initial commit to add heat flux to some regressions

Author: WallyMaier

TestCases/hybrid_regression.py

@@ -254,8 +254,8 @@ def main():
     axi_rans_air_nozzle.cfg_dir   = "axisymmetric_rans/air_nozzle"
     axi_rans_air_nozzle.cfg_file  = "air_nozzle.cfg"
     axi_rans_air_nozzle.test_iter = 10
-    axi_rans_air_nozzle.test_vals         = [-12.093575, -6.630426, -8.798725, -2.399130]
-    axi_rans_air_nozzle.test_vals_aarch64 = [-12.093539, -6.630357, -8.798732, -2.399130]
+    axi_rans_air_nozzle.test_vals         = [-12.093575, -6.630426, -8.798725, -2.399130, 0.0]
+    axi_rans_air_nozzle.test_vals_aarch64 = [-12.093539, -6.630357, -8.798732, -2.399130, 0.0]
     test_list.append(axi_rans_air_nozzle)
 
     #################################
@@ -392,8 +392,8 @@ def main():
     inc_poly_cylinder.cfg_dir   = "incomp_navierstokes/cylinder"
     inc_poly_cylinder.cfg_file  = "poly_cylinder.cfg"
     inc_poly_cylinder.test_iter = 20
-    inc_poly_cylinder.test_vals         = [-7.851512, -2.093420, 0.029974, 1.921595]
-    inc_poly_cylinder.test_vals_aarch64 = [-7.851510, -2.093419, 0.029974, 1.921595]
+    inc_poly_cylinder.test_vals         = [-7.851512, -2.093420, 0.029974, 1.921595, 0.0]
+    inc_poly_cylinder.test_vals_aarch64 = [-7.851510, -2.093419, 0.029974, 1.921595, 0.0]
     inc_poly_cylinder.new_output  = True
     test_list.append(inc_poly_cylinder)
 
@@ -424,7 +424,7 @@ def main():
     inc_turb_naca0012_sst_sust.cfg_dir   = "incomp_rans/naca0012"
     inc_turb_naca0012_sst_sust.cfg_file  = "naca0012_SST_SUST.cfg"
     inc_turb_naca0012_sst_sust.test_iter = 20
-    inc_turb_naca0012_sst_sust.test_vals = [-7.276424, 0.145860, 0.000003, 0.312011]
+    inc_turb_naca0012_sst_sust.test_vals = [-7.276424, 0.145860, 0.000003, 0.312011, 0.0]
     test_list.append(inc_turb_naca0012_sst_sust)
 
     ######################################
@@ -486,7 +486,7 @@ def main():
     ddes_flatplate.cfg_dir   = "ddes/flatplate"
     ddes_flatplate.cfg_file  = "ddes_flatplate.cfg"
     ddes_flatplate.test_iter = 10
-    ddes_flatplate.test_vals = [-2.714758, -5.883004, -0.215005, 0.023783]
+    ddes_flatplate.test_vals = [-2.714758, -5.883004, -0.215005, 0.023783, 0.0]
     ddes_flatplate.unsteady  = True
     test_list.append(ddes_flatplate)
 

TestCases/parallel_regression.py

@@ -97,8 +97,8 @@ def main():
     visc_cone.cfg_dir   = "nonequilibrium/axi_visccone"
     visc_cone.cfg_file  = "axi_visccone.cfg"
     visc_cone.test_iter = 10
-    visc_cone.test_vals         = [-5.222278, -5.746529, -20.569425, -20.633787, -20.547644, -1.928717, -2.247306, 1.255759, -3.208374]
-    visc_cone.test_vals_aarch64 = [-5.222267, -5.746522, -20.569408, -20.633783, -20.546393, -1.928714, -2.247317, 1.255761, -3.208360]
+    visc_cone.test_vals         = [-5.222278, -5.746529, -20.569425, -20.633787, -20.547644, -1.928717, -2.247306, 1.255759, -3.208374, 0.0]
+    visc_cone.test_vals_aarch64 = [-5.222267, -5.746522, -20.569408, -20.633783, -20.546393, -1.928714, -2.247317, 1.255761, -3.208360, 0.0]
     visc_cone.su2_exec  = "mpirun -n 2 SU2_CFD"
     visc_cone.timeout   = 1600
     visc_cone.new_output = True
@@ -254,7 +254,7 @@ def main():
     cylinder_lowmach.cfg_dir   = "navierstokes/cylinder"
     cylinder_lowmach.cfg_file  = "cylinder_lowmach.cfg"
     cylinder_lowmach.test_iter = 25
-    cylinder_lowmach.test_vals = [-6.858484, -1.396528, -1.854558, 110.033249]
+    cylinder_lowmach.test_vals = [-6.858484, -1.396528, -1.854558, 110.033249, 0.0]
     cylinder_lowmach.su2_exec  = "parallel_computation.py -f"
     cylinder_lowmach.timeout   = 1600
     cylinder_lowmach.tol       = 0.00001
@@ -292,7 +292,7 @@ def main():
     rae2822_sa.cfg_dir   = "rans/rae2822"
     rae2822_sa.cfg_file  = "turb_SA_RAE2822.cfg"
     rae2822_sa.test_iter = 20
-    rae2822_sa.test_vals = [-2.004689, -5.265793, 0.809463, 0.062016]
+    rae2822_sa.test_vals = [-2.004689, -5.265793, 0.809463, 0.062016, 0.0]
     rae2822_sa.su2_exec  = "parallel_computation.py -f"
     rae2822_sa.timeout   = 1600
     rae2822_sa.tol       = 0.00001
@@ -303,7 +303,7 @@ def main():
     rae2822_sst.cfg_dir   = "rans/rae2822"
     rae2822_sst.cfg_file  = "turb_SST_RAE2822.cfg"
     rae2822_sst.test_iter = 20
-    rae2822_sst.test_vals = [-0.510641, 4.870022, 0.813722, 0.062439]
+    rae2822_sst.test_vals = [-0.510641, 4.870022, 0.813722, 0.062439, 0.0]
     rae2822_sst.su2_exec  = "parallel_computation.py -f"
     rae2822_sst.timeout   = 1600
     rae2822_sst.tol       = 0.00001
@@ -369,7 +369,7 @@ def main():
     turb_naca0012_sa.cfg_dir   = "rans/naca0012"
     turb_naca0012_sa.cfg_file  = "turb_NACA0012_sa.cfg"
     turb_naca0012_sa.test_iter = 10
-    turb_naca0012_sa.test_vals = [-8.621456, -10.378269, 1.064502, 0.019710, 20.000000, -1.811700, 20.000000, -5.171326]
+    turb_naca0012_sa.test_vals = [-8.621456, -10.378269, 1.064502, 0.019710, 20.000000, -1.811700, 20.000000, -5.171326, 0.0]
     turb_naca0012_sa.su2_exec  = "parallel_computation.py -f"
     turb_naca0012_sa.timeout   = 3200
     turb_naca0012_sa.tol       = 0.00001
@@ -380,7 +380,7 @@ 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 = [-11.456387, -12.800055, -5.865784, 1.049989, 0.019163, -1.838252]
+    turb_naca0012_sst.test_vals = [-11.456387, -12.800055, -5.865784, 1.049989, 0.019163, -1.838252, 0.0]
     turb_naca0012_sst.su2_exec  = "parallel_computation.py -f"
     turb_naca0012_sst.timeout   = 3200
     turb_naca0012_sst.tol       = 0.00001
@@ -462,7 +462,7 @@ def main():
     axi_rans_air_nozzle.cfg_dir   = "axisymmetric_rans/air_nozzle"
     axi_rans_air_nozzle.cfg_file  = "air_nozzle.cfg"
     axi_rans_air_nozzle.test_iter = 10
-    axi_rans_air_nozzle.test_vals = [-12.096377, -6.636625, -8.786639, -2.399099]
+    axi_rans_air_nozzle.test_vals = [-12.096377, -6.636625, -8.786639, -2.399099, 0.0]
     axi_rans_air_nozzle.su2_exec  = "mpirun -n 2 SU2_CFD"
     axi_rans_air_nozzle.timeout   = 1600
     axi_rans_air_nozzle.tol       = 0.0001
@@ -519,7 +519,7 @@ def main():
     inc_lam_cylinder.cfg_dir   = "incomp_navierstokes/cylinder"
     inc_lam_cylinder.cfg_file  = "incomp_cylinder.cfg"
     inc_lam_cylinder.test_iter = 10
-    inc_lam_cylinder.test_vals = [-4.004072, -3.194881, -0.076553, 7.780048]
+    inc_lam_cylinder.test_vals = [-4.004072, -3.194881, -0.076553, 7.780048, 0.0]
     inc_lam_cylinder.su2_exec  = "parallel_computation.py -f"
     inc_lam_cylinder.timeout   = 1600
     inc_lam_cylinder.tol       = 0.00001
@@ -552,7 +552,7 @@ def main():
     inc_lam_bend.cfg_dir   = "incomp_navierstokes/bend"
     inc_lam_bend.cfg_file  = "lam_bend.cfg"
     inc_lam_bend.test_iter = 10
-    inc_lam_bend.test_vals = [-3.447746, -3.085237, -0.020816, 1.147373]
+    inc_lam_bend.test_vals = [-3.447746, -3.085237, -0.020816, 1.147373, 0.0]
     inc_lam_bend.su2_exec  = "mpirun -n 2 SU2_CFD"
     inc_lam_bend.timeout   = 1600
     inc_lam_bend.tol       = 0.00001
@@ -600,7 +600,7 @@ def main():
     inc_turb_naca0012_sst_sust.cfg_dir   = "incomp_rans/naca0012"
     inc_turb_naca0012_sst_sust.cfg_file  = "naca0012_SST_SUST.cfg"
     inc_turb_naca0012_sst_sust.test_iter = 20
-    inc_turb_naca0012_sst_sust.test_vals = [-7.276430, 0.145859, -0.000001, 0.312020]
+    inc_turb_naca0012_sst_sust.test_vals = [-7.276430, 0.145859, -0.000001, 0.312020, 0.0]
     inc_turb_naca0012_sst_sust.su2_exec  = "parallel_computation.py -f"
     inc_turb_naca0012_sst_sust.timeout   = 1600
     inc_turb_naca0012_sst_sust.tol       = 0.00001
@@ -714,8 +714,8 @@ 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         = [-1.355605, 1.464131, 1.314243, -1.997959, 1.135210, 0.398906]
-    turbmod_sa_neg_rae2822.test_vals_aarch64 = [-1.298704, 1.476866, 1.303138, 0.694951, 1.397494, 0.534572]
+    turbmod_sa_neg_rae2822.test_vals         = [-1.355605, 1.464131, 1.314243, -1.997959, 1.135210, 0.398906, 0.0]
+    turbmod_sa_neg_rae2822.test_vals_aarch64 = [-1.298704, 1.476866, 1.303138, 0.694951, 1.397494, 0.534572, 0.0]
     turbmod_sa_neg_rae2822.su2_exec  = "mpirun -n 2 SU2_CFD"
     turbmod_sa_neg_rae2822.timeout   = 1600
     turbmod_sa_neg_rae2822.new_output = True
@@ -779,7 +779,7 @@ def main():
     schubauer_klebanoff_transition.cfg_dir      = "transition/Schubauer_Klebanoff"
     schubauer_klebanoff_transition.cfg_file     = "transitional_BC_model_ConfigFile.cfg"
     schubauer_klebanoff_transition.test_iter    = 10
-    schubauer_klebanoff_transition.test_vals    = [-7.994740, -13.240225, 0.000046, 0.007987]
+    schubauer_klebanoff_transition.test_vals    = [-7.994740, -13.240225, 0.000046, 0.007987, 0.0]
     schubauer_klebanoff_transition.su2_exec     = "parallel_computation.py -f"
     schubauer_klebanoff_transition.timeout      = 1600
     schubauer_klebanoff_transition.tol          = 0.00001
@@ -1044,7 +1044,7 @@ 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 = [-1.162664, 0.066378, 1.399789, 2.220404, 1.399743, 2.218605]
+    square_cylinder.test_vals = [-1.162664, 0.066378, 1.399789, 2.220404, 1.399743, 2.218605, 0.0]
     square_cylinder.su2_exec  = "parallel_computation.py -f"
     square_cylinder.timeout   = 1600
     square_cylinder.tol       = 0.00001
@@ -1080,7 +1080,7 @@ def main():
     ddes_flatplate.cfg_dir   = "ddes/flatplate"
     ddes_flatplate.cfg_file  = "ddes_flatplate.cfg"
     ddes_flatplate.test_iter = 10
-    ddes_flatplate.test_vals = [-2.714758, -5.883004, -0.215005, 0.023783] #last 4 columns
+    ddes_flatplate.test_vals = [-2.714758, -5.883004, -0.215005, 0.023783, 0.0] #last 4 columns
     ddes_flatplate.su2_exec  = "parallel_computation.py -f"
     ddes_flatplate.timeout   = 1600
     ddes_flatplate.tol       = 0.00001
@@ -1409,7 +1409,7 @@ def main():
     p1rad.cfg_file  = "configp1.cfg"
     p1rad.new_output= True
     p1rad.test_iter = 100
-    p1rad.test_vals = [-7.743666, -7.921411, -2.111848, 0.098302] #last 4 columns
+    p1rad.test_vals = [-7.743666, -7.921411, -2.111848, 0.098302, 0.0] #last 4 columns
     p1rad.su2_exec  = "mpirun -n 2 SU2_CFD"
     p1rad.timeout   = 1600
     p1rad.tol       = 0.00001
@@ -1425,8 +1425,8 @@ def main():
     solid_periodic_pins.cfg_dir   = "solid_heat_conduction/periodic_pins"
     solid_periodic_pins.cfg_file  = "configSolid.cfg"
     solid_periodic_pins.test_iter = 750
-    solid_periodic_pins.test_vals         = [-15.878958, -14.569206, 300.900000, 425.320000, 0.000000, 5.000000, -1.672714] #last 7 lines
-    solid_periodic_pins.test_vals_aarch64 = [-15.879010, -14.569206, 300.900000, 425.320000, 0.000000, 5.000000, -1.672630] #last 7 lines
+    solid_periodic_pins.test_vals         = [-15.878958, -14.569206, 300.900000, 425.320000, 0.000000, 5.000000, -1.672714, 0.0] #last 7 lines
+    solid_periodic_pins.test_vals_aarch64 = [-15.879010, -14.569206, 300.900000, 425.320000, 0.000000, 5.000000, -1.672630, 0.0] #last 7 lines
     solid_periodic_pins.su2_exec  = "mpirun -n 2 SU2_CFD"
     solid_periodic_pins.timeout   = 1600
     solid_periodic_pins.tol       = 0.00001
@@ -1441,7 +1441,7 @@ def main():
     cht_incompressible.cfg_dir   = "coupled_cht/incomp_2d"
     cht_incompressible.cfg_file  = "cht_2d_3cylinders.cfg"
     cht_incompressible.test_iter = 10
-    cht_incompressible.test_vals = [-2.128826, -0.588813, -0.588813, -0.588813] #last 4 columns
+    cht_incompressible.test_vals = [-2.128826, -0.588813, -0.588813, -0.588813, 0.0] #last 4 columns
     cht_incompressible.su2_exec  = "SU2_CFD"
     cht_incompressible.timeout   = 1600
     cht_incompressible.multizone = True
@@ -1477,8 +1477,8 @@ def main():
     sp_pinArray_3d_cht_mf_hf_tp.cfg_dir   = "incomp_navierstokes/streamwise_periodic/chtPinArray_3d"
     sp_pinArray_3d_cht_mf_hf_tp.cfg_file  = "configMaster.cfg"
     sp_pinArray_3d_cht_mf_hf_tp.test_iter = 30
-    sp_pinArray_3d_cht_mf_hf_tp.test_vals         = [-13.374306, -7.476945, -7.025285, -0.009675, 99.879812, 419.200000]
-    sp_pinArray_3d_cht_mf_hf_tp.test_vals_aarch64 = [-13.400623, -7.476945, -7.025285, -0.009675, 99.879812, 419.200000]
+    sp_pinArray_3d_cht_mf_hf_tp.test_vals         = [-13.374306, -7.476945, -7.025285, -0.009675, 99.879812, 419.200000, 0.0]
+    sp_pinArray_3d_cht_mf_hf_tp.test_vals_aarch64 = [-13.400623, -7.476945, -7.025285, -0.009675, 99.879812, 419.200000, 0.0]
     sp_pinArray_3d_cht_mf_hf_tp.su2_exec  = "mpirun -n 2 SU2_CFD"
     sp_pinArray_3d_cht_mf_hf_tp.timeout   = 1600
     sp_pinArray_3d_cht_mf_hf_tp.tol       = 0.00001

TestCases/serial_regression.py

@@ -82,8 +82,8 @@ def main():
     visc_cone.cfg_dir   = "nonequilibrium/axi_visccone"
     visc_cone.cfg_file  = "axi_visccone.cfg"
     visc_cone.test_iter = 10
-    visc_cone.test_vals         = [-5.215236, -5.739371, -20.545048, -20.618700, -20.502532, -1.917617, -2.239664, 1.262783, -3.205463]
-    visc_cone.test_vals_aarch64 = [-5.215236, -5.739371, -20.545048, -20.618697, -20.501528, -1.917617, -2.239664, 1.262783, -3.205463]
+    visc_cone.test_vals         = [-5.215236, -5.739371, -20.545048, -20.618700, -20.502532, -1.917617, -2.239664, 1.262783, -3.205463, 0.0]
+    visc_cone.test_vals_aarch64 = [-5.215236, -5.739371, -20.545048, -20.618697, -20.501528, -1.917617, -2.239664, 1.262783, -3.205463, 0.0]
     visc_cone.su2_exec  = "SU2_CFD"
     visc_cone.timeout   = 1600
     visc_cone.new_output = True
@@ -217,7 +217,7 @@ def main():
     cylinder.cfg_dir   = "navierstokes/cylinder"
     cylinder.cfg_file  = "lam_cylinder.cfg"
     cylinder.test_iter = 25
-    cylinder.test_vals = [-6.765430, -1.297426, 0.019508, 0.310015] #last 4 columns
+    cylinder.test_vals = [-6.765430, -1.297426, 0.019508, 0.310015, 0.0] #last 4 columns
     cylinder.su2_exec  = "SU2_CFD"
     cylinder.new_output = True
     cylinder.timeout   = 1600
@@ -241,7 +241,7 @@ def main():
     poiseuille.cfg_dir   = "navierstokes/poiseuille"
     poiseuille.cfg_file  = "lam_poiseuille.cfg"
     poiseuille.test_iter = 10
-    poiseuille.test_vals = [-5.050732, 0.648355, 0.012273, 13.643219] #last 4 columns
+    poiseuille.test_vals = [-5.050732, 0.648355, 0.012273, 13.643219, 0.0] #last 4 columns
     poiseuille.su2_exec  = "SU2_CFD"
     poiseuille.new_output = True
     poiseuille.timeout   = 1600
@@ -278,7 +278,7 @@ def main():
     rae2822_sa.cfg_dir   = "rans/rae2822"
     rae2822_sa.cfg_file  = "turb_SA_RAE2822.cfg"
     rae2822_sa.test_iter = 20
-    rae2822_sa.test_vals = [-2.020123, -5.269330, 0.807147, 0.060499]
+    rae2822_sa.test_vals = [-2.020123, -5.269330, 0.807147, 0.060499, 0.0]
     rae2822_sa.su2_exec  = "SU2_CFD"
     rae2822_sa.timeout   = 1600
     rae2822_sa.new_output = True
@@ -290,7 +290,7 @@ def main():
     rae2822_sst.cfg_dir   = "rans/rae2822"
     rae2822_sst.cfg_file  = "turb_SST_RAE2822.cfg"
     rae2822_sst.test_iter = 20
-    rae2822_sst.test_vals = [-0.510639, 4.872266, 0.812659, 0.061095]
+    rae2822_sst.test_vals = [-0.510639, 4.872266, 0.812659, 0.061095, 0.0]
     rae2822_sst.su2_exec  = "SU2_CFD"
     rae2822_sst.new_output = True
     rae2822_sst.timeout   = 1600
@@ -347,7 +347,7 @@ def main():
     turb_oneram6.cfg_dir   = "rans/oneram6"
     turb_oneram6.cfg_file  = "turb_ONERAM6.cfg"
     turb_oneram6.test_iter = 10
-    turb_oneram6.test_vals = [-2.388841, -6.689414, 0.230321, 0.157640]#last 4 columns
+    turb_oneram6.test_vals = [-2.388841, -6.689414, 0.230321, 0.157640, 0.0]#last 4 columns
     turb_oneram6.su2_exec  = "SU2_CFD"
     turb_oneram6.new_output = True
     turb_oneram6.timeout   = 3200
@@ -384,7 +384,7 @@ def main():
     turb_naca0012_sst_2003m.cfg_dir   = "rans/naca0012"
     turb_naca0012_sst_2003m.cfg_file  = "turb_NACA0012_sst_2003m.cfg"
     turb_naca0012_sst_2003m.test_iter = 10
-    turb_naca0012_sst_2003m.test_vals = [-7.698435, -10.060146, -3.421602, 1.049412, 0.019691, -2.193389]
+    turb_naca0012_sst_2003m.test_vals = [-7.698435, -10.060146, -3.421602, 1.049412, 0.019691, -2.193389, 0.0]
     turb_naca0012_sst_2003m.su2_exec  = "SU2_CFD"
     turb_naca0012_sst_2003m.new_output  = True
     turb_naca0012_sst_2003m.timeout   = 3200
@@ -434,7 +434,7 @@ def main():
     axi_rans_air_nozzle.cfg_dir   = "axisymmetric_rans/air_nozzle"
     axi_rans_air_nozzle.cfg_file  = "air_nozzle.cfg"
     axi_rans_air_nozzle.test_iter = 10
-    axi_rans_air_nozzle.test_vals = [ -12.092891, -6.630495, -8.784840, -2.399099]
+    axi_rans_air_nozzle.test_vals = [ -12.092891, -6.630495, -8.784840, -2.399099, 0.0]
     axi_rans_air_nozzle.su2_exec  = "SU2_CFD"
     axi_rans_air_nozzle.timeout   = 1600
     axi_rans_air_nozzle.tol       = 0.0001
@@ -510,7 +510,7 @@ def main():
     inc_lam_cylinder.cfg_dir   = "incomp_navierstokes/cylinder"
     inc_lam_cylinder.cfg_file  = "incomp_cylinder.cfg"
     inc_lam_cylinder.test_iter = 10
-    inc_lam_cylinder.test_vals = [-4.004277, -3.227956, 0.003852, 7.626578] #last 4 columns
+    inc_lam_cylinder.test_vals = [-4.004277, -3.227956, 0.003852, 7.626578, 0.0] #last 4 columns
     inc_lam_cylinder.new_output  = True
     inc_lam_cylinder.su2_exec  = "SU2_CFD"
     inc_lam_cylinder.timeout   = 1600
@@ -534,7 +534,7 @@ def main():
     inc_poly_cylinder.cfg_dir   = "incomp_navierstokes/cylinder"
     inc_poly_cylinder.cfg_file  = "poly_cylinder.cfg"
     inc_poly_cylinder.test_iter = 20
-    inc_poly_cylinder.test_vals = [-8.106741, -2.160042, 0.019225, 1.902421] #last 4 columns
+    inc_poly_cylinder.test_vals = [-8.106741, -2.160042, 0.019225, 1.902421, 0.0] #last 4 columns
     inc_poly_cylinder.new_output  = True
     inc_poly_cylinder.su2_exec  = "SU2_CFD"
     inc_poly_cylinder.timeout   = 1600
@@ -569,7 +569,7 @@ def main():
     inc_turb_naca0012.cfg_dir   = "incomp_rans/naca0012"
     inc_turb_naca0012.cfg_file  = "naca0012.cfg"
     inc_turb_naca0012.test_iter = 20
-    inc_turb_naca0012.test_vals = [-4.788495, -11.040511, 0.000023, 0.309503] #last 4 columns
+    inc_turb_naca0012.test_vals = [-4.788495, -11.040511, 0.000023, 0.309503, 0.0] #last 4 columns
     inc_turb_naca0012.new_output  = True
     inc_turb_naca0012.su2_exec  = "SU2_CFD"
     inc_turb_naca0012.timeout   = 1600
@@ -592,7 +592,7 @@ def main():
     inc_turb_wallfunction_flatplate_sst.cfg_dir   = "wallfunctions/flatplate/incompressible_SST"
     inc_turb_wallfunction_flatplate_sst.cfg_file  = "turb_SST_flatplate.cfg"
     inc_turb_wallfunction_flatplate_sst.test_iter = 10
-    inc_turb_wallfunction_flatplate_sst.test_vals = [-6.561293, -5.730190, -6.305916, -4.230297, -7.164083, -2.047256, 10, -2.941818, 0.000974, 0.003195] #last 10 columns
+    inc_turb_wallfunction_flatplate_sst.test_vals = [-6.561293, -5.730190, -6.305916, -4.230297, -7.164083, -2.047256, 10, -2.941818, 0.000974, 0.003195, 0.0] #last 10 columns
     inc_turb_wallfunction_flatplate_sst.su2_exec  = "SU2_CFD"
     inc_turb_wallfunction_flatplate_sst.timeout   = 1600
     inc_turb_wallfunction_flatplate_sst.tol       = 0.00001