update values and config template

su2code · Dec 25, 2024 · 28fb23d · 28fb23d
1 parent bee055e
commit 28fb23d
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Showing 2 changed files with 24 additions and 28 deletions.
diff --git a/TestCases/parallel_regression.py b/TestCases/parallel_regression.py
@@ -1233,8 +1233,7 @@ def main():
     # For a thin disk with the inner and outer radius of this geometry, from
     # "Formulas for Stress, Strain, and Structural Matrices", 2nd Edition, figure 19-4,
     # the maximum stress is 165.6MPa, we get a Von Misses stress very close to that.
-    rotating_cylinder_fea.test_vals = [-1.986097, -1.023250, -1.022700, 47, -8.101266, 1.6458e+08]
-    rotating_cylinder_fea.command   = TestCase.Command(exec = "parallel_computation_fsi.py", param = "-f")
+    rotating_cylinder_fea.test_vals = [-6.005467, -5.615543, -5.615527, 38, -8.126591, 1.6457e8]
     test_list.append(rotating_cylinder_fea)
 
     # Dynamic beam, 2d

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