Update isnans

Author: joshkellyjak

SU2_CFD/src/output/CFlowCompOutput.cpp

@@ -773,13 +773,13 @@ void CFlowCompOutput::WriteTurboSpanwisePerformance(std::shared_ptr<CTurboOutput
     }
     file.width(30); file << BladePerf->GetInletState().GetVelocityValue()*config[ZONE_0]->GetVelocity_Ref();
     // This captures NaNs
-    if(isnan(BladePerf->GetInletState().GetAbsFlowAngle())){
+    if(std::isnan(BladePerf->GetInletState().GetAbsFlowAngle())){
       file.width(30); file << "0.0000";
     }
     else {
       file.width(30); file << BladePerf->GetInletState().GetAbsFlowAngle()*180.0/PI_NUMBER;
     }
-    if(isnan(BladePerf->GetInletState().GetFlowAngle())){
+    if(std::isnan(BladePerf->GetInletState().GetFlowAngle())){
       file.width(30); file << "0.0000";
     }
     else{
@@ -836,13 +836,13 @@ void CFlowCompOutput::WriteTurboSpanwisePerformance(std::shared_ptr<CTurboOutput
       file.width(30); file << BladePerf->GetOutletState().GetVelocity()[iDim]*config[ZONE_0]->GetVelocity_Ref();
     }
     file.width(30); file << BladePerf->GetInletState().GetVelocityValue()*config[ZONE_0]->GetVelocity_Ref();
-    if(isnan(BladePerf->GetInletState().GetAbsFlowAngle())){
+    if(std::isnan(BladePerf->GetInletState().GetAbsFlowAngle())){
       file.width(30); file << "0.0000";
     }
     else {
       file.width(30); file << BladePerf->GetOutletState().GetAbsFlowAngle()*180.0/PI_NUMBER;
     }
-    if(isnan(BladePerf->GetInletState().GetAbsFlowAngle())){
+    if(std::isnan(BladePerf->GetInletState().GetAbsFlowAngle())){
       file.width(30); file << "0.0000";
     }
     else{

SU2_CFD/src/solvers/CEulerSolver.cpp

@@ -9191,7 +9191,7 @@ void CEulerSolver::TurboAverageProcess(CSolver **solver, CGeometry *geometry, CC
                 for (auto iDim = 2; iDim < nDim +1;iDim++)
                   avgVelocity[iDim-1]  = AverageFlux[iMarker][iSpan][iDim] / AverageFlux[iMarker][iSpan][0];
 
-                if (isnan(avgDensity) || isnan(avgPressure) || avgPressure < 0.0 || avgDensity < 0.0 ){
+                if (std::isnan(avgDensity) || std::isnan(avgPressure) || avgPressure < 0.0 || avgDensity < 0.0 ){
                   val_init_pressure = TotalAreaPressure / TotalArea;
                   MixedOut_Average (config, val_init_pressure, AverageFlux[iMarker][iSpan], AverageTurboNormal, avgPressure, avgDensity);
                   avgVelocity[0]          = ( AverageFlux[iMarker][iSpan][1] - avgPressure) / AverageFlux[iMarker][iSpan][0];
@@ -9228,7 +9228,7 @@ void CEulerSolver::TurboAverageProcess(CSolver **solver, CGeometry *geometry, CC
             }
 
             /* --- check if averaged quantities are correct otherwise reset the old quantities ---*/
-            const bool nanSolution = (isnan(AverageDensity[iMarker][iSpan]) || isnan(AveragePressure[iMarker][iSpan]));
+            const bool nanSolution = (std::isnan(AverageDensity[iMarker][iSpan]) || std::isnan(AveragePressure[iMarker][iSpan]));
             const bool negSolution = (AverageDensity[iMarker][iSpan] < 0.0 || AveragePressure[iMarker][iSpan] < 0.0);
             if (nanSolution || negSolution){
               if (nanSolution)