = 'disp_x disp_y'
temperature = temp
order = SECOND
family = LAGRANGE
energy_per_fission = 3.2e-11
volumetric_locking_correction = false
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
acceptable_iterations = 30
acceptable_multiplier = 10
[]
[Mesh]
coord_type = RZ
[smeared_pellet_mesh]
type = FuelPinMeshGenerator
clad_mesh_density = customize
pellet_mesh_density = customize
nx_p = 11
ny_p = 164
ny_cu = 3
ny_c = 170
ny_cl = 3
nx_c = 4
clad_thickness = 0.00057825
pellet_outer_radius = 0.0040959
pellet_quantity = 41
pellet_height = 0.0137414
clad_top_gap_height = 0.04081553
clad_bot_gap_height = 0.003
clad_gap_width = 82.0e-6
bottom_clad_height = 0.0015
top_clad_height = 0.0015
elem_type = QUAD8
[]
patch_size = 40
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temp]
initial_condition = 293.15
[]
[]
[AuxVariables]
[fast_neutron_flux]
block = 1
[]
[fast_neutron_fluence]
block = 1
[]
[grain_radius]
block = 3
initial_condition = 5.0e-6 # Assume Grain size 10 microns
[]
[gap_cond]
order = CONSTANT
family = MONOMIAL
[]
[fuel_cond]
order = CONSTANT
family = MONOMIAL
[]
[swelling_strain]
order = CONSTANT
family = MONOMIAL
block = 3
[]
[total_hoop_strain]
order = CONSTANT
family = MONOMIAL
[]
[total_axial_strain]
order = CONSTANT
family = MONOMIAL
[]
[clad_coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[coolant_temp]
order = CONSTANT
family = MONOMIAL
[]
[clad_coolant_flux]
order = CONSTANT
family = MONOMIAL
[]
[coolant_channel_hmode]
order = CONSTANT
family = MONOMIAL
[]
[coolant_channel_htype]
order = CONSTANT
family = MONOMIAL
[]
[critical_heat_flux]
order = CONSTANT
family = MONOMIAL
[]
[oxide_thickness]
order = CONSTANT
family = MONOMIAL
[]
[SED]
order = CONSTANT
family = MONOMIAL
block = 1
[]
[oxywtfract_total]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfgain_total]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[]
[Functions]
[power_profile]
type = PiecewiseLinear
data_file = REPNa5_power_history_Full.csv
format = columns
[]
[axial_peaking_factors]
type = PiecewiseBilinear
data_file = REPNa5_axial_peaking_Full.csv
axis = 1
[]
[pressure_ramp]
type = PiecewiseLinear
xy_data = '0 101325
8640 15499970
124675200 15499970
124718400 101325
125193600 101325
125193610 101325
125193650 500008
125193700 500008
125193900 500008
125194000 101325
125194100 101325'
[]
[temp_ramp]
type = PiecewiseLinear
xy_data = '0 293.15
8640 560.15
124675200 560.15
124761600 293.15
125193600 293.15
125193610 293.15
125193650 553.15
125193700 553.15
125193900 553.15
125194000 293.15
125194100 293.15'
[]
[Fuel_CTE_function] #Fuel CTE as a function of temp from MATPRO data
type = PiecewiseLinear
xy_data = ' 0 1.000E-05
300 1.000E-05
350 1.000E-05
400 1.000E-05
450 1.000E-05
500 1.001E-05
550 1.002E-05
600 1.003E-05
650 1.005E-05
700 1.008E-05
750 1.011E-05
800 1.015E-05
850 1.020E-05
900 1.026E-05
950 1.032E-05
1000 1.039E-05
1050 1.046E-05
1100 1.053E-05
1150 1.061E-05
1200 1.069E-05
1250 1.077E-05
1300 1.085E-05
1350 1.094E-05
1400 1.102E-05
1450 1.111E-05
1500 1.119E-05
1550 1.127E-05
1600 1.135E-05
1650 1.143E-05
1700 1.151E-05
1750 1.158E-05
1800 1.166E-05
1850 1.173E-05
1900 1.180E-05
1950 1.187E-05
2000 1.193E-05
2050 1.199E-05
2100 1.205E-05
2150 1.211E-05
2200 1.217E-05
2250 1.222E-05
2300 1.227E-05
2350 1.232E-05
2400 1.237E-05
2450 1.242E-05
2500 1.246E-05
2550 1.250E-05
2600 1.254E-05
2650 1.258E-05
2700 1.262E-05
2750 1.265E-05
2800 1.268E-05
2850 1.271E-05
2900 1.274E-05
2950 1.277E-05
3000 1.280E-05
3050 1.282E-05
3100 1.285E-05'
[]
[burnup_GWd]
type = ParsedFunction
expression = bu*950
symbol_names = 'bu'
symbol_values = 'average_burnup'
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[fuel]
block = 3
strain = FINITE
incremental = true
eigenstrain_names = 'fuel_relocation_eigenstrain fuel_thermal_eigenstrain
fuel_volumetric_swelling_eigenstrain'
extra_vector_tags = 'ref'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz'
[]
[clad]
block = 1
strain = FINITE
incremental = true
eigenstrain_names = 'clad_irradiation_growth_eigenstrain
clad_thermal_eigenstrain'
extra_vector_tags = 'ref'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz plastic_strain_xx plastic_strain_yy plastic_strain_zz
creep_strain_xx creep_strain_yy creep_strain_zz elastic_strain_xx
elastic_strain_yy elastic_strain_zz hoop_stress'
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temp
extra_vector_tags = 'ref'
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temp
extra_vector_tags = 'ref'
[]
[heat_source_fuel]
type = NeutronHeatSource
variable = temp
block = 3
burnup_function = burnup
extra_vector_tags = 'ref'
[]
[]
[Burnup]
[burnup]
block = 3
rod_ave_lin_pow = power_profile
axial_power_profile = axial_peaking_factors
num_radial = 80
num_axial = 42
a_upper = 0.5678974
a_lower = 0.0045
fuel_inner_radius = 0
fuel_outer_radius = 0.0040959
fuel_volume_ratio = 1
isotopes = 'U235 U238 Pu239 Pu240 Pu241 Pu242'
isotope_fractions = '0.0449 0.9551 0 0 0 0'
RPF = RPF
order = CONSTANT
family = MONOMIAL
[]
[]
[AuxKernels]
[fast_neutron_flux]
type = FastNeutronFluxAux
variable = fast_neutron_flux
block = 1
axial_power_profile = axial_peaking_factors
rod_ave_lin_pow = power_profile
factor = 3e13 #n/m2-s
execute_on = timestep_begin
[]
[fast_neutron_fluence]
type = FastNeutronFluenceAux
variable = fast_neutron_fluence
fast_neutron_flux = fast_neutron_flux
block = 1
execute_on = timestep_begin
[]
[grain_radius]
type = GrainRadiusAux
block = 3
variable = grain_radius
temperature = temp
execute_on = linear
[]
[gap_conductance]
type = MaterialRealAux
property = gap_conductance
variable = gap_cond
boundary = 10
[]
[fuel_conductance]
type = MaterialRealAux
property = thermal_conductivity
variable = fuel_cond
block = 3
[]
[swelling_strain]
type = MaterialRealAux
property = volumetric_swelling_strain
variable = swelling_strain
block = 3
[]
[total_hoop_strain]
type = RankTwoScalarAux
rank_two_tensor = total_strain
variable = total_hoop_strain
scalar_type = HoopStress
execute_on = timestep_end
block = 1
[]
[total_axial_strain]
type = RankTwoScalarAux
rank_two_tensor = total_strain
variable = total_axial_strain
scalar_type = AxialStress
execute_on = timestep_end
block = 1
[]
[clad_coolant_htc]
type = MaterialRealAux
property = coolant_channel_htc
variable = clad_coolant_htc
boundary = 2
[]
[coolant_temp]
type = MaterialRealAux
property = coolant_temperature
variable = coolant_temp
boundary = 2
[]
[clad_coolant_flux]
type = MaterialRealAux
property = output_heat_flux
variable = clad_coolant_flux
boundary = 2
[]
[coolant_channel_hmode]
type = MaterialRealAux
property = coolant_channel_hmode
variable = coolant_channel_hmode
boundary = 2
[]
[coolant_channel_htype]
type = MaterialRealAux
property = coolant_channel_htype
variable = coolant_channel_htype
boundary = 2
[]
[critical_heat_flux]
type = MaterialRealAux
property = critical_heat_flux
variable = critical_heat_flux
boundary = 2
[]
[oxide]
type = MaterialRealAux
property = oxide_scale_thickness
variable = oxide_thickness
boundary = 2
[]
[SED]
type = MaterialRealAux
variable = SED
property = strain_energy_density
execute_on = timestep_end
[]
[ofract_total]
type = MaterialRealAux
variable = oxywtfract_total
property = current_oxygen_weight_frac_total
execute_on = timestep_end
boundary = 2
[]
[ofgain_total]
type = MaterialRealAux
variable = oxywtfgain_total
property = oxygen_weight_frac_gained_total
execute_on = timestep_end
boundary = 2
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
block = 1
[]
[]
[Contact]
[pellet_clad_mechanical]
primary = 5
secondary = 10
penalty = 1e10
formulation = penalty
normalize_penalty = false
model = frictionless
normal_smoothing_distance = 0.1
[]
[]
[ThermalContact]
[thermal_contact]
type = GasGapHeatTransfer
variable = temp
primary = 5
secondary = 10
initial_moles = initial_moles
gas_released = fission_gas_released
jump_distance_model = LANNING
plenum_pressure = plenum_pressure
contact_pressure = contact_pressure
roughness_primary = 2.0e-6
roughness_secondary = 0.5e-6
roughness_coef = 3.2
normal_smoothing_distance = 0.1
quadrature = true
emissivity_primary = 0.797698
emissivity_secondary = 0.325
refab_time = 125107200
refab_gas_types = He
refab_fractions = 1
[]
[]
[BCs]
[no_x_all]
type = DirichletBC
variable = disp_x
boundary = 12
value = 0.0
[]
[no_y_clad_bottom]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[]
[no_y_fuel_bottom]
type = DirichletBC
variable = disp_y
boundary = 20
value = 0.0
[]
[Pressure]
[coolantPressure]
boundary = '1 2 3'
function = pressure_ramp
[]
[]
[PlenumPressure]
[plenumPressure]
boundary = 9
initial_temperature = 293.15
initial_pressure = 2.60e6
startup_time = 0
R = 8.3143
output_initial_moles = initial_moles
temperature = plenum_temperature
volume = plenum_volume
material_input = fission_gas_released
output = plenum_pressure
refab_time = 125107200
refab_pressure = 0.302e6
refab_temperature = 293.15
refab_volume = 2.4e-6
[]
[]
[]
[CoolantChannel]
[convective_clad_surface]
boundary = '1 2 3'
variable = temp
inlet_temperature = temp_ramp # K
inlet_pressure = pressure_ramp # Pa
inlet_massflux = 3244.044104 # kg/m^2-sec
rod_diameter = 0.00951 # m
rod_pitch = 1.26e-2 # m
coolant_material = 'water'
compute_enthalpy = true
oxide_thickness = oxide_thickness
number_axial_zone = 50
[]
[]
[Materials]
[swelling]
type = UO2VolumetricSwellingEigenstrain
block = 3
burnup_function = burnup
initial_fuel_density = 10476.35
include_solid_swelling = true
include_densification = true
total_densification = 0.00675
initial_porosity = 0.045
eigenstrain_name = 'fuel_volumetric_swelling_eigenstrain'
[]
[fuel_thermal]
type = UO2Thermal
block = 3
thermal_conductivity_model = NFIR
temperature = temp
burnup_function = burnup
initial_porosity = 0.045
[]
[fuel_elastic_stress]
type = ComputeFiniteStrainElasticStress
block = 3
[]
[fuel_elasticity_tensor]
type = UO2ElasticityTensor
block = 3
[]
[fuel_thermal_expansion]
type = ComputeInstantaneousThermalExpansionFunctionEigenstrain
block = 3
stress_free_temperature = 293.15
thermal_expansion_function = Fuel_CTE_function
eigenstrain_name = 'fuel_thermal_eigenstrain'
[]
[fuel_relocation]
type = UO2RelocationEigenstrain
block = 3
burnup_function = burnup
diameter = 0.00819179 #Fuel pellet diameter in m
rod_ave_lin_pow = power_profile
axial_power_profile = axial_peaking_factors
diametral_gap =164.0e-6
burnup_relocation_stop = 0.0223
relocation_activation1 = 5000
eigenstrain_name = 'fuel_relocation_eigenstrain'
[]
[clad_thermal]
type = ZryThermal
block = 1
temperature = temp
[]
[clad_zrycreep]
type = ZryCreepLimbackHoppeUpdate
block = 1
fast_neutron_flux = fast_neutron_flux
fast_neutron_fluence = fast_neutron_fluence
zircaloy_material_type = stress_relief_annealed
max_inelastic_increment = 1.0e-4
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = 1
fast_neutron_fluence = fast_neutron_fluence
cold_work_factor = 0.5
oxygen_concentration = 0.0
matpro_poissons_ratio = false
matpro_youngs_modulus = true
[]
[clad_inelastic_stress]
type = ComputeMultipleInelasticStress
block = 1
tangent_operator = elastic
inelastic_models = 'clad_zrycreep plasticity'
[]
[clad_thermal_eigenstrain] # thermoelasticity, plasticity, and thermal and irradiation creep for Zr4
type = ZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 293.15
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[clad_irradiation_eigenstrain]
type = ZryIrradiationGrowthEigenstrain
block = 1
fast_neutron_fluence = fast_neutron_fluence
zircaloy_material_type = stress_relief_annealed
eigenstrain_name = 'clad_irradiation_growth_eigenstrain'
[]
[plasticity]
type = ZryPlasticityUpdate
block = 1
cold_work_factor = 0.5
fast_neutron_fluence = fast_neutron_fluence
fast_neutron_flux = fast_neutron_flux
plasticity_model_type = MATPRO
oxygen_concentration = 0.0
max_inelastic_increment = 1.0e-4
[]
[density_clad]
type = Density
block = 1
density = 6550
[]
[density_fuel]
type = Density
block = 3
[]
[fission_gas_release]
type = UO2Sifgrs
block = 3
temperature = temp
burnup_function = burnup
initial_porosity = 0.045
grain_radius = grain_radius
gbs_model = true
transient_option = NO_TRANSIENT
[]
[ZryOxidation]
type = ZryOxidation
boundary = 2
clad_inner_radius = 0.0041178
clad_outer_radius = 0.0047549
use_coolant_channel = true
fast_neutron_flux = fast_neutron_flux
[]
[phase]
type = ZrPhase
block = 1
numerical_method = 2
[]
[strain_energy_density]
type = StrainEnergyDensity
incremental = true
[]
[]
[Dampers]
[BoundingValueNodalDamper]
type = BoundingValueNodalDamper
max_value = 3200
min_value = 200
variable = temp
[]
[contact_slip]
type = ContactSlipDamper
primary = 5
secondary = 10
min_damping_factor = 0.05
[]
[]
[Preconditioning]
[SMP]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-3
nl_max_its = 40
nl_rel_tol = 1e-4
nl_abs_tol = 1e-10
start_time = 0
end_time = 125193600
dtmax = 1e6
dtmin = 1e-7
[TimeStepper]
type = IterationAdaptiveDT
dt = 1.0e3
optimal_iterations = 100
iteration_window = 4
linear_iteration_ratio = 100
timestep_limiting_function = power_profile
max_function_change = 1e6
force_step_every_function_point = true
timestep_limiting_postprocessor = material_timestep_control
time_t = '125193610 125193620 125193630 125193640 125193650 125193660 125193670 125193680'
time_dt = '10 10 10 10 10 10 10 10'
[]
[Quadrature]
order = FIFTH
side_order = SEVENTH
[]
[]
[Postprocessors]
[fis_gas_grain]
type = ElementIntegralFisGasGrainSifgrs
block = 3
outputs = exodus
[]
[fis_gas_boundary]
type = ElementIntegralFisGasBoundarySifgrs
block = 3
outputs = exodus
[]
[rod_input_power]
type = FunctionValuePostprocessor
function = power_profile
[]
[burnup_GWd]
type = FunctionValuePostprocessor
function = burnup_GWd
[]
#######################################
[penetration]
type = NodalVariableValue
variable = penetration
nodeid = 5780
use_displaced_mesh = 1
[]
[contact_pressure]
type = NodalVariableValue
variable = contact_pressure
nodeid = 5780
use_displaced_mesh = 1
[]
[gap_cond]
type = ElementalVariableValue
variable = gap_cond
elementid = 1737
use_displaced_mesh = 1
[]
[creep_hoop_strain]
type = ElementalVariableValue
variable = creep_strain_zz
elementid = 388
use_displaced_mesh = 1
[]
[elastic_hoop_strain]
type = ElementalVariableValue
variable = elastic_strain_zz
elementid = 388
use_displaced_mesh = 1
[]
[plastic_hoop_strain]
type = ElementalVariableValue
variable = plastic_strain_zz
elementid = 388
use_displaced_mesh = 1
[]
[total_hoop_strain]
type = ElementalVariableValue
variable = total_hoop_strain
elementid = 388
use_displaced_mesh = 1
[]
[clad_hoop_stress]
type = ElementalVariableValue
variable = hoop_stress
elementid = 388
use_displaced_mesh = 1
[]
[clad_axial_elongation]
type = NodalVariableValue
variable = disp_y
nodeid = 2591
use_displaced_mesh = 1
[]
[clad_oxide_thickness]
type = ElementalVariableValue
variable = oxide_thickness
elementid = 388
use_displaced_mesh = 1
[]
[clad_coolant_htc]
type = ElementalVariableValue
variable = clad_coolant_htc
elementid = 388
use_displaced_mesh = 1
[]
[coolant_temp]
type = ElementalVariableValue
variable = coolant_temp
elementid = 388
use_displaced_mesh = 1
[]
[fuel_centerline_temp]
type = NodalVariableValue
variable = temp
nodeid = 5749
[]
[fuel_surface_temp]
type = NodalVariableValue
variable = temp
nodeid = 5780
[]
[clad_inner_surface_temp]
type = NodalVariableValue
variable = temp
nodeid = 1349
[]
[clad_outer_surface_temp]
type = NodalVariableValue
variable = temp
nodeid = 1359
[]
[fuel_axial_elongation]
type = NodalVariableValue
variable = disp_y
nodeid = 8475
[]
[clad_radial_elongation]
type = NodalVariableValue
variable = disp_x
nodeid = 1359
[]
[fuel_radial_elongation]
type = NodalVariableValue
variable = disp_x
nodeid = 5780
[]
[SED_PPN_O]
type = ElementalVariableValue
variable = SED
elementid = 388
use_displaced_mesh = 1
[]
[SED_PPN_I]
type = ElementalVariableValue
variable = SED
elementid = 385
use_displaced_mesh = 1
[]
[OFract_PPN_O]
type = ElementalVariableValue
variable = oxywtfract_total
elementid = 388
use_displaced_mesh = 1
[]
[OGain_PPN_O]
type = ElementalVariableValue
variable = oxywtfgain_total
elementid = 388
use_displaced_mesh = 1
[]
#######################################
[max_fuel_temp]
type = NodalExtremeValue
block = 3
variable = temp
[]
[max_clad_temp]
type = NodalExtremeValue
block = clad
variable = temp
[]
[max_clad_SED]
type = ElementExtremeValue
block = clad
variable = SED
value_type = max
[]
[RAE]
type = RadialAverageEnthalpy
vector_postprocessor = rad_temp
radial_direction = x
axial_direction = y
axial_position = 0.3
temperature_name = temp
[]
[material_timestep_control]
type = MaterialTimeStepPostprocessor
block = 1
[]
[peak_RAE]
type = TimeExtremeValue
postprocessor = RAE
[]
[]
[VectorPostprocessors]
[ox_thick]
type = SideValueSampler
variable = oxide_thickness
boundary = 2
sort_by = y
outputs = 'outfile_oxide_thickness'
[]
[rad_temp]
type = NodalValueSampler
block = 3
sort_by = y
variable = temp
execute_on = timestep_end
outputs = 'outfile_radial_temp'
[]
[]
[StandardLWRFuelRodOutputs]
fuel_pellet_blocks = 3
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
csv = true
color = true
[outfile_oxide_thickness]
type = CSV
sync_times = '125193600 125194100'
sync_only = true
[]
[outfile_radial_temp]
type = CSV
enable = false
[]
[console]
type = Console
output_linear = true
max_rows = 10
[]
[checkpoint]
type = Checkpoint
num_files = 2
file_base = recover_files
sync_times = '125193600'
sync_only = true
[]
[chkfile]
type = CSV
show = 'plenum_temperature fission_gas_released_percentage
average_centerline_fuel_temperature average_burnup peak_RAE'
execute_on = 'FINAL'
[]
[exodus]
type = Exodus
time_step_interval = 4
end_time = 125193700
[]
[exodus_RIA]
type = Exodus
time_step_interval = 2
start_time = 125193695
[]
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-20/puzry-20_aniso.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-20.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 2500. '
y = '1.e+05 1.e+05 3.475e+06' # Linear increase at 0.0225 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 2500. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
# Circumferential steady-state creep test and analysis of Zircaloy-4 fuel cladding
# Nuclear Engineering and Design, 53, 2312-2322 (2021)
[F]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.738 0.738 0.57'
[]
[G]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.174 0.174 0.45'
[]
[H]
type = PiecewiseLinear
x = '293 1073 1400'
y = '0.588 0.588 0.48'
[]
[L]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[M]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[N]
type = PiecewiseLinear
x = '-1000 10000'
y = '1.0 1.0'
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = TaylorExpansion
use_automatic_differentiation = true
[]
[]
[]
[]
[Kernels]
[heat]
type = ADHeatConduction
variable = temperature
[]
[heat_ie]
type = ADHeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = ADMaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = ADMaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = ADMaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = ADMaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = ADMaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = ADFunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = ADDirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = ADDirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ADZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ADComputeIsotropicElasticityTensor
youngs_modulus = 1.e+11
poissons_ratio = 0.3
block = 1
[]
[hill_constants]
type = ADHillConstants
hill_constants = "0.738 0.174 0.588 1.0 1.0 1.0"
function_names = "F G H L M N"
temperature = temperature
[]
[creep_update]
type = ADZryAnisoCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 7.5e-05
temperature = temperature
temperature_standard_thermal_creep_end = 700
temperature_loca_creep_begin = 900.
fract_beta_phase_name = 'fract_beta_phase'
max_integration_error = 1000000.0
absolute_tolerance = 1e-07
relative_tolerance = 1e-07
[]
[creep]
type = ADComputeMultipleInelasticStress
block = 1
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ADZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = ADDensity
block = 1
[]
[phase]
type = ADZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ADZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = NEWTON
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0.
n_startup_steps = 1
end_time = 2500.
dtmax = 1.
dtmin = 1.0e-9
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-20_aniso_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/RIA_CABRI_REP_Na/analysis/REP_Na_3/REP_Na_3.i)
# REP Na 3 Rodlet Base Irradiation
[GlobalParams]
density = 10394.075 # assumed TD = 10970
displacements = 'disp_x disp_y'
temperature = temp
order = SECOND
family = LAGRANGE
energy_per_fission = 3.2e-11
volumetric_locking_correction = false
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
acceptable_iterations = 30
acceptable_multiplier = 10
[]
[Mesh]
coord_type = RZ
[smeared_pellet_mesh]
type = FuelPinMeshGenerator
clad_mesh_density = customize
pellet_mesh_density = customize
nx_p = 11
ny_p = 128
ny_cu = 3
ny_c = 130
ny_cl = 3
nx_c = 4
clad_thickness = 0.000596
pellet_outer_radius = 0.0040956
pellet_quantity = 32
pellet_height = 0.0135890
clad_top_gap_height = 0.0298168
clad_bot_gap_height = 0.003
clad_gap_width = 82.0e-6
bottom_clad_height = 0.0015
top_clad_height = 0.0015
elem_type = QUAD8
[]
patch_size = 40
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temp]
initial_condition = 293.15
[]
[]
[AuxVariables]
[fast_neutron_flux]
block = 1
[]
[fast_neutron_fluence]
block = 1
[]
[grain_radius]
block = 3
initial_condition = 5.0e-6
[]
[gap_cond]
order = CONSTANT
family = MONOMIAL
[]
[fuel_cond]
order = CONSTANT
family = MONOMIAL
[]
[swelling_strain]
order = CONSTANT
family = MONOMIAL
block = 3
[]
[total_hoop_strain]
order = CONSTANT
family = MONOMIAL
[]
[total_axial_strain]
order = CONSTANT
family = MONOMIAL
[]
[clad_coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[coolant_temp]
order = CONSTANT
family = MONOMIAL
[]
[clad_coolant_flux]
order = CONSTANT
family = MONOMIAL
[]
[coolant_channel_hmode]
order = CONSTANT
family = MONOMIAL
[]
[coolant_channel_htype]
order = CONSTANT
family = MONOMIAL
[]
[critical_heat_flux]
order = CONSTANT
family = MONOMIAL
[]
[oxide_thickness]
order = CONSTANT
family = MONOMIAL
[]
[SED]
order = CONSTANT
family = MONOMIAL
block = 1
[]
[oxywtfract_total]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfgain_total]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[]
[Functions]
[power_profile]
type = PiecewiseLinear
data_file = REPNa3_power_history_Full.csv
format = columns
[]
[axial_peaking_factors]
type = PiecewiseBilinear
data_file = REPNa3_axial_peaking_Full.csv
axis = 1
[]
[pressure_ramp]
type = PiecewiseLinear
xy_data = '0 101325
8640 15499970
17280 15499970
25920 15499970
34560 15499970
43200 15499970
51840 15499970
98798400 15499970
99273600 101325
99273610 101325
99273650 500008
99273700 500008
99273900 500008
99274000 101325
99274100 101325'
[]
[temp_ramp]
type = PiecewiseLinear
xy_data = '0 293.15
8640 583.15
17280 583.15
25920 583.15
34560 583.15
43200 583.15
51840 583.15
98798400 583.15
99273600 293.15
99273610 293.15
99273650 553.15
99273700 553.15
99273900 553.15
99274000 293.15
99274100 293.15'
[]
[Fuel_CTE_function] #Fuel CTE as a function of temp from MATPRO data
type = PiecewiseLinear
xy_data = ' 0 1.000E-05
300 1.000E-05
350 1.000E-05
400 1.000E-05
450 1.000E-05
500 1.001E-05
550 1.002E-05
600 1.003E-05
650 1.005E-05
700 1.008E-05
750 1.011E-05
800 1.015E-05
850 1.020E-05
900 1.026E-05
950 1.032E-05
1000 1.039E-05
1050 1.046E-05
1100 1.053E-05
1150 1.061E-05
1200 1.069E-05
1250 1.077E-05
1300 1.085E-05
1350 1.094E-05
1400 1.102E-05
1450 1.111E-05
1500 1.119E-05
1550 1.127E-05
1600 1.135E-05
1650 1.143E-05
1700 1.151E-05
1750 1.158E-05
1800 1.166E-05
1850 1.173E-05
1900 1.180E-05
1950 1.187E-05
2000 1.193E-05
2050 1.199E-05
2100 1.205E-05
2150 1.211E-05
2200 1.217E-05
2250 1.222E-05
2300 1.227E-05
2350 1.232E-05
2400 1.237E-05
2450 1.242E-05
2500 1.246E-05
2550 1.250E-05
2600 1.254E-05
2650 1.258E-05
2700 1.262E-05
2750 1.265E-05
2800 1.268E-05
2850 1.271E-05
2900 1.274E-05
2950 1.277E-05
3000 1.280E-05
3050 1.282E-05
3100 1.285E-05'
[]
[burnup_GWd]
type = ParsedFunction
expression = bu*950
symbol_names = 'bu'
symbol_values = 'average_burnup'
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[fuel]
block = 3
strain = FINITE
incremental = true
eigenstrain_names = 'fuel_relocation_eigenstrain fuel_thermal_eigenstrain
fuel_volumetric_swelling_eigenstrain'
extra_vector_tags = 'ref'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz'
[]
[clad]
block = 1
strain = FINITE
incremental = true
eigenstrain_names = 'clad_irradiation_growth_eigenstrain
clad_thermal_eigenstrain'
extra_vector_tags = 'ref'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz plastic_strain_xx plastic_strain_yy plastic_strain_zz
creep_strain_xx creep_strain_yy creep_strain_zz elastic_strain_xx
elastic_strain_yy elastic_strain_zz hoop_stress'
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temp
extra_vector_tags = 'ref'
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temp
extra_vector_tags = 'ref'
[]
[heat_source_fuel]
type = NeutronHeatSource
variable = temp
block = 3
burnup_function = burnup
extra_vector_tags = 'ref'
[]
[]
[Burnup]
[burnup]
block = 3
rod_ave_lin_pow = power_profile
axial_power_profile = axial_peaking_factors
num_radial = 80
num_axial = 33
a_upper = 0.4393480
a_lower = 0.0045
fuel_inner_radius = 0
fuel_outer_radius = 0.0040956
fuel_volume_ratio = 1
isotopes = 'U235 U238 Pu239 Pu240 Pu241 Pu242'
isotope_fractions = '0.045 0.955 0 0 0 0'
RPF = RPF
order = CONSTANT
family = MONOMIAL
[]
[]
[AuxKernels]
[fast_neutron_flux]
type = FastNeutronFluxAux
variable = fast_neutron_flux
block = 1
axial_power_profile = axial_peaking_factors
rod_ave_lin_pow = power_profile
factor = 3e13 #n/m2-s
execute_on = timestep_begin
[]
[fast_neutron_fluence]
type = FastNeutronFluenceAux
variable = fast_neutron_fluence
fast_neutron_flux = fast_neutron_flux
block = 1
execute_on = timestep_begin
[]
[grain_radius]
type = GrainRadiusAux
block = 3
variable = grain_radius
temperature = temp
execute_on = linear
[]
[gap_conductance]
type = MaterialRealAux
property = gap_conductance
variable = gap_cond
boundary = 10
[]
[fuel_conductance]
type = MaterialRealAux
property = thermal_conductivity
variable = fuel_cond
block = 3
[]
[swelling_strain]
type = MaterialRealAux
property = volumetric_swelling_strain
variable = swelling_strain
block = 3
[]
[total_hoop_strain]
type = RankTwoScalarAux
rank_two_tensor = total_strain
variable = total_hoop_strain
scalar_type = HoopStress
execute_on = timestep_end
block = 1
[]
[total_axial_strain]
type = RankTwoScalarAux
rank_two_tensor = total_strain
variable = total_axial_strain
scalar_type = AxialStress
execute_on = timestep_end
block = 1
[]
[clad_coolant_htc]
type = MaterialRealAux
property = coolant_channel_htc
variable = clad_coolant_htc
boundary = 2
[]
[coolant_temp]
type = MaterialRealAux
property = coolant_temperature
variable = coolant_temp
boundary = 2
[]
[clad_coolant_flux]
type = MaterialRealAux
property = output_heat_flux
variable = clad_coolant_flux
boundary = 2
[]
[coolant_channel_hmode]
type = MaterialRealAux
property = coolant_channel_hmode
variable = coolant_channel_hmode
boundary = 2
[]
[coolant_channel_htype]
type = MaterialRealAux
property = coolant_channel_htype
variable = coolant_channel_htype
boundary = 2
[]
[critical_heat_flux]
type = MaterialRealAux
property = critical_heat_flux
variable = critical_heat_flux
boundary = 2
[]
[oxide]
type = MaterialRealAux
property = oxide_scale_thickness
variable = oxide_thickness
boundary = 2
[]
[SED]
type = MaterialRealAux
variable = SED
property = strain_energy_density
execute_on = timestep_end
[]
[ofract_total]
type = MaterialRealAux
variable = oxywtfract_total
property = current_oxygen_weight_frac_total
execute_on = timestep_end
boundary = 2
[]
[ofgain_total]
type = MaterialRealAux
variable = oxywtfgain_total
property = oxygen_weight_frac_gained_total
execute_on = timestep_end
boundary = 2
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
block = 1
[]
[]
[Contact]
[pellet_clad_mechanical]
primary = 5
secondary = 10
penalty = 1e10
formulation = penalty
normalize_penalty = false
model = frictionless
normal_smoothing_distance = 0.1
[]
[]
[ThermalContact]
[thermal_contact]
type = GasGapHeatTransfer
variable = temp
primary = 5
secondary = 10
initial_moles = initial_moles
gas_released = fission_gas_released
jump_distance_model = LANNING
plenum_pressure = plenum_pressure
contact_pressure = contact_pressure
roughness_primary = 2.0e-6
roughness_secondary = 0.5e-6
roughness_coef = 3.2
normal_smoothing_distance = 0.1
quadrature = true
emissivity_primary = 0.797698
emissivity_secondary = 0.325
refab_time = 99187200
refab_gas_types = He
refab_fractions = 1
[]
[]
[BCs]
[no_x_all]
type = DirichletBC
variable = disp_x
boundary = 12
value = 0.0
[]
[no_y_clad_bottom]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[]
[no_y_fuel_bottom]
type = DirichletBC
variable = disp_y
boundary = 20
value = 0.0
[]
[Pressure]
[coolantPressure]
boundary = '1 2 3'
function = pressure_ramp
[]
[]
[PlenumPressure]
[plenumPressure]
boundary = 9
initial_temperature = 293.15
initial_pressure = 2.60e6
startup_time = 0
R = 8.3143
output_initial_moles = initial_moles
temperature = plenum_temperature
volume = plenum_volume
material_input = fission_gas_released
output = plenum_pressure
refab_time = 99187200
refab_pressure = 0.31e6
refab_temperature = 293.15
refab_volume = 2.0e-6
[]
[]
[]
[CoolantChannel]
[convective_clad_surface]
boundary = '1 2 3'
variable = temp
inlet_temperature = temp_ramp # K
inlet_pressure = pressure_ramp # Pa
inlet_massflux = 3244.044104 # kg/m^2-sec
rod_diameter = 0.0095 # m
rod_pitch = 1.26e-2 # m
coolant_material = 'water'
compute_enthalpy = true
oxide_thickness = oxide_thickness
number_axial_zone = 50
[]
[]
[Materials]
[swelling]
type = UO2VolumetricSwellingEigenstrain
block = 3
burnup_function = burnup
initial_fuel_density = 10394.075
include_solid_swelling = true
include_densification = true
total_densification = 0.00675
initial_porosity = 0.0525
eigenstrain_name = 'fuel_volumetric_swelling_eigenstrain'
[]
[fuel_thermal]
type = UO2Thermal
block = 3
thermal_conductivity_model = NFIR
temperature = temp
burnup_function = burnup
initial_porosity = 0.0525
[]
[fuel_elastic_stress]
type = ComputeFiniteStrainElasticStress
block = 3
[]
[fuel_elasticity_tensor]
type = UO2ElasticityTensor
block = 3
[]
[fuel_thermal_expansion]
type = ComputeInstantaneousThermalExpansionFunctionEigenstrain
block = 3
stress_free_temperature = 293.15
thermal_expansion_function = Fuel_CTE_function
eigenstrain_name = 'fuel_thermal_eigenstrain'
[]
[fuel_relocation]
type = UO2RelocationEigenstrain
block = 3
burnup_function = burnup
diameter = 0.0081912 #Fuel pellet diameter in m
rod_ave_lin_pow = power_profile
axial_power_profile = axial_peaking_factors
diametral_gap =164.0e-6
burnup_relocation_stop = 0.0242
relocation_activation1 = 5000
eigenstrain_name = 'fuel_relocation_eigenstrain'
[]
[clad_thermal]
type = ZryThermal
block = 1
temperature = temp
[]
[clad_zrycreep]
type = ZryCreepLimbackHoppeUpdate
block = 1
fast_neutron_flux = fast_neutron_flux
fast_neutron_fluence = fast_neutron_fluence
zircaloy_material_type = stress_relief_annealed
max_inelastic_increment = 1.0e-4
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = 1
fast_neutron_fluence = fast_neutron_fluence
cold_work_factor = 0.5
oxygen_concentration = 0.0
matpro_poissons_ratio = false
matpro_youngs_modulus = true
[]
[clad_inelastic_stress]
type = ComputeMultipleInelasticStress
block = 1
tangent_operator = elastic
inelastic_models = 'clad_zrycreep plasticity'
[]
[clad_thermal_eigenstrain]
type = ZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 293.15
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[clad_irradiation_eigenstrain]
type = ZryIrradiationGrowthEigenstrain
block = 1
fast_neutron_fluence = fast_neutron_fluence
zircaloy_material_type = stress_relief_annealed
eigenstrain_name = 'clad_irradiation_growth_eigenstrain'
[]
[plasticity]
type = ZryPlasticityUpdate
block = 1
cold_work_factor = 0.5
fast_neutron_fluence = fast_neutron_fluence
fast_neutron_flux = fast_neutron_flux
plasticity_model_type = MATPRO
oxygen_concentration = 0.0
max_inelastic_increment = 1.0e-4
[]
[density_clad]
type = Density
block = 1
density = 6550
[]
[density_fuel]
type = Density
block = 3
[]
[fission_gas_release]
type = UO2Sifgrs
block = 3
temperature = temp
burnup_function = burnup
initial_porosity = 0.0525
grain_radius = grain_radius
gbs_model = true
transient_option = NO_TRANSIENT
[]
[ZryOxidation]
type = ZryOxidation
boundary = 2
clad_inner_radius = 0.0041178
clad_outer_radius = 0.0047549
use_coolant_channel = true
fast_neutron_flux = fast_neutron_flux
[]
[phase]
type = ZrPhase
block = 1
numerical_method = 2
[]
[strain_energy_density]
type = StrainEnergyDensity
incremental = true
[]
[]
[Dampers]
[BoundingValueNodalDamper]
type = BoundingValueNodalDamper
max_value = 3200
min_value = 200
variable = temp
[]
[contact_slip]
type = ContactSlipDamper
primary = 5
secondary = 10
min_damping_factor = 0.05
[]
[]
[Preconditioning]
[SMP]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-3
nl_max_its = 40
nl_rel_tol = 1e-4
nl_abs_tol = 1e-10
start_time = 0
end_time = 99273600
dtmax = 1e6
dtmin = 1e-7
[TimeStepper]
type = IterationAdaptiveDT
dt = 1.0e3
optimal_iterations = 100
iteration_window = 4
linear_iteration_ratio = 100
timestep_limiting_function = power_profile
max_function_change = 1e6
force_step_every_function_point = true
timestep_limiting_postprocessor = material_timestep_control
time_t = '99273610 99273620 99273630 99273640 99273650 99273660 99273670 99273680'
time_dt = '10 10 10 10 10 10 10 10'
[]
[Quadrature]
order = FIFTH
side_order = SEVENTH
[]
[]
[Postprocessors]
[fis_gas_grain]
type = ElementIntegralFisGasGrainSifgrs
block = 3
outputs = exodus
[]
[fis_gas_boundary]
type = ElementIntegralFisGasBoundarySifgrs
block = 3
outputs = exodus
[]
[rod_input_power]
type = FunctionValuePostprocessor
function = power_profile
[]
[burnup_GWd]
type = FunctionValuePostprocessor
function = burnup_GWd
[]
#######################################
[penetration]
type = NodalVariableValue
variable = penetration
nodeid = 4415
use_displaced_mesh = 1
[]
[contact_pressure]
type = NodalVariableValue
variable = contact_pressure
nodeid = 4415
use_displaced_mesh = 1
[]
[gap_cond]
type = ElementalVariableValue
variable = gap_cond
elementid = 1324
use_displaced_mesh = 1
[]
[creep_hoop_strain]
type = ElementalVariableValue
variable = creep_strain_zz
elementid = 292
use_displaced_mesh = 1
[]
[elastic_hoop_strain]
type = ElementalVariableValue
variable = elastic_strain_zz
elementid = 292
use_displaced_mesh = 1
[]
[plastic_hoop_strain]
type = ElementalVariableValue
variable = plastic_strain_zz
elementid = 292
use_displaced_mesh = 1
[]
[total_hoop_strain]
type = ElementalVariableValue
variable = total_hoop_strain
elementid = 292
use_displaced_mesh = 1
[]
[clad_hoop_stress]
type = ElementalVariableValue
variable = hoop_stress
elementid = 292
use_displaced_mesh = 1
[]
[clad_axial_elongation]
type = NodalVariableValue
variable = disp_y
nodeid = 2031
use_displaced_mesh = 1
[]
[clad_oxide_thickness]
type = ElementalVariableValue
variable = oxide_thickness
elementid = 292
use_displaced_mesh = 1
[]
[clad_coolant_htc]
type = ElementalVariableValue
variable = clad_coolant_htc
elementid = 292
use_displaced_mesh = 1
[]
[coolant_temp]
type = ElementalVariableValue
variable = coolant_temp
elementid = 292
use_displaced_mesh = 1
[]
[fuel_centerline_temp]
type = NodalVariableValue
variable = temp
nodeid = 4384
[]
[fuel_surface_temp]
type = NodalVariableValue
variable = temp
nodeid = 4415
[]
[clad_inner_surface_temp]
type = NodalVariableValue
variable = temp
nodeid = 1027
[]
[clad_outer_surface_temp]
type = NodalVariableValue
variable = temp
nodeid = 1037
[]
[fuel_axial_elongation]
type = NodalVariableValue
variable = disp_y
nodeid = 6655
[]
[clad_radial_elongation]
type = NodalVariableValue
variable = disp_x
nodeid = 1037
[]
[fuel_radial_elongation]
type = NodalVariableValue
variable = disp_x
nodeid = 4415
[]
[SED_PPN_O]
type = ElementalVariableValue
variable = SED
elementid = 292
use_displaced_mesh = 1
[]
[SED_PPN_I]
type = ElementalVariableValue
variable = SED
elementid = 289
use_displaced_mesh = 1
[]
[OFract_PPN_O]
type = ElementalVariableValue
variable = oxywtfract_total
elementid = 292
use_displaced_mesh = 1
[]
[OGain_PPN_O]
type = ElementalVariableValue
variable = oxywtfgain_total
elementid = 292
use_displaced_mesh = 1
[]
#######################################
[max_fuel_temp]
type = NodalExtremeValue
block = 3
variable = temp
[]
[max_clad_temp]
type = NodalExtremeValue
block = 1
variable = temp
[]
[max_clad_SED]
type = ElementExtremeValue
block = 1
variable = SED
value_type = max
[]
[RAE]
type = RadialAverageEnthalpy
vector_postprocessor = rad_temp
radial_direction = x
axial_direction = y
axial_position = 0.22
temperature_name = temp
[]
[material_timestep_control]
type = MaterialTimeStepPostprocessor
block = 1
[]
[peak_RAE]
type = TimeExtremeValue
postprocessor = RAE
[]
[]
[VectorPostprocessors]
[ox_thick]
type = SideValueSampler
variable = oxide_thickness
boundary = 2
sort_by = y
outputs = 'outfile_oxide_thickness'
[]
[rad_temp]
type = NodalValueSampler
block = 3
sort_by = y
variable = temp
execute_on = timestep_end
outputs = 'outfile_radial_temp'
[]
[]
[StandardLWRFuelRodOutputs]
fuel_pellet_blocks = 3
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
csv = true
color = true
[outfile_oxide_thickness]
type = CSV
sync_times = '99273600 99274100'
sync_only = true
[]
[outfile_radial_temp]
type = CSV
enable = false
[]
[console]
type = Console
output_linear = true
max_rows = 10
[]
[checkpoint]
type = Checkpoint
num_files = 2
file_base = recover_files
sync_times = '99273600'
sync_only = true
[]
[chkfile]
type = CSV
show = 'plenum_temperature fission_gas_released_percentage
average_centerline_fuel_temperature average_burnup peak_RAE'
execute_on = 'FINAL'
[]
[exodus]
type = Exodus
time_step_interval = 4
end_time = 99273700
[]
[exodus_RIA]
type = Exodus
time_step_interval = 2
start_time = 99273695
[]
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-02/puzry-02.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-02.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 2000. '
y = '1.e+05 1.e+05 7.5e+05' # Linear increase at 0.0065 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 2000. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = EigenSolution
[]
[]
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = MaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = FunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = DirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = DirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1.e+11
poissons_ratio = 0.3
block = 1
[]
[creep_update]
type = ZryCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 1.e-04
temperature = temperature
temperature_standard_thermal_creep_end = 700
temperature_loca_creep_begin = 900.
[]
[creep]
type = ComputeMultipleInelasticStress
block = 1
tangent_operator = elastic
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = Density
block = 1
[]
[phase]
type = ZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
active = 'smp'
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0.
n_startup_steps = 1
end_time = 2000.
dtmax = 1.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-02_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/LOCA_ORNL_cladding_burst_tests/analysis/Zr2_2/ornl_zr2_2.i)
# Simulation ORNL burst tests Zr2_2
[GlobalParams]
density = 6550.
order = SECOND
family = LAGRANGE
displacements = 'disp_x disp_y'
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = zr2_ornl_burst_test_mesh.e
[]
[]
[Variables]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func] # only 10 inches of the rod are within the heated zone (cf. Terrani email)
type = PiecewiseBilinear
data_file = temperature_ornl_zr2_2.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
data_file = pressure_inner_ornl_zr2_2.csv
scale_factor = 1.e+06
format = columns
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 700. '
y = '0.1 0.1 ' # atmospheric pressure
scale_factor = 1.e+06
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[clad]
block = cladding
add_variables = true
strain = FINITE
decomposition_method = EigenSolution
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
generate_output = 'vonmises_stress stress_xx stress_yy stress_zz strain_xx
strain_yy strain_zz hoop_stress'
[]
[]
[AuxVariables]
[creep_rate_aux]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase]
order = CONSTANT
family = MONOMIAL
[]
[scale_thickness]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfract_total]
order = CONSTANT
family = MONOMIAL
[]
[oxywtfgain_total]
order = CONSTANT
family = MONOMIAL
[]
[burst_stress]
order = CONSTANT
family = MONOMIAL
[]
[burst]
order = CONSTANT
family = MONOMIAL
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate_aux]
type = MaterialRealAux
variable = creep_rate_aux
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[scl_thickness]
type = MaterialRealAux
variable = scale_thickness
property = oxide_scale_thickness
boundary = 2
[]
[ofract_total]
type = MaterialRealAux
variable = oxywtfract_total
property = current_oxygen_weight_frac_total
boundary = 2
[]
[ofgain_total]
type = MaterialRealAux
boundary = 2
variable = oxywtfgain_total
property = oxygen_weight_frac_gained_total
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = 2
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = 2
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = FunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 4'
preset = false
[]
[no_y_top]
type = DirichletBC
variable = disp_y
boundary = 3
value = 0.
preset = false
[]
[Pressure]
[outer_pressure] # apply steam pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[mid_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 2 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
type = ZryThermal
block = cladding
temperature = temperature
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = cladding
matpro_youngs_modulus = false
matpro_poissons_ratio = false
[]
[clad_stress]
type = ComputeMultipleInelasticStress
tangent_operator = elastic
inelastic_models = 'clad_zrycreep'
block = cladding
[]
[clad_zrycreep]
type = ZryCreepLOCAUpdate
block = cladding
temperature = temperature
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
temperature_loca_creep_begin = 301
temperature_standard_thermal_creep_end = 300
[]
[thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = cladding
temperature = temperature
stress_free_temperature = 300.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[density]
type = Density
block = cladding
[]
[phase]
type = ZrPhase
block = cladding
temperature = temperature
numerical_method = 2
[]
[oxidation]
type = ZryOxidation
boundary = 2
temperature = temperature
clad_inner_radius = 0.004875
clad_outer_radius = 0.005580
normal_operating_temperature_model = epri_kwu_ce
high_temperature_model = leistikow
#use_coolant_channel = true
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = 2
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate_aux
temperature = temperature
fraction_beta_phase = fract_beta_phase
fraction_oxygen_gain = oxywtfgain_total
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0
n_startup_steps = 1
end_time = 700.
dtmax = 2.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 2.
[]
[]
[Postprocessors]
[pressure_inner]
type = FunctionValuePostprocessor
function = inner_pressure_func
execute_on = 'initial timestep_end'
[]
[pressure_outer]
type = FunctionValuePostprocessor
function = outer_pressure_func
execute_on = 'initial timestep_end'
[]
[ave_clad_temp]
type = SideAverageValue
boundary = 2
variable = temperature
execute_on = 'initial timestep_end'
[]
[max_clad_temp]
type = NodalExtremeValue
block = cladding
value_type = max
variable = temperature
execute_on = 'initial timestep_end'
[]
[min_clad_temp]
type = NodalExtremeValue
block = cladding
value_type = min
variable = temperature
execute_on = 'initial timestep_end'
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = cladding
[]
[max_oxygen_fract]
type = ElementExtremeValue
block = cladding
value_type = max
variable = oxywtfract_total
execute_on = 'initial timestep_end'
[]
[max_betaph_fract]
type = ElementExtremeValue
block = cladding
value_type = max
variable = fract_beta_phase
execute_on = 'initial timestep_end'
[]
[max_creep_rate]
type = ElementExtremeValue
block = cladding
value_type = max
variable = creep_rate_aux
execute_on = 'initial timestep_end'
[]
[max_creep_strain_mag]
type = ElementExtremeValue
block = cladding
value_type = max
variable = creep_strain_mag
execute_on = 'initial timestep_end'
[]
[max_hoop_strain]
type = ElementExtremeValue
block = cladding
value_type = max
variable = strain_zz
execute_on = 'initial timestep_end'
[]
[max_hoop_stress]
type = ElementExtremeValue
block = cladding
value_type = max
variable = hoop_stress
[]
[vonmises_stress_clad]
type = ElementAverageValue
block = cladding
variable = vonmises_stress
execute_on = 'initial timestep_end'
[]
[min_burst_stress]
type = ElementExtremeValue
block = cladding
value_type = min
variable = burst_stress
execute_on = 'initial timestep_end'
[]
[burst]
type = ElementExtremeValue
block = cladding
value_type = max
variable = burst
execute_on = 'initial timestep_end'
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = cladding
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[mid_disp_r_clad]
type = NodalVariableValue
variable = disp_x
nodeid = 22
[]
[stress_xx_midplane] # stress in the mid Element
type = ElementalVariableValue
variable = stress_xx
elementid = 19
[]
[stress_yy_midplane] # stress in the mid Element
type = ElementalVariableValue
variable = stress_yy
elementid = 19
[]
[stress_zz_midplane] # stress in the mid Element
type = ElementalVariableValue
variable = stress_zz
elementid = 19
[]
[strain_zz_midplane] # strain in the mid Element
type = ElementalVariableValue
variable = strain_zz
elementid = 19
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
plenum_boundary_name = 4
cladding_blocks = cladding
[]
[PerformanceMetricOutputs]
[]
[Outputs]
exodus = true
perf_graph = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 20
[]
[chkfile]
type = CSV
file_base = ornl_zr2_2_chkfile
show = 'pressure_inner max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/LOCA_PUZRY_cladding_burst_tests/analysis/puzry-08/puzry-08.i)
# Simulation of REBEKA single-rod, cladding-only LOCA tests.
[GlobalParams]
density = 6550.
displacements = 'disp_x disp_y'
order = SECOND
family = LAGRANGE
[]
[Mesh]
coord_type = RZ
[mesh]
type = FileMeshGenerator
file = puzry_mesh.e
[]
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temperature]
initial_condition = 300.
[]
[]
[Functions]
[temperature_func]
type = PiecewiseBilinear
data_file = temperature_puzry-08.csv
axis = 1 # (0,1,2) => (x,y,z)
[]
[inner_pressure_func]
type = PiecewiseLinear
x = '0. 1000. 1200. '
y = '1.e+05 1.e+05 1.626e+06' # Linear increase at 0.0763 bar/s
[]
[outer_pressure_func]
type = PiecewiseLinear
x = '0. 1200. '
y = '1.e+05 1.e+05' # Argon at 1 bar
[]
[]
[AuxVariables]
[creep_rate]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[coolant_htc]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[clad]
strain = FINITE
eigenstrain_names = 'clad_thermal_eigenstrain'
cylindrical_axis_point1 = '0 0 0'
cylindrical_axis_point2 = '0 1 0'
additional_generate_output = 'stress_xx stress_yy stress_zz
vonmises_stress strain_zz hoop_stress'
decomposition_method = EigenSolution
[]
[]
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
[]
[]
[AuxKernels]
[creep_rate]
type = MaterialRealAux
variable = creep_rate
property = creep_rate
execute_on = timestep_end
[]
[creep_strain_mag]
type = MaterialRealAux
property = effective_creep_strain
variable = creep_strain_mag
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
variable = fract_beta_phase
property = fract_beta_phase
[]
[sigmaburst]
type = MaterialRealAux
variable = burst_stress
property = burst_stress
boundary = '2 5'
[]
[hasburst]
type = MaterialRealAux
variable = burst
property = failed
boundary = '2 5'
execute_on = timestep_end
[]
[]
[BCs]
[temperature]
type = FunctionDirichletBC
variable = temperature
function = temperature_func
boundary = '2 5'
[]
[no_x_plug]
type = DirichletBC
variable = disp_x
boundary = 6
value = 0.
[]
[no_y_mid_plane]
type = DirichletBC
variable = disp_y
boundary = 3
value = 0.
[]
[Pressure]
[outer_pressure] # apply Ar pressure on clad outer wall
boundary = 2
function = outer_pressure_func
[]
[inner_pressure] # apply He pressure on clad inner wall
boundary = 4
function = inner_pressure_func
[]
[]
[]
[Constraints]
[bottom_section_plane]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = 126 # node on boundary
secondary = 1 # boundary
penalty = 1.e+10
[]
[]
[Materials]
[thermal]
block = 1
type = ZryThermal
temperature = temperature
[]
[elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1.e+11
poissons_ratio = 0.3
block = 1
[]
[creep_update]
type = ZryCreepLOCAUpdate
block = 1
model_irradiation_creep = false
model_primary_creep = false
model_thermal_creep = true
max_inelastic_increment = 1.e-04
temperature = temperature
temperature_standard_thermal_creep_end = 700
temperature_loca_creep_begin = 900.
[]
[creep]
type = ComputeMultipleInelasticStress
block = 1
tangent_operator = elastic
inelastic_models = 'creep_update'
[]
[clad_thermal_eigenstrain]
type = ZryThermalExpansionMATPROEigenstrain
block = 1
stress_free_temperature = 300.
temperature = temperature
eigenstrain_name = 'clad_thermal_eigenstrain'
[]
[density]
type = Density
block = 1
[]
[phase]
type = ZrPhase
block = 1
temperature = temperature
numerical_method = 2
[]
[failure_criterion]
type = ZryCladdingFailure
boundary = '2 5'
failure_criterion = combined_overstress_and_plastic_instability
hoop_stress = hoop_stress
effective_strain_rate_creep = creep_rate
temperature = temperature
fraction_beta_phase = fract_beta_phase
[]
[]
[Preconditioning]
active = 'smp'
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 100
l_tol = 1e-2
nl_max_its = 15
nl_rel_tol = 1.e-04
nl_abs_tol = 1.e-08
start_time = 0.
n_startup_steps = 1
end_time = 1200.
dtmax = 1.
dtmin = 0.00000001
[TimeStepper]
type = PostprocessorDT
postprocessor = material_timestep
dt = 1.
[]
[]
[UserObjects]
[terminator]
type = Terminator
expression = 'burst > 0'
[]
[fuel_pin_geo]
type = FuelPinGeometry
clad_outer_wall = '2'
clad_inner_wall = '4'
include_fuel = false
[]
[]
[Postprocessors]
[ave_clad_exterior_temp] # average cladding temperature (outer)
type = SideAverageValue
boundary = 2
variable = temperature
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
[]
[max_clad_temp]
type = NodalExtremeValue
value_type = max
variable = temperature
[]
[max_betaph_fract]
type = ElementExtremeValue
value_type = max
variable = fract_beta_phase
[]
[max_creep_rate]
type = ElementExtremeValue
value_type = max
variable = creep_rate
[]
[max_creep_strain_mag]
type = ElementExtremeValue
value_type = max
variable = creep_strain_mag
[]
[max_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
[]
[max_hoop_stress]
type = ElementExtremeValue
value_type = max
variable = hoop_stress
[]
[min_burst_stress]
type = ElementExtremeValue
value_type = min
variable = burst_stress
[]
[pressure_inn]
type = FunctionValuePostprocessor
function = inner_pressure_func
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
[]
[peak_hoop_strain]
type = ElementExtremeValue
value_type = max
variable = strain_zz
block = 1
[]
[zry_burst_opening_area]
type = ZryBurstOpening
fuel_pin_geometry = fuel_pin_geo
peak_hoop_strain = peak_hoop_strain
estimate = limiting
opening_shape = rectangle
output = area
[]
[]
[StandardLWRFuelRodOutputs]
rod_component = clad
cladding_blocks = 1
plenum_boundary_name = '4 6'
external_clad_boundary_name = '2 5'
[]
[PerformanceMetricOutputs]
[]
[Outputs]
perf_graph = true
exodus = true
csv = true
[console]
type = Console
output_linear = true
max_rows = 25
[]
[chkfile]
type = CSV
file_base = puzry-08_out_chkfile
show = 'average_interior_clad_temperature max_hoop_strain max_hoop_stress'
execute_on = 'FINAL'
[]
[]
(assessment/LWR/validation/LOCA_Studsvik/analysis/rod_196/Studsvik_196_part2_1p5d_fr_ffrd.i)
[GlobalParams]
density = 10431.0
initial_porosity = 0.05
order = SECOND
family = LAGRANGE
energy_per_fission = 3.2e-11 # J/fission
volumetric_locking_correction = false
displacements = 'disp_x'
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
restart_file_base = 'Studsvik_196_part1_1p5d_fr_ffrd_checkpoint_cp/LATEST'
[]
[Mesh]
coord_type = RZ
[layered1D_mesh]
type = Layered1DMeshGenerator
slices_per_block = 10
clad_gap_width = 80e-6
plenum_height = 0.0393576
pellet_outer_radius = 3.92e-3
clad_thickness = 0.57e-3
fuel_height = 0.2606424
# nx_c = 2
# nx_p = 11
elem_type = EDGE3
[]
patch_update_strategy = auto
patch_size = 10 # For contact algorithm
partitioner = centroid
centroid_partitioner_direction = y
[]
[Variables]
[temperature]
[]
[]
[AuxVariables]
# Define auxilary variables
[strain_yy_0]
order = CONSTANT
family = MONOMIAL
[]
[fast_neutron_flux]
block = clad
[]
[fast_neutron_fluence]
block = clad
[]
[grain_radius]
block = fuel
[]
[creep_strain_rate]
order = CONSTANT
family = MONOMIAL
[]
[effective_creep_strain]
order = CONSTANT
family = MONOMIAL
[]
[creep_strain_mag]
order = CONSTANT
family = MONOMIAL
[]
[hoop_strain]
order = CONSTANT
family = MONOMIAL
[]
[fract_beta_phase] # Fraction of beta phase in Zry
order = CONSTANT
family = MONOMIAL
[]
[scale_thickness] # ZrO2 scale thickness (m)
order = CONSTANT
family = MONOMIAL
[]
[oxywtfract_total] # Current oxigen weight fraction (oxide+metal) (/)
order = CONSTANT
family = MONOMIAL
[]
[oxywtfgain_total] # Gained oxygen weight fraction (oxide+metal) (/)
order = CONSTANT
family = MONOMIAL
[]
[burst_stress] # Hoop stress at cladding burst
order = CONSTANT
family = MONOMIAL
[]
[burst] # Did cladding burst occur?
order = CONSTANT
family = MONOMIAL
[]
[gap_cond]
order = CONSTANT
family = MONOMIAL
[]
[tangential_contact_pressure_aux]
block = fuel
[]
[]
[Functions]
[power_history]
type = PiecewiseLinear
data_file = power_history.csv
format = columns
scale_factor = 1
[]
[axial_peaking_factors]
type = ParsedFunction
expression = 1
[]
[pressure_ramp] # reads and interpolates input data defining amplitude curve for fill gas pressure
type = PiecewiseLinear
x = '-200 0 86400 47386400 47472800 47559200 47645600 94945600 95032000'
y = '0.0065371 1 1 1 1 1 1 1 0.0065371'
scale_factor = 15.5e6
[]
[clad_surface_temperature]
type = PiecewiseBilinear
axis = 1
data_file = clad_temperature.csv
[]
[forced_times]
type = PiecewiseLinear
data_file = timestep_limiting.csv
scale_factor = 1
format = columns
[]
[clad_axial_pressure]
type = CladdingAxialPressureFunction
plenum_pressure = plenum_pressure
coolant_pressure = pressure_ramp
coolant_pressure_scaling_factor = 1.0
fuel_pin_geometry = fuel_pin_geometry
[]
[fuel_axial_pressure]
type = ParsedFunction
expression = plenum_pressure
symbol_names = plenum_pressure
symbol_values = plenum_pressure
[]
[]
[Physics]
[SolidMechanics]
[Layered1D]
[fuel]
block = fuel
add_variables = true
add_scalar_variables = true
strain = FINITE
out_of_plane_strain_name = strain_yy
eigenstrain_names = 'fuel_thermal_eigenstrain fuel_volumetric_eigenstrain axial_relocation_eigenstrain'
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress strain_xx hoop_stress creep_strain_zz strain_zz'
extra_vector_tags = 'ref'
fuel_pin_geometry = fuel_pin_geometry
group_scalar_vars_in_reference_residual = true
mesh_generator = layered1D_mesh
decomposition_method = EigenSolution
temperature = temperature
out_of_plane_pressure_function = fuel_axial_pressure
layer_friction_user_object = 1DFriction_secondary
[]
[clad]
block = clad
add_variables = true
add_scalar_variables = true
strain = FINITE
out_of_plane_strain_name = strain_yy
eigenstrain_names = 'clad_thermal_eigenstrain clad_irradiation_eigenstrain'
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress strain_xx hoop_stress creep_strain_zz strain_zz'
extra_vector_tags = 'ref'
fuel_pin_geometry = fuel_pin_geometry
group_scalar_vars_in_reference_residual = true
mesh_generator = layered1D_mesh
decomposition_method = EigenSolution
temperature = temperature
out_of_plane_pressure_function = clad_axial_pressure
layer_friction_user_object = 1DFriction_primary
[]
[]
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temperature
extra_vector_tags = 'ref'
[]
[heat_ie]
type = HeatConductionTimeDerivative
variable = temperature
extra_vector_tags = 'ref'
[]
[heat_source]
type = NeutronHeatSource
variable = temperature
extra_vector_tags = 'ref'
block = fuel
burnup_function = burnup
axial_relocation_object = axial_relocation
[]
[]
[Burnup]
[burnup]
block = fuel
rod_ave_lin_pow = power_history # using the power function defined above
axial_power_profile = axial_peaking_factors # using the axial power profile function defined above
num_radial = 80
num_axial = 11
fuel_pin_geometry = fuel_pin_geometry
fuel_volume_ratio = 1.0 # for use with dished pellets (ratio of actual volume to cylinder volume)
order = CONSTANT
family = MONOMIAL
RPF = RPF
isotopes = 'U235 U238 Pu239 Pu240 Pu241 Pu242'
isotope_fractions = '0.05 0.95 0 0 0 0'
[]
[]
[AuxKernels]
# Define auxilliary kernels for each of the aux variables
[tangential_contact_pressure_aux]
type = SpatialUserObjectAux
variable = tangential_contact_pressure_aux
user_object = 1DFriction_secondary
block = fuel
execute_on = 'TIMESTEP_END'
[]
[fast_neutron_flux]
type = FastNeutronFluxAux
variable = fast_neutron_flux
block = clad
rod_ave_lin_pow = power_history
axial_power_profile = axial_peaking_factors
factor = 3e13
execute_on = timestep_begin
[]
[fast_neutron_fluence]
type = FastNeutronFluenceAux
variable = fast_neutron_fluence
block = clad
fast_neutron_flux = fast_neutron_flux
execute_on = timestep_begin
[]
[grain_radius]
type = GrainRadiusAux
block = fuel
variable = grain_radius
temperature = temperature
execute_on = linear
[]
[creep_strain_rate]
type = MaterialRealAux
property = creep_rate
variable = creep_strain_rate
block = clad
[]
[effective_creep_strain]
type = MaterialRealAux
property = effective_creep_strain
variable = effective_creep_strain
block = clad
execute_on = timestep_end
[]
[fract_bphase]
type = MaterialRealAux
block = clad
variable = fract_beta_phase
property = fract_beta_phase
[]
[scl_thickness]
type = MaterialRealAux
boundary = 2
variable = scale_thickness
property = oxide_scale_thickness
[]
[ofract_total]
type = MaterialRealAux
boundary = 2
variable = oxywtfract_total
property = current_oxygen_weight_frac_total
[]
[ofgain_total]
type = MaterialRealAux
boundary = 2
variable = oxywtfgain_total
property = oxygen_weight_frac_gained_total
[]
[sigmaburst]
type = MaterialRealAux
boundary = 2
variable = burst_stress
property = burst_stress
[]
[hasburst]
type = MaterialRealAux
boundary = 2
variable = burst
property = failed
execute_on = timestep_end
[]
[conductance]
type = MaterialRealAux
property = gap_conductance
variable = gap_cond
boundary = 10
execute_on = 'linear'
[]
[]
[Contact]
[pellet_clad_mechanical]
primary = 5
secondary = 10
formulation = kinematic
model = frictionless
penalty = 1e7
[]
[]
[ThermalContact]
[thermal_contact]
type = GasGapHeatTransfer
variable = temperature
primary = 5
secondary = 10
initial_moles = initial_moles
gas_released = 'fission_gas_released he_prod'
released_gas_types = 'Kr Xe;
He'
released_fractions = '0.153 0.847;
1'
quadrature = true
contact_pressure = contact_pressure
refab_gas_types = He
refab_fractions = 1
refab_time = 95032000
refab_type = 0
[]
[]
[BCs]
[no_x_all]
type = DirichletBC
variable = disp_x
boundary = 12
value = 0.0
[]
[Pressure]
[coolantPressure]
boundary = '2'
function = pressure_ramp
[]
[]
[PlenumPressure]
[plenumPressure]
boundary = 9
initial_pressure = 3.44738e6
startup_time = 0
R = 8.3143
output_initial_moles = initial_moles
temperature = plenum_temp
volume = plenum_volume
material_input = 'fission_gas_released he_prod'
output = plenum_pressure
refab_time = 95032000
refab_pressure = 8.2e6
refab_temperature = 295.0
refab_volume = 1.04e-05
cladding_failure_status = burst
equilibrium_pressure = equilibrium_pressure
additional_volumes = additional_volume
temperature_of_additional_volumes = addition_temperature
[]
[]
[clad_temp]
type = FunctionDirichletBC
function = clad_surface_temperature
variable = temperature
boundary = 2
[]
[]
[UserObjects]
[layered_average_hoop_strain]
type = LayeredAverage
block = clad
num_layers = 10
direction = y
variable = strain_zz
[]
[cladding_strain_yy]
type = LayeredAverage
block = clad
num_layers = 11
direction = y
variable = strain_yy
execute_on = 'initial timestep_end'
[]
[fuel_strain_yy]
type = LayeredAverage
block = fuel
num_layers = 10
direction = y
variable = strain_yy
execute_on = 'initial timestep_end'
[]
[1DContactStressOOP_fuel]
type = Layered1DContactInterfaceStress
direction = y
stress_name = stress
num_layers = 10
# If we do not provide the numbers below, it will look at the mesh, in all blocks to set the layer number. Then, it will
# be wrong because the cladding has more height and won't be able to identify layers in the fuel.
direction_min = 0.01306
direction_max = 0.24761028
block = fuel
execute_on = 'LINEAR NONLINEAR'
[]
[1DContactStressOOP_cladding]
type = Layered1DContactInterfaceStress
direction = y
stress_name = stress
num_layers = 10
# If we do not provide the numbers below, it will look at the mesh, in all blocks to set the layer number. Then, it will
# be wrong because the cladding has more height and won't be able to identify layers in the fuel.
direction_min = 0.01306
direction_max = 0.24761028
block = clad
execute_on = 'LINEAR NONLINEAR'
[]
[1DFriction_secondary]
type = Layered1DFrictionalForce
force_postaux = true
contact_pressure = contact_pressure
direction = y
boundary = pellet_outer_radial_surface
num_layers = 10
interface_oop_stress_provider_fuel = 1DContactStressOOP_fuel
interface_oop_stress_provider_cladding = 1DContactStressOOP_cladding
is_secondary_side = true
tangential_pressure = tangential_contact_pressure_aux
friction_coefficient = 0.2
thickness = 0.02606424
penalty_factor = 1.0e13
# If we do not provide the numbers below, it will look at the mesh, in all blocks to set the layer number. Then, it will
# be wrong because the cladding has more height and won't be able to identify layers in the fuel.
direction_min = 0.01306
direction_max = 0.24761028
scalar_var_name_base_fuel = scalar_strain_yy_fuel
scalar_num_variable_fuel = 10
scalar_var_name_base_cladding = scalar_strain_yy_clad
scalar_num_variable_cladding = 10
execute_on = 'LINEAR NONLINEAR'
[]
[1DFriction_primary]
type = Layered1DFrictionalForce
force_postaux = true
contact_pressure = contact_pressure
direction = y
boundary = clad_inside_right
num_layers = 10
# If we do not provide the numbers below, it will look at the mesh, in all blocks to set the layer number. Then, it will
# be wrong because the cladding has more height and won't be able to identify layers in the fuel.
direction_min = 0.0165094
direction_max = 0.24761028
interface_oop_stress_provider_fuel = 1DContactStressOOP_fuel
interface_oop_stress_provider_cladding = 1DContactStressOOP_cladding
is_secondary_side = false
secondary_side_frictional_user_object = 1DFriction_secondary
friction_coefficient = 0.2
thickness = 0.02606424
penalty_factor = 1.0e13
scalar_var_name_base_fuel = scalar_strain_yy_fuel
scalar_num_variable_fuel = 10
scalar_var_name_base_cladding = scalar_strain_yy_clad
scalar_num_variable_cladding = 10
execute_on = 'LINEAR NONLINEAR'
[]
[terminator]
type = Terminator
expression = 'max_axial_relocation_strain > 0.25'
[]
[]
[PlenumTemperature]
[plenum_temp]
boundary = 5
inner_surfaces = '5'
outer_surfaces = '10'
temperature = temperature
[]
[]
[CoolantChannel]
[convective_clad_surface] # apply convective boundary to clad outer surface
boundary = 2
variable = temperature
inlet_temperature = 580
inlet_pressure = 15.5e6 # Pa
inlet_massflux = 3800 # kg/m^2-sec
rod_diameter = 0.00914 # m
rod_pitch = 1.26e-2 # m
compute_enthalpy = false
linear_heat_rate = power_history
axial_power_profile = axial_peaking_factors
output_properties = 'coolant_channel_htype coolant_channel_hmode'
[]
[]
[Materials]
[fuel_dispersal]
type = UO2Dispersal
block = fuel
axial_relocation_object = axial_relocation
layered_average_burnup = layered_average_burnup
layered_average_hoop_strain = layered_average_hoop_strain
dispersal_model = ONE_MM_TWO_PERCENT_STRAIN
[]
# Define material behavior models and input material property data
[fuel_thermal] # temperature and burnup dependent thermal properties of UO2 (BISON kernel)
type = UO2Thermal
block = fuel
thermal_conductivity_model = NFIR
temperature = temperature
burnup_function = burnup
axial_relocation_object = axial_relocation
gap_thermal_conductivity = layered_average_gap_conductivity
[]
[fuel_elasticity_tensor]
type = UO2IsotropicDamageElasticityTensor
block = fuel
fragmentation_model = BARANI
rod_ave_lin_pow = power_history
temperature = temperature
axial_relocation_object = axial_relocation
[]
[fuel_elastic_stress]
type = ComputeMultipleInelasticStress
tangent_operator = elastic
inelastic_models = 'fuel_creep'
block = fuel
[]
[fuel_creep]
type = UO2CreepUpdate
block = fuel
temperature = temperature
fission_rate = fission_rate
initial_grain_radius = 10.0e-6
oxygen_to_metal_ratio = 2.0
[]
[fuel_thermal_expansion]
type = ComputeThermalExpansionEigenstrain
block = fuel
thermal_expansion_coeff = 10.0e-6
temperature = temperature
stress_free_temperature = 295.0
eigenstrain_name = fuel_thermal_eigenstrain
[]
[fuel_volumetric_swelling]
type = UO2VolumetricSwellingEigenstrain
gas_swelling_model_type = SIFGRS
block = fuel
temperature = temperature
burnup_function = burnup
initial_fuel_density = 10431.0
eigenstrain_name = fuel_volumetric_eigenstrain
[]
[fission_gas_release]
type = UO2Sifgrs
block = fuel
temperature = temperature
burnup_function = burnup
grain_radius = grain_radius
gbs_model = true
[]
[clad_density]
type = Density
block = clad
density = 6550.
[]
[clad_thermal]
block = clad
type = ZryThermal
temperature = temperature
[]
[clad_thermal_expansion]
type = ZryThermalExpansionMATPROEigenstrain
block = clad
temperature = temperature
stress_free_temperature = 295.0
eigenstrain_name = clad_thermal_eigenstrain
[]
[clad_elasticity_tensor]
type = ZryElasticityTensor
block = clad
temperature = temperature
[]
[zry_thermal_creep]
type = ZryCreepLOCAUpdate
block = clad
temperature = temperature
model_irradiation_creep = true
model_primary_creep = true
model_thermal_creep = true
max_inelastic_increment = 5e-4
fast_neutron_flux = fast_neutron_flux
fast_neutron_fluence = fast_neutron_fluence
zircaloy_material_type = zirlo
[]
[clad_stress]
type = ComputeMultipleInelasticStress
tangent_operator = elastic
inelastic_models = 'zry_thermal_creep'
block = clad
[]
[clad_irradiation_growth]
type = ZryIrradiationGrowthEigenstrain
block = clad
fast_neutron_fluence = fast_neutron_fluence
zircaloy_material_type = zirlo
eigenstrain_name = clad_irradiation_eigenstrain
[]
[clad_phase]
type = ZrPhase
block = clad
temperature = temperature
numerical_method = 2
[]
[clad_oxidation]
type = ZryOxidation
boundary = 2
temperature = temperature
clad_inner_radius = 4.18e-03
clad_outer_radius = 4.75e-03
normal_operating_temperature_model = epri_kwu_ce
high_temperature_model = leistikow
[]
[clad_failure_criterion]
type = ZryCladdingFailure
boundary = 2
failure_criterion = overstrain
hoop_stress = hoop_stress
hoop_creep_strain = creep_strain_zz
fraction_beta_phase = fract_beta_phase
fraction_oxygen_gain = oxywtfract_total
temperature = temperature
[]
[fuel_density]
type = Density
block = fuel
[]
[]
[VectorPostprocessors]
[cladding_outer]
type = NodalValueSampler
boundary = 5
variable = disp_x
sort_by = y
[]
[]
[AxialRelocation]
[relocation]
rod_ave_lin_pow = power_history
axial_direction = y
fuel_blocks = fuel
clad_blocks = clad
contact_pressure_variable = contact_pressure
out_of_plane_strain_variable = strain_yy_0
penetration_variable = penetration
clad_inner_volume_addition = 0
burnup_variable = burnup
temperature = temperature
axial_relocation_output_options = MASS_FRACTION
mesh_generator = layered1D_mesh
# CHANGE
gap_thickness_threshold = 0.000050
[]
[]
[Postprocessors]
[volume_fuel_dispersed]
type = LayeredElementIntegralMaterialProperty
block = fuel
mat_prop = dispersed
fuel_pin_geometry = fuel_pin_geometry
execute_on = 'initial timestep_end'
[]
[mass_fuel_dispersed]
type = ParsedPostprocessor
pp_names = volume_fuel_dispersed
expression = '10431 * volume_fuel_dispersed'
execute_on = 'initial timestep_end'
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
l_max_its = 50
l_tol = 8e-3
nl_max_its = 15
nl_rel_tol = 1e-4
nl_abs_tol = 1e-8
n_startup_steps = 1
end_time = 95033429.6
dtmax = 20
dtmin = 1e-6
[TimeStepper]
type = IterationAdaptiveDT
timestep_limiting_postprocessor = material_timestep
dt = 10
optimal_iterations = 20
iteration_window = 4
linear_iteration_ratio = 100
growth_factor = 2
cutback_factor = .5
timestep_limiting_function = forced_times
force_step_every_function_point = true
[]
[Quadrature]
order = FIFTH
side_order = SEVENTH
[]
[]
[Postprocessors]
[ave_temp_interior]
type = SideAverageValue
boundary = 9
variable = temperature
execute_on = 'initial linear'
[]
[clad_inner_vol]
type = InternalVolume
boundary = 7
#outputs = exodus
execute_on = 'initial timestep_end'
[]
[fission_gas_produced] # fission gas produced (moles)
type = ElementIntegralFisGasGeneratedSifgrs
block = fuel
execute_on = 'linear'
[]
[fission_gas_grain]
type = ElementIntegralFisGasGrainSifgrs
block = fuel
outputs = exodus
execute_on = 'linear'
[]
[fission_gas_boundary]
type = ElementIntegralFisGasBoundarySifgrs
block = fuel
outputs = exodus
execute_on = 'linear'
[]
[flux_from_clad] # area integrated heat flux from the cladding
type = SideDiffusiveFluxIntegral
variable = temperature
boundary = 5
diffusivity = thermal_conductivity
[]
[flux_from_fuel] # area integrated heat flux from the fuel
type = SideDiffusiveFluxIntegral
variable = temperature
boundary = 10
diffusivity = thermal_conductivity
[]
[rod_total_power]
type = ElementIntegralPower
variable = temperature
burnup_function = burnup
block = fuel
[]
[max_fuel_temp]
type = NodalExtremeValue
block = fuel
value_type = max
variable = temperature
[]
[max_clad_temp]
type = NodalExtremeValue
block = clad
value_type = max
variable = temperature
[]
[max_clad_hoop_strain]
type = ElementExtremeValue
block = clad
value_type = max
variable = strain_zz
[]
[material_timestep]
type = MaterialTimeStepPostprocessor
block = clad
[]
[max_axial_relocation_strain]
type = ElementExtremeValue
value_type = max
variable = axial_relocation_strain
block = fuel
execute_on = 'initial timestep_end'
[]
[he_prod]
type = IFBAHeProduction
b10_load = 9.27165354e-5
b10_enrich = 0.5
burnup = average_burnup
zrb2_thick = 10e-6
fuel_out_rad = 9.32e-3
ifba_len = 0.3
u235_enrich = 0.05
[]
[burst]
type = ElementExtremeValue
value_type = max
variable = burst
block = clad
execute_on = 'initial timestep_end'
[]
[volume_pulverized]
type = ElementIntegralMaterialProperty
mat_prop = pulverized
block = fuel
[]
[max_fuel_temp_periphery]
type = NodalExtremeValue
value_type = max
variable = temperature
boundary = 10
[]
[additional_volume]
type = FunctionValuePostprocessor
function = 8.5e-6
execute_on = 'initial linear'
[]
[addition_temperature]
type = FunctionValuePostprocessor
function = 300.0
execute_on = 'initial linear'
[]
[equilibrium_pressure]
type = FunctionValuePostprocessor
function = 101325.0
execute_on = 'initial linear'
[]
[]
[PerformanceMetricOutputs]
[]
[StandardLWRFuelRodOutputs]
temperature = temperature
layered = true
fuel_pellet_blocks = 'fuel'
fuel_pin_geometry = fuel_pin_geometry
[]
[Outputs]
perf_graph = true
exodus = true
color = false
csv = true
[chkfile]
type = CSV
execute_on = FINAL
show = 'volume_pulverized'
[]
[]