new config for transonic_stator AD and more regression updates

Author: Bot-Enigma-0

TestCases/disc_adj_turbomachinery/transonic_stator_2D/transonic_stator.cfg

@@ -169,6 +169,24 @@ CONV_STARTITER= 10
 CONV_CAUCHY_ELEMS= 100
 CONV_CAUCHY_EPS= 1E-6
 
+% ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
+%
+CONV_NUM_METHOD_ADJFLOW= ROE
+MUSCL_ADJFLOW= NO
+TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
+RELAXATION_FACTOR_ADJOINT= 0.1
+QUASI_NEWTON_NUM_SAMPLES= 20
+CFL_REDUCTION_ADJFLOW= 0.4
+FROZEN_VISC_DISC= YES
+INCONSISTENT_DISC= YES
+
+% ---------------- ADJOINT-TURBULENT NUMERICAL METHOD DEFINITION --------------%
+%
+CONV_NUM_METHOD_ADJTURB= SCALAR_UPWIND
+TIME_DISCRE_ADJTURB= EULER_IMPLICIT
+CFL_REDUCTION_ADJTURB= 0.01
+MUSCL_ADJTURB= NO
+
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
 MESH_FILENAME= mesh_stator_turb.su2

TestCases/hybrid_regression.py

@@ -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 = [-12.065954, -6.836372, -8.889803, -3.832665, 0.000000]
+    axi_rans_air_nozzle_restart.test_vals = [-14.137579, -9.105575, -10.894183, -5.810269, 0.000000]
     test_list.append(axi_rans_air_nozzle_restart)
 
     #################################

TestCases/parallel_regression.py

@@ -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 = [-14.803856, -9.213258, 0.478298, 6.060787, 0.000000]
+    axi_rans_air_nozzle_restart.test_vals = [-14.140338, -9.122501, -10.859866, -5.788769, 0.000000]
     axi_rans_air_nozzle_restart.tol       = 0.0001
     test_list.append(axi_rans_air_nozzle_restart)
 

TestCases/parallel_regression_AD.py

@@ -150,7 +150,7 @@ def main():
     discadj_axisymmetric_rans_nozzle.cfg_dir    = "axisymmetric_rans/air_nozzle"
     discadj_axisymmetric_rans_nozzle.cfg_file   = "air_nozzle_restart.cfg"
     discadj_axisymmetric_rans_nozzle.test_iter  = 10
-    discadj_axisymmetric_rans_nozzle.test_vals  = [9.748075, 5.149375, 7.147505, 2.805312]
+    discadj_axisymmetric_rans_nozzle.test_vals  = [ 9.748080, 5.149371, 7.147528, 2.805292]
     discadj_axisymmetric_rans_nozzle.no_restart = True
     test_list.append(discadj_axisymmetric_rans_nozzle)
 
@@ -299,7 +299,7 @@ def main():
     da_sp_pinArray_cht_2d_dp_hf.cfg_dir   = "incomp_navierstokes/streamwise_periodic/chtPinArray_2d"
     da_sp_pinArray_cht_2d_dp_hf.cfg_file  = "DA_configMaster.cfg"
     da_sp_pinArray_cht_2d_dp_hf.test_iter = 100
-    da_sp_pinArray_cht_2d_dp_hf.test_vals = [-4.755247, -4.057866, -4.137464]
+    da_sp_pinArray_cht_2d_dp_hf.test_vals = [-5.081814, -3.881868, -4.127717]
     da_sp_pinArray_cht_2d_dp_hf.multizone = True
     test_list.append(da_sp_pinArray_cht_2d_dp_hf)
 

TestCases/serial_regression.py

@@ -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 = [-12.067274, -6.841605, -8.843340, -3.783551, 0.000000]
+    axi_rans_air_nozzle_restart.test_vals = [-14.141446, -9.134033, -10.848810, -5.776634, 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)