Updated data-driven fluid regression test

Author: EvertBunschoten

SU2_CFD/src/solvers/CEulerSolver.cpp

@@ -4627,7 +4627,7 @@ void CEulerSolver::BC_Riemann(CGeometry *geometry, CSolver **solver_container,
       StaticEnergy_i = Energy_i - 0.5*Velocity2_i;
 
       GetFluidModel()->SetTDState_rhoe(Density_i, StaticEnergy_i);
-      
+
       Pressure_i = GetFluidModel()->GetPressure();
       Enthalpy_i = Energy_i + Pressure_i/Density_i;
 

SU2_CFD/src/solvers/CFEM_DG_EulerSolver.cpp

@@ -7902,7 +7902,7 @@ void CFEM_DG_EulerSolver::BoundaryStates_Riemann(CConfig                  *confi
 
       P_static /= config->GetPressure_Ref();
       Rho_static /= config->GetDensity_Ref();
-      
+
       /* Compute the prescribed pressure, static energy per unit mass
          and speed of sound. */
       FluidModel->SetTDState_Prho(P_static, Rho_static);

TestCases/nicf/datadriven/datadriven_nozzle.cfg

@@ -15,7 +15,7 @@
 SOLVER= RANS
 KIND_TURB_MODEL= SST
 MATH_PROBLEM= DIRECT
-RESTART_SOL= YES
+RESTART_SOL= NO
 SYSTEM_MEASUREMENTS= SI
 %
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%

TestCases/parallel_regression.py

@@ -1002,8 +1002,8 @@ def main():
     datadriven_fluidModel           = TestCase('datadriven_fluidModel')
     datadriven_fluidModel.cfg_dir   = "nicf/datadriven"
     datadriven_fluidModel.cfg_file  = "datadriven_nozzle.cfg"
-    datadriven_fluidModel.test_iter = 10
-    datadriven_fluidModel.test_vals = [-14.397040, -9.904042, -5.038828, 0.000000, 0.000000]
+    datadriven_fluidModel.test_iter = 50
+    datadriven_fluidModel.test_vals = [-2.623753, 0.145100, 4.688298, 0.000000, 0.000000]
     test_list.append(datadriven_fluidModel)
 
     # Rarefaction Q1D nozzle, include CoolProp transport model