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update values and config template
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TestCases/parallel_regression.py

Lines changed: 1 addition & 2 deletions
Original file line numberDiff line numberDiff line change
@@ -1233,8 +1233,7 @@ def main():
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# For a thin disk with the inner and outer radius of this geometry, from
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# "Formulas for Stress, Strain, and Structural Matrices", 2nd Edition, figure 19-4,
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# the maximum stress is 165.6MPa, we get a Von Misses stress very close to that.
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rotating_cylinder_fea.test_vals = [-1.986097, -1.023250, -1.022700, 47, -8.101266, 1.6458e+08]
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rotating_cylinder_fea.command = TestCase.Command(exec = "parallel_computation_fsi.py", param = "-f")
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rotating_cylinder_fea.test_vals = [-6.005467, -5.615543, -5.615527, 38, -8.126591, 1.6457e8]
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test_list.append(rotating_cylinder_fea)
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# Dynamic beam, 2d

config_template.cfg

Lines changed: 23 additions & 26 deletions
Original file line numberDiff line numberDiff line change
@@ -1742,12 +1742,17 @@ KNOWLES_N= 1.0
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% ID of the region we want to compute the sensitivities using direct differentiation
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FEA_ID_DIRECTDIFF= 0
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%
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%
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RESTART_STEADY_STATE= NO
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%
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% Time discretization
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TIME_DISCRE_FEA= NEWMARK_IMPLICIT
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%
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% Iterative method for non-linear structural analysis
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NONLINEAR_FEM_SOLUTION_METHOD= NEWTON_RAPHSON
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%
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% Pseudo static analysis (no density in dynamic analysis)
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PSEUDO_STATIC= NO
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%
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% Parameter alpha for Newmark scheme (s)
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NEWMARK_BETA= 0.25
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%
@@ -1781,6 +1786,9 @@ MATERIAL_MODEL= LINEAR_ELASTIC
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% Compressibility of the material
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MATERIAL_COMPRESSIBILITY= COMPRESSIBLE
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%
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% Formulation for 2-dimensional elasticity solver
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FORMULATION_ELASTICITY_2D= PLANE_STRAIN
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%
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% -------------------- Dielectric effects ------------------%
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%
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% Include DE effects
@@ -1794,6 +1802,20 @@ ELECTRIC_FIELD_MOD= 20e5
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%
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% Direction of the Electic Fields
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ELECTRIC_FIELD_DIR= (0.0, 1.0)
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%
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% ------------------------ Prestretch -----------------------%
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%
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% Consider a prestretch in the structural domain
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PRESTRETCH= NO
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%
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% Filename to input for prestretching membranes
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PRESTRETCH_FILENAME= prestretch_file.dat
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%
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% ----------------------- Body Forces -----------------------%
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%
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% Centrifugal forces due to ROTATION_RATE around MOTION_ORIGIN.
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% GRAVITY_FORCE and BODY_FORCE can also be used with the FEA solver.
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CENTRIFUGAL_FORCE= NO
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% -------------------- Weakly Coupled Heat ------------------%
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%
@@ -2010,31 +2032,6 @@ STRESS_PENALTY_PARAM= (1.0, 10.0)
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% Preaccumulation in the AD mode.
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PREACC= YES
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% ---------------- PRESTRETCH FOR STRUCTURES -------------------%
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% Consider a prestretch in the structural domain
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PRESTRETCH= NO
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%
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% Filename to input for prestretching membranes
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PRESTRETCH_FILENAME= prestretch_file.dat
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%
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% Iterative method for non-linear structural analysis
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NONLINEAR_FEM_SOLUTION_METHOD= NEWTON_RAPHSON
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%
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% Formulation for bidimensional elasticity solver
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FORMULATION_ELASTICITY_2D= PLANE_STRAIN
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%
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% Pseudo static analysis (no density in dynamic analysis)
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PSEUDO_STATIC= NO
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%
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% Dynamic or static structural analysis (deprecated -> use TIME_DOMAIN)
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DYNAMIC_ANALYSIS= NO
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%
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% Time Step for dynamic analysis (s) (deprecated -> use TIME_STEP)
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DYN_TIMESTEP= 0.0
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%
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% Total Physical Time for dual time stepping simulations (s) (deprecated -> use MAX_TIME)
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DYN_TIME= 1.0
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% ---------------- MESH DEFORMATION PARAMETERS (NEW SOLVER) -------------------%
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%
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% Use the reformatted pseudo-elastic solver for grid deformation

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