fix leak set incomp hybrid regression residuals

Author: pcarruscag

SU2_CFD/include/solvers/CFVMFlowSolverBase.hpp

@@ -1036,7 +1036,7 @@ class CFVMFlowSolverBase : public CSolver {
       StrainMag(iPoint) = sqrt(2.0*StrainMag(iPoint));
       AD::SetPreaccOut(StrainMag(iPoint));
 
-      /*--- Max is not differentiable, we so not register for preacc. ---*/
+      /*--- Max is not differentiable, so we not register them for preacc. ---*/
       strainMax = max(strainMax, StrainMag(iPoint));
       omegaMax = max(omegaMax, GeometryToolbox::Norm(3, Vorticity));
 

SU2_CFD/src/drivers/CDiscAdjMultizoneDriver.cpp

@@ -197,7 +197,7 @@ void CDiscAdjMultizoneDriver::Run() {
 
   /*--- Initialize External with the objective function gradient. ---*/
 
-   su2double rhs_norm = 0.0;
+  su2double rhs_norm = 0.0;
 
   for (iZone = 0; iZone < nZone; iZone++) {
 

SU2_CFD/src/solvers/CIncEulerSolver.cpp

@@ -3097,7 +3097,7 @@ void CIncEulerSolver::LoadRestart(CGeometry **geometry, CSolver ***solver, CConf
     SU2_OMP_FOR_STAT(omp_chunk_size)
     for (iPoint = 0; iPoint < geometry[iMesh]->GetnPoint(); iPoint++) {
       Area_Parent = geometry[iMesh]->nodes->GetVolume(iPoint);
-      for (iVar = 0; iVar < nVar; iVar++) Solution[iVar] = 0.0;
+      su2double Solution[MAXNVAR] = {0.0};
       for (iChildren = 0; iChildren < geometry[iMesh]->nodes->GetnChildren_CV(iPoint); iChildren++) {
         Point_Fine = geometry[iMesh]->nodes->GetChildren_CV(iPoint, iChildren);
         Area_Children = geometry[iMesh-1]->nodes->GetVolume(Point_Fine);

TestCases/hybrid_regression.py

@@ -307,7 +307,7 @@ def main():
     inc_nozzle.cfg_dir   = "incomp_euler/nozzle"
     inc_nozzle.cfg_file  = "inv_nozzle.cfg"
     inc_nozzle.test_iter = 20
-    inc_nozzle.test_vals = [-5.971283, -4.911145, -0.000201, 0.121631]
+    inc_nozzle.test_vals = [-5.973103, -4.911802, -0.000195, 0.121643]
     inc_nozzle.new_output = True
     test_list.append(inc_nozzle)
 
@@ -329,7 +329,7 @@ def main():
     inc_buoyancy.cfg_dir   = "incomp_navierstokes/buoyancy_cavity"
     inc_buoyancy.cfg_file  = "lam_buoyancy_cavity.cfg"
     inc_buoyancy.test_iter = 20
-    inc_buoyancy.test_vals = [-4.436657, 0.507847, 0.000000, 0.000000]
+    inc_buoyancy.test_vals = [-4.432484, 0.507522, 0.000000, 0.000000]
     inc_buoyancy.new_output  = True
     test_list.append(inc_buoyancy)
 
@@ -338,7 +338,7 @@ 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 = [-8.108218, -2.158606, 0.019142, 1.902461]
+    inc_poly_cylinder.test_vals = [-7.852778, -2.091519, 0.029298, 1.922006]
     inc_poly_cylinder.new_output  = True
     test_list.append(inc_poly_cylinder)
 
@@ -347,7 +347,7 @@ 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 = [-3.450879, -3.083720, -0.020699, -0.168420]
+    inc_lam_bend.test_vals = [-3.438863, -3.102176, -0.017532, -0.193429]
     test_list.append(inc_lam_bend)
 
     ############################
@@ -368,7 +368,7 @@ 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 = [-7.276273, 0.145895, 0.000021, 0.312004]
+    inc_turb_naca0012_sst_sust.test_vals = [-7.276424, 0.145861, 0.000003, 0.312011]
     test_list.append(inc_turb_naca0012_sst_sust)
 
     ######################################
@@ -436,7 +436,7 @@ def main():
     unst_inc_turb_naca0015_sa.cfg_dir   = "unsteady/pitching_naca0015_rans_inc"
     unst_inc_turb_naca0015_sa.cfg_file  = "config_incomp_turb_sa.cfg"
     unst_inc_turb_naca0015_sa.test_iter = 1
-    unst_inc_turb_naca0015_sa.test_vals = [-3.007635, -6.879789, 1.445300, 0.419281]
+    unst_inc_turb_naca0015_sa.test_vals = [-3.008629, -6.888974, 1.435193, 0.433537]
     unst_inc_turb_naca0015_sa.unsteady  = True
     test_list.append(unst_inc_turb_naca0015_sa)
 
@@ -596,7 +596,7 @@ def main():
     slinc_steady.cfg_dir   = "sliding_interface/incompressible_steady"
     slinc_steady.cfg_file  = "config.cfg"
     slinc_steady.test_iter = 19
-    slinc_steady.test_vals = [19.000000, -1.766116, -2.206522] #last 3 columns
+    slinc_steady.test_vals = [19.000000, -1.762730, -2.263278] #last 3 columns
     slinc_steady.multizone = True
     test_list.append(slinc_steady)
 
@@ -676,7 +676,7 @@ def main():
     mms_fvm_inc_euler.cfg_dir   = "mms/fvm_incomp_euler"
     mms_fvm_inc_euler.cfg_file  = "inv_mms_jst.cfg"
     mms_fvm_inc_euler.test_iter = 20
-    mms_fvm_inc_euler.test_vals = [-9.128345, -9.441741, 0.000000, 0.000000]
+    mms_fvm_inc_euler.test_vals = [-9.128033, -9.441406, 0.000000, 0.000000]
     test_list.append(mms_fvm_inc_euler)
 
     # FVM, incompressible, laminar N-S