update parallel regression

Author: bigfooted

SU2_CFD/include/numerics/turbulent/turb_sources.hpp

@@ -715,7 +715,6 @@ class CSourcePieceWise_TurbSST final : public CNumerics {
     AD::SetPreaccIn(PrimVar_Grad_i, nDim + idx.Velocity(), nDim);
     AD::SetPreaccIn(Vorticity_i, 3);
     AD::SetPreaccIn(V_i[idx.Density()], V_i[idx.LaminarViscosity()], V_i[idx.EddyViscosity()]);
-    //AD::SetPreaccIn(Coord_i[1]);
     AD::SetPreaccIn(V_i[idx.Velocity() + 1]);
 
     Density_i = V_i[idx.Density()];

SU2_CFD/include/solvers/CFVMFlowSolverBase.inl

@@ -613,9 +613,9 @@ void CFVMFlowSolverBase<V, R>::ComputeVorticityAndStrainMag(const CConfig& confi
 
     const su2double vy = nodes->GetVelocity(iPoint, 1);
     const su2double y = geometry->nodes->GetCoord(iPoint, 1);
-    //AD::StartPreacc();
-    //AD::SetPreaccIn(VelocityGradient, nDim, nDim);
-    //AD::SetPreaccIn(vy, y);
+    AD::StartPreacc();
+    AD::SetPreaccIn(VelocityGradient, nDim, nDim);
+    AD::SetPreaccIn(vy, y);
 
     StrainMag(iPoint) = 0.0;
 
@@ -638,7 +638,7 @@ void CFVMFlowSolverBase<V, R>::ComputeVorticityAndStrainMag(const CConfig& confi
     }
 
     StrainMag(iPoint) = sqrt(2.0*StrainMag(iPoint));
-    //AD::SetPreaccOut(StrainMag(iPoint));
+    AD::SetPreaccOut(StrainMag(iPoint));
 
     /*--- Max is not differentiable, so we not register them for preacc. ---*/
     strainMax = max(strainMax, StrainMag(iPoint));

TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/of_grad_findiff.csv.ref

@@ -1,2 +1,2 @@
 "VARIABLE"      , "AVG_DENSITY[0]", "AVG_ENTHALPY[0]", "AVG_NORMALVEL[0]", "DRAG[0]"       , "EFFICIENCY[0]" , "FORCE_X[0]"    , "FORCE_Y[0]"    , "FORCE_Z[0]"    , "LIFT[0]"       , "MOMENT_X[0]"   , "MOMENT_Y[0]"   , "MOMENT_Z[0]"   , "SIDEFORCE[0]"  , "SURFACE_MACH[0]", "SURFACE_MASSFLOW[0]", "SURFACE_MOM_DISTORTION[0]", "SURFACE_PRESSURE_DROP[0]", "SURFACE_SECONDARY[0]", "SURFACE_SECOND_OVER_UNIFORM[0]", "SURFACE_STATIC_PRESSURE[0]", "SURFACE_STATIC_TEMPERATURE[0]", "SURFACE_TOTAL_PRESSURE[0]", "SURFACE_TOTAL_TEMPERATURE[0]", "SURFACE_UNIFORMITY[0]", "AVG_TEMPERATURE[1]", "MAXIMUM_HEATFLUX[1]", "TOTAL_HEATFLUX[1]", "FINDIFF_STEP"  
-0               , 0.0             , -99999.96982514858, -2.2204000000409886e-08, 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , -0.04000000053405728, 0.0                , -2.060000001136153       , 0.0                     , 2.12000000054946    , 3.700000000828041             , 330.00000030369847        , -30.00000106112566           , 314.99999977313564       , -30.00000106112566          , -1.400000004814217   , -140.0000030571391, 0.0                , -509.99999530176865, 1e-08           
++0               , 0.0             , -100000.01639127731, -1.1101999999881826e-08, 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , 0.0             , -0.0399999991462785, 0.0                , -2.1099999997220564      , 0.0                     , 2.1799999999627673  , 3.8000000007754053            , 319.9999980552093         , -39.999997625272954          , 318.0000007318995        , -39.999997625272954         , -1.400000004814217   , -139.99999737279722, 0.0                , -540.0000077315781, 1e-08

TestCases/parallel_regression.py

@@ -394,7 +394,7 @@ 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 = [-12.096361, -6.636587, -8.786643, -2.399099, -1938.200000]
+    axi_rans_air_nozzle.test_vals = [-1.619755, 3.971206, -7.170784, 4.821522, 66.092000]
     axi_rans_air_nozzle.tol       = 0.0001
     test_list.append(axi_rans_air_nozzle)
 
@@ -403,7 +403,7 @@ 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 = [-12.096361, -6.636587, -8.786643, -2.399099, -1938.200000]
+    axi_rans_air_nozzle_restart.test_vals = [-2.211671, 3.475255, -6.023273, 4.454529, 195.920000]
     axi_rans_air_nozzle_restart.tol       = 0.0001
     test_list.append(axi_rans_air_nozzle_restart)
 
@@ -932,7 +932,7 @@ def main():
     Jones_tc.cfg_dir   = "turbomachinery/APU_turbocharger"
     Jones_tc.cfg_file  = "Jones.cfg"
     Jones_tc.test_iter = 5
-    Jones_tc.test_vals = [5.283772, 0.374024, 72.236800, 1.276420]
+    Jones_tc.test_vals = [-5.283772, 0.374024, 72.236800, 1.276420]
     Jones_tc.new_output = False
     test_list.append(Jones_tc)