updating residuals regression cases

Author: Cristopher-Morales

TestCases/hybrid_regression.py

@@ -111,7 +111,7 @@ def main():
     cylinder.cfg_dir   = "navierstokes/cylinder"
     cylinder.cfg_file  = "lam_cylinder.cfg"
     cylinder.test_iter = 25
-    cylinder.test_vals = [-8.266513, -2.783904, -0.019899, 1.615668, 0]
+    cylinder.test_vals = [-8.266602, -2.784028, -0.019899, 1.615655, 0.000000]
     test_list.append(cylinder)
 
     # Laminar cylinder (low Mach correction)
@@ -197,16 +197,16 @@ def main():
     turb_naca0012_sa.cfg_dir   = "rans/naca0012"
     turb_naca0012_sa.cfg_file  = "turb_NACA0012_sa.cfg"
     turb_naca0012_sa.test_iter = 5
-    turb_naca0012_sa.test_vals         = [-12.050637, -16.149098, 1.058588, 0.022984, 20.000000, -2.832819, 0.000000, -14.067279, 0]
-    turb_naca0012_sa.test_vals_aarch64 = [-12.050637, -16.149098, 1.058588, 0.022984, 20.000000, -2.832819, 0.000000, -14.067279, 0]
+    turb_naca0012_sa.test_vals         = [-12.050557, -16.149098, 1.058588, 0.022984, 20.000000, -2.832714, 0.000000, -14.067279, 0.000000]
+    turb_naca0012_sa.test_vals_aarch64 = [-12.050557, -16.149098, 1.058588, 0.022984, 20.000000, -2.832714, 0.000000, -14.067279, 0.000000]
     test_list.append(turb_naca0012_sa)
 
     # NACA0012 (SST, FUN3D finest grid results: CL=1.0840, CD=0.01253)
     turb_naca0012_sst           = TestCase('turb_naca0012_sst')
     turb_naca0012_sst.cfg_dir   = "rans/naca0012"
     turb_naca0012_sst.cfg_file  = "turb_NACA0012_sst.cfg"
     turb_naca0012_sst.test_iter = 10
-    turb_naca0012_sst.test_vals = [-12.079595, -15.284132, -5.859466, 1.048053, 0.019238, -2.814059, 0.000000]
+    turb_naca0012_sst.test_vals = [-12.079119, -15.284130, -5.859467, 1.048053, 0.019238, -2.814455, 0.000000]
     test_list.append(turb_naca0012_sst)
 
     # NACA0012 (SST_SUST, FUN3D finest grid results: CL=1.0840, CD=0.01253)
@@ -250,7 +250,7 @@ def main():
     axi_rans_air_nozzle_restart.cfg_dir   = "axisymmetric_rans/air_nozzle"
     axi_rans_air_nozzle_restart.cfg_file  = "air_nozzle_restart.cfg"
     axi_rans_air_nozzle_restart.test_iter = 10
-    axi_rans_air_nozzle_restart.test_vals = [-14.137579, -9.105575, -10.894183, -5.810269, 0.000000]
+    axi_rans_air_nozzle_restart.test_vals = [-14.137398, -9.107808, -10.879850, -5.806591, 0.000000]
     test_list.append(axi_rans_air_nozzle_restart)
 
     #################################
@@ -419,7 +419,7 @@ def main():
     inc_weakly_coupled.cfg_dir = "disc_adj_heat"
     inc_weakly_coupled.cfg_file = "primal.cfg"
     inc_weakly_coupled.test_iter = 10
-    inc_weakly_coupled.test_vals = [-18.095922, -16.331787, -16.514014, -13.703679, -18.203865, -14.053738, 5.545900]
+    inc_weakly_coupled.test_vals = [-18.095922, -16.331787, -16.514014, -9.756795, -18.203865, -14.053738, 5.550800]
     test_list.append(inc_weakly_coupled)
 
     ######################################
@@ -452,7 +452,7 @@ def main():
     square_cylinder.cfg_dir   = "unsteady/square_cylinder"
     square_cylinder.cfg_file  = "turb_square.cfg"
     square_cylinder.test_iter = 3
-    square_cylinder.test_vals = [-2.560838, -1.175929, 0.062081, 1.399401, 2.220361, 1.399349, 2.218600, 0.000000]
+    square_cylinder.test_vals = [-2.560665, -1.175915, 0.062109, 1.399401, 2.220361, 1.399349, 2.218600, 0.000000]
     square_cylinder.test_vals_aarch64 = [-2.557902, -1.173574, 0.058050, 1.399794, 2.220402, 1.399748, 2.218604, 0]
     square_cylinder.unsteady  = True
     test_list.append(square_cylinder)

TestCases/hybrid_regression_AD.py

@@ -86,7 +86,7 @@ def main():
     discadj_rans_naca0012_sst.cfg_dir   = "disc_adj_rans/naca0012"
     discadj_rans_naca0012_sst.cfg_file  = "turb_NACA0012_sst.cfg"
     discadj_rans_naca0012_sst.test_iter = 10
-    discadj_rans_naca0012_sst.test_vals = [-2.236574, -0.190312, 2.762800, -0.039660]
+    discadj_rans_naca0012_sst.test_vals = [-2.236564, -0.190312, 2.762900, -0.039660]
     test_list.append(discadj_rans_naca0012_sst)
 
     #######################################

TestCases/parallel_regression.py

@@ -319,15 +319,15 @@ def main():
     cylinder.cfg_dir   = "navierstokes/cylinder"
     cylinder.cfg_file  = "lam_cylinder.cfg"
     cylinder.test_iter = 25
-    cylinder.test_vals = [-8.422091, -2.930561, -0.003396, 1.608418, 0.000000]
+    cylinder.test_vals = [-8.422012, -2.930518, -0.003394, 1.608420, 0.000000]
     test_list.append(cylinder)
 
     # Laminar cylinder (low Mach correction)
     cylinder_lowmach           = TestCase('cylinder_lowmach')
     cylinder_lowmach.cfg_dir   = "navierstokes/cylinder"
     cylinder_lowmach.cfg_file  = "cylinder_lowmach.cfg"
     cylinder_lowmach.test_iter = 25
-    cylinder_lowmach.test_vals = [-6.841604, -1.379532, -1.266739, 76.118218, 0.000000]
+    cylinder_lowmach.test_vals = [-6.841606, -1.379533, -1.266782, 76.118168, 0.000000]
     test_list.append(cylinder_lowmach)
 
     # 2D Poiseuille flow (body force driven with periodic inlet / outlet)
@@ -389,7 +389,7 @@ def main():
     turb_flatplate_species.cfg_dir   = "rans/flatplate"
     turb_flatplate_species.cfg_file  = "turb_SA_flatplate_species.cfg"
     turb_flatplate_species.test_iter = 20
-    turb_flatplate_species.test_vals = [-4.249474, -0.634908, -1.716288, 1.223201, -3.307930, 9.000000, -6.634095, 5.000000, -6.986784, 10.000000, -6.255641, 0.999903, 0.999903]
+    turb_flatplate_species.test_vals = [-4.249462, -0.634904, -1.716285, 1.223210, -3.307930, 9.000000, -6.633666, 5.000000, -6.986787, 10.000000, -6.255670, 0.999903, 0.9999033]
     test_list.append(turb_flatplate_species)
 
     # Flat plate SST compressibility correction Wilcox
@@ -441,7 +441,7 @@ def main():
     turb_naca0012_sa.cfg_dir   = "rans/naca0012"
     turb_naca0012_sa.cfg_file  = "turb_NACA0012_sa.cfg"
     turb_naca0012_sa.test_iter = 5
-    turb_naca0012_sa.test_vals = [-12.050143, -16.185204, 1.058588, 0.022984, 20.000000, -1.562786, 20.000000, -3.900124, 0.000000]
+    turb_naca0012_sa.test_vals = [12.050132, -16.185205, 1.058588, 0.022984, 20.000000, -1.562866, 20.000000, -3.900107, 0.000000]
     turb_naca0012_sa.timeout   = 3200
     test_list.append(turb_naca0012_sa)
 
@@ -450,7 +450,7 @@ def main():
     turb_naca0012_sst.cfg_dir   = "rans/naca0012"
     turb_naca0012_sst.cfg_file  = "turb_NACA0012_sst.cfg"
     turb_naca0012_sst.test_iter = 10
-    turb_naca0012_sst.test_vals = [-12.078661, -15.284104, -5.859484, 1.048053, 0.019238, -2.015232, 0.000000]
+    turb_naca0012_sst.test_vals = [-12.078069, -15.284102, -5.859484, 1.048053, 0.019238, -2.015780, 0.000000]
     turb_naca0012_sst.test_vals_aarch64 = [-12.232530, -14.435294, -6.037147, 1.047444, 0.019214, -1.704457, 0.000000]
     turb_naca0012_sst.timeout   = 3200
     test_list.append(turb_naca0012_sst)
@@ -460,7 +460,7 @@ def main():
     turb_naca0012_sst_sust.cfg_dir   = "rans/naca0012"
     turb_naca0012_sst_sust.cfg_file  = "turb_NACA0012_sst_sust.cfg"
     turb_naca0012_sst_sust.test_iter = 10
-    turb_naca0012_sst_sust.test_vals = [-12.075115, -14.836721, -5.743103, 1.000050, 0.019144, -2.229293]
+    turb_naca0012_sst_sust.test_vals = [-12.075017, -14.836721, -5.743103, 1.000050, 0.019144, -2.229488]
     turb_naca0012_sst_sust.test_vals_aarch64 = [-12.146171, -14.781592, -6.358755, 1.000270, 0.019123, -1.593320]
     turb_naca0012_sst_sust.timeout   = 3200
     test_list.append(turb_naca0012_sst_sust)
@@ -530,7 +530,7 @@ def main():
     axi_rans_air_nozzle_restart.cfg_dir   = "axisymmetric_rans/air_nozzle"
     axi_rans_air_nozzle_restart.cfg_file  = "air_nozzle_restart.cfg"
     axi_rans_air_nozzle_restart.test_iter = 10
-    axi_rans_air_nozzle_restart.test_vals = [-14.140338, -9.122501, -10.859866, -5.788769, 0.000000]
+    axi_rans_air_nozzle_restart.test_vals = [-14.140949, -9.128061, -10.858923, -5.788079, 0.000000]
     axi_rans_air_nozzle_restart.tol       = 0.0001
     test_list.append(axi_rans_air_nozzle_restart)
 
@@ -740,7 +740,7 @@ def main():
     turbmod_sa_neg_rae2822.cfg_dir   = "turbulence_models/sa/rae2822"
     turbmod_sa_neg_rae2822.cfg_file  = "turb_SA_NEG_RAE2822.cfg"
     turbmod_sa_neg_rae2822.test_iter = 10
-    turbmod_sa_neg_rae2822.test_vals         = [-1.345491, 1.448526, 1.208572, -0.846542, 1.263765, 0.494751, 0.000000]
+    turbmod_sa_neg_rae2822.test_vals         = [-1.345531, 1.448387, 1.208638, -0.846585, 1.271362, 0.497475, 0.000000]
     turbmod_sa_neg_rae2822.test_vals_aarch64 = [-1.359612, 1.493629, 1.218367, -1.441703, 1.248499, 0.457987, 0]
     test_list.append(turbmod_sa_neg_rae2822)
 
@@ -913,7 +913,7 @@ def main():
     turb_naca0012_p1c1.cfg_dir   = "rans_uq/naca0012"
     turb_naca0012_p1c1.cfg_file  = "turb_NACA0012_uq_p1c1.cfg"
     turb_naca0012_p1c1.test_iter = 10
-    turb_naca0012_p1c1.test_vals = [-5.122030, 1.284489, 0.608721, -0.008603]
+    turb_naca0012_p1c1.test_vals = [-5.122041, 1.284479, 0.608705, -0.008610]
     test_list.append(turb_naca0012_p1c1)
 
     # NACA0012 p1c2
@@ -970,7 +970,7 @@ def main():
     spinning_cylinder.cfg_dir   = "moving_wall/spinning_cylinder"
     spinning_cylinder.cfg_file  = "spinning_cylinder.cfg"
     spinning_cylinder.test_iter = 25
-    spinning_cylinder.test_vals = [-7.806056, -2.364884, 1.685228, 1.518276]
+    spinning_cylinder.test_vals = [-7.806025, -2.364860, 1.685247, 1.518292]
     test_list.append(spinning_cylinder)
 
     ######################################
@@ -982,7 +982,7 @@ def main():
     square_cylinder.cfg_dir   = "unsteady/square_cylinder"
     square_cylinder.cfg_file  = "turb_square.cfg"
     square_cylinder.test_iter = 3
-    square_cylinder.test_vals = [-1.175927, 0.062096, 1.399402, 2.220364, 1.399350, 2.218602, 0.000000]
+    square_cylinder.test_vals = [-1.175913, 0.062109, 1.399402, 2.220364, 1.399350, 2.218602, 0.000000]
     square_cylinder.unsteady  = True
     test_list.append(square_cylinder)
 
@@ -1387,7 +1387,7 @@ def main():
     pywrapper_turb_naca0012_sst.cfg_dir   = "rans/naca0012"
     pywrapper_turb_naca0012_sst.cfg_file  = "turb_NACA0012_sst.cfg"
     pywrapper_turb_naca0012_sst.test_iter = 10
-    pywrapper_turb_naca0012_sst.test_vals = [-12.078661, -15.284104, -5.859484, 1.048053, 0.019238, -2.015232, 0.000000]
+    pywrapper_turb_naca0012_sst.test_vals = [-12.078069, -15.284102, -5.859484, 1.048053, 0.019238, -2.015780, 0.000000]
     pywrapper_turb_naca0012_sst.test_vals_aarch64 = [-12.232530, -14.435294, -6.037147, 1.047444, 0.019214, -1.704457, 0.000000]
     pywrapper_turb_naca0012_sst.command   = TestCase.Command("mpirun -np 2", "SU2_CFD.py", "--parallel -f")
     pywrapper_turb_naca0012_sst.timeout   = 3200
@@ -1398,7 +1398,7 @@ def main():
     pywrapper_square_cylinder.cfg_dir   = "unsteady/square_cylinder"
     pywrapper_square_cylinder.cfg_file  = "turb_square.cfg"
     pywrapper_square_cylinder.test_iter = 10
-    pywrapper_square_cylinder.test_vals = [-1.178785, -0.349895, 1.401059, 2.358075, 1.401421, 2.301174, 0.000000]
+    pywrapper_square_cylinder.test_vals = [-1.178684, -0.349677, 1.401059, 2.358075, 1.401421, 2.301174, 0.000000]
     pywrapper_square_cylinder.command   = TestCase.Command("mpirun -np 2", "SU2_CFD.py", "--parallel -f")
     pywrapper_square_cylinder.unsteady  = True
     test_list.append(pywrapper_square_cylinder)

TestCases/parallel_regression_AD.py

@@ -230,8 +230,8 @@ def main():
     discadj_trans_stator.cfg_dir   = "disc_adj_turbomachinery/transonic_stator_2D"
     discadj_trans_stator.cfg_file  = "transonic_stator.cfg"
     discadj_trans_stator.test_iter = 79
-    discadj_trans_stator.test_vals = [79, 0.668058, 0.483608, 0.518789, -1.013227]
-    discadj_trans_stator.test_vals_aarch64 = [79, 0.668058, 0.483608, 0.518789, -1.013227]
+    discadj_trans_stator.test_vals = [79.000000, 0.667030, 0.483921, 0.518403, -1.013538]
+    discadj_trans_stator.test_vals_aarch64 = [79.000000, 0.667030, 0.483921, 0.518403, -1.013538]
     test_list.append(discadj_trans_stator)
 
     ###################################
@@ -256,7 +256,7 @@ def main():
     discadj_heat.cfg_dir   = "disc_adj_heat"
     discadj_heat.cfg_file  = "disc_adj_heat.cfg"
     discadj_heat.test_iter = 10
-    discadj_heat.test_vals         = [-1.999669, 0.657451, 0.000000, 0.006210]
+    discadj_heat.test_vals         = [-2.001337, 0.655543, 0.000000, 0.006170]
     discadj_heat.test_vals_aarch64 = [-2.226539, 0.605868, 0.000000, -6.256400]
     test_list.append(discadj_heat)
 
@@ -269,7 +269,7 @@ def main():
     discadj_fsi.cfg_dir   = "disc_adj_fsi"
     discadj_fsi.cfg_file  = "config.cfg"
     discadj_fsi.test_iter = 6
-    discadj_fsi.test_vals = [6.000000, -7.017319, -7.872545, 3.9968e-09, -2.4097e-05]
+    discadj_fsi.test_vals = [6.000000, -7.017369, -7.872619, 0.000000, -0.000024]
     test_list.append(discadj_fsi)
 
     # Multi physics framework
@@ -512,7 +512,7 @@ def main():
     pywrapper_wavy_wall_steady.cfg_dir = "py_wrapper/wavy_wall"
     pywrapper_wavy_wall_steady.cfg_file = "run_steady.py"
     pywrapper_wavy_wall_steady.test_iter = 100
-    pywrapper_wavy_wall_steady.test_vals = [-1.352680, 2.579322, -2.898321]
+    pywrapper_wavy_wall_steady.test_vals = [-1.353007, 2.581051, -2.900574]
     pywrapper_wavy_wall_steady.command = TestCase.Command("mpirun -n 2", "python", "run_steady.py")
     pywrapper_wavy_wall_steady.timeout = 1600
     pywrapper_wavy_wall_steady.tol = 0.00001

TestCases/serial_regression.py

@@ -174,15 +174,15 @@ def main():
     cylinder.cfg_dir   = "navierstokes/cylinder"
     cylinder.cfg_file  = "lam_cylinder.cfg"
     cylinder.test_iter = 25
-    cylinder.test_vals = [-8.363995, -2.882536, -0.017780, 1.607979, 0]
+    cylinder.test_vals = [-8.363897, -2.882485, -0.017777, 1.607978, 0.000000]
     test_list.append(cylinder)
 
     # Laminar cylinder (low Mach correction)
     cylinder_lowmach           = TestCase('cylinder_lowmach')
     cylinder_lowmach.cfg_dir   = "navierstokes/cylinder"
     cylinder_lowmach.cfg_file  = "cylinder_lowmach.cfg"
     cylinder_lowmach.test_iter = 25
-    cylinder_lowmach.test_vals = [-6.830989, -1.368842, -0.143838, 73.962440, 0]
+    cylinder_lowmach.test_vals = [-6.830989, -1.368842, -0.143868, 73.962350, 0.000000]
     test_list.append(cylinder_lowmach)
 
     # 2D Poiseuille flow (body force driven with periodic inlet / outlet)
@@ -275,7 +275,7 @@ def main():
     turb_naca0012_sa.cfg_dir   = "rans/naca0012"
     turb_naca0012_sa.cfg_file  = "turb_NACA0012_sa.cfg"
     turb_naca0012_sa.test_iter = 5
-    turb_naca0012_sa.test_vals = [-12.049550, -16.193702, 1.058588, 0.022984, 20.000000, -3.437275, 20.000000, -4.705227, 0.000000]
+    turb_naca0012_sa.test_vals = [-12.049543, -16.193702, 1.058588, 0.022984, 20.000000, -3.435258, 20.000000, -4.705244, 0.000000]
     turb_naca0012_sa.timeout   = 3200
     test_list.append(turb_naca0012_sa)
 
@@ -284,7 +284,7 @@ def main():
     turb_naca0012_sst.cfg_dir   = "rans/naca0012"
     turb_naca0012_sst.cfg_file  = "turb_NACA0012_sst.cfg"
     turb_naca0012_sst.test_iter = 10
-    turb_naca0012_sst.test_vals         = [ -12.079361, -15.284135, -5.859500, 1.048053, 0.019238, -3.272617, 0.000000]
+    turb_naca0012_sst.test_vals         = [ -12.078427, -15.284133, -5.859499, 1.048053, 0.019238, -3.274052, 0.000000]
     turb_naca0012_sst.test_vals_aarch64 = [-12.229890, -14.434837, -6.410709, 1.047444, 0.019214, -2.107944, 0.000000]
     turb_naca0012_sst.timeout   = 3200
     test_list.append(turb_naca0012_sst)
@@ -303,7 +303,7 @@ def main():
     turb_naca0012_sst_sust_restart.cfg_dir   = "rans/naca0012"
     turb_naca0012_sst_sust_restart.cfg_file  = "turb_NACA0012_sst_sust.cfg"
     turb_naca0012_sst_sust_restart.test_iter = 10
-    turb_naca0012_sst_sust_restart.test_vals = [-12.075450, -14.836721, -5.743110, 1.000050, 0.019144, -3.329048]
+    turb_naca0012_sst_sust_restart.test_vals = [12.075358, -14.836721, -5.743110, 1.000050, 0.019144, -3.328948]
     turb_naca0012_sst_sust_restart.test_vals_aarch64 = [-12.157374, -14.782027, -6.726462, 1.000270, 0.019123, -1.780624]
     turb_naca0012_sst_sust_restart.timeout   = 3200
     test_list.append(turb_naca0012_sst_sust_restart)
@@ -335,7 +335,7 @@ def main():
     axi_rans_air_nozzle_restart.cfg_dir   = "axisymmetric_rans/air_nozzle"
     axi_rans_air_nozzle_restart.cfg_file  = "air_nozzle_restart.cfg"
     axi_rans_air_nozzle_restart.test_iter = 10
-    axi_rans_air_nozzle_restart.test_vals = [-14.141446, -9.134033, -10.848810, -5.776634, 0.000000]
+    axi_rans_air_nozzle_restart.test_vals = [-14.141146, -9.130663, -10.848556, -5.776412, 0.000000]
     axi_rans_air_nozzle_restart.test_vals_aarch64 = [-12.067037, -6.840810, -8.843191, -3.783401, 0.000000]
     axi_rans_air_nozzle_restart.tol       = 0.0001
     test_list.append(axi_rans_air_nozzle_restart)
@@ -701,7 +701,7 @@ def main():
     turb_naca0012_p1c1.cfg_dir   = "rans_uq/naca0012"
     turb_naca0012_p1c1.cfg_file  = "turb_NACA0012_uq_p1c1.cfg"
     turb_naca0012_p1c1.test_iter = 10
-    turb_naca0012_p1c1.test_vals = [-5.119755, 1.283950, 0.486285, -0.021511]
+    turb_naca0012_p1c1.test_vals = [-5.119769, 1.283940, 0.486285, -0.021511]
     test_list.append(turb_naca0012_p1c1)
 
     # NACA0012 p1c2
@@ -769,7 +769,7 @@ def main():
     square_cylinder.cfg_dir   = "unsteady/square_cylinder"
     square_cylinder.cfg_file  = "turb_square.cfg"
     square_cylinder.test_iter = 3
-    square_cylinder.test_vals = [-2.560839, -1.175927, 0.062095, 1.399401, 2.220371, 1.399349, 2.218609, 0.000000]
+    square_cylinder.test_vals = [-2.560665, -1.175914, 0.062108, 1.399401, 2.220371, 1.399349, 2.218609, 0.000000]
     square_cylinder.unsteady  = True
     test_list.append(square_cylinder)
 
@@ -1529,7 +1529,7 @@ def main():
     pywrapper_turb_naca0012_sst.cfg_dir   = "rans/naca0012"
     pywrapper_turb_naca0012_sst.cfg_file  = "turb_NACA0012_sst.cfg"
     pywrapper_turb_naca0012_sst.test_iter = 10
-    pywrapper_turb_naca0012_sst.test_vals         = [-12.079361, -15.284135, -5.859500, 1.048053, 0.019238, -3.272617, 0.000000]
+    pywrapper_turb_naca0012_sst.test_vals         = [-12.078427, -15.284133, -5.859499, 1.048053, 0.019238, -3.274052, 0.000000]
     pywrapper_turb_naca0012_sst.test_vals_aarch64 = [-12.229889, -14.434883, -6.037177, 1.047444, 0.019214, -2.108366, 0.000000]
     pywrapper_turb_naca0012_sst.command   =  TestCase.Command(exec = "SU2_CFD.py", param = "-f")
     pywrapper_turb_naca0012_sst.timeout   = 3200
@@ -1543,7 +1543,7 @@ def main():
     pywrapper_square_cylinder.cfg_dir   = "unsteady/square_cylinder"
     pywrapper_square_cylinder.cfg_file  = "turb_square.cfg"
     pywrapper_square_cylinder.test_iter = 3
-    pywrapper_square_cylinder.test_vals = [-2.560839, -1.175927, 0.062095, 1.399401, 2.220371, 1.399349, 2.218609, 0.000000]
+    pywrapper_square_cylinder.test_vals = [2.560665, -1.175914, 0.062108, 1.399401, 2.220371, 1.399349, 2.218609, 0.000000]
     pywrapper_square_cylinder.command   =  TestCase.Command(exec = "SU2_CFD.py", param = "-f")
     pywrapper_square_cylinder.timeout   = 1600
     pywrapper_square_cylinder.tol       = 0.00001

TestCases/serial_regression_AD.py

@@ -193,7 +193,7 @@ def main():
     discadj_heat.cfg_dir   = "disc_adj_heat"
     discadj_heat.cfg_file  = "disc_adj_heat.cfg"
     discadj_heat.test_iter = 10
-    discadj_heat.test_vals = [-2.174674, 0.581857, 0.000000, 0.008748]
+    discadj_heat.test_vals = [-2.178141, 0.578576, 0.000000, 0.008712]
     test_list.append(discadj_heat)
 
     ###################################
@@ -205,7 +205,7 @@ def main():
     discadj_fsi.cfg_dir   = "disc_adj_fsi"
     discadj_fsi.cfg_file  = "config.cfg"
     discadj_fsi.test_iter = 6
-    discadj_fsi.test_vals = [6.000000, -8.928327, -10.009868, 3.1056e-11, -1.7613e-06]
+    discadj_fsi.test_vals = [6.000000, -8.929426, -10.024862, 0.000000, -0.000002]
     test_list.append(discadj_fsi)
 
     ###################################