New turbo ouputs

.clang-format

@@ -2,4 +2,4 @@ BasedOnStyle: Google
 PointerAlignment: Left
 DerivePointerAlignment: false
 ColumnLimit: 120
-SortIncludes: Never
+SortIncludes: false

Common/include/CConfig.hpp

@@ -71,7 +71,6 @@ class CConfig {
   unsigned short Kind_PerformanceAverageProcess; /*!< \brief Kind of mixing process.*/
   unsigned short Kind_MixingPlaneInterface;      /*!< \brief Kind of mixing process.*/
   unsigned short Kind_SpanWise;                  /*!< \brief Kind of span-wise section computation.*/
-  unsigned short *Kind_TurboMachinery;           /*!< \brief Kind of turbomachynery architecture.*/
   unsigned short iZone, nZone;    /*!< \brief Number of zones in the mesh. */
   unsigned short nZoneSpecified;  /*!< \brief Number of zones that are specified in config file. */
   su2double Highlite_Area;        /*!< \brief Highlite area. */
@@ -435,6 +434,9 @@ class CConfig {
   Max_DeltaTime,               /*!< \brief Max delta time. */
   Unst_CFL;                    /*!< \brief Unsteady CFL number. */
 
+  TURBO_PERF_KIND *Kind_TurboPerf;           /*!< \brief Kind of turbomachynery architecture.*/
+  TURBOMACHINERY_TYPE *Kind_TurboMachinery;
+
   /* Gradient smoothing options */
   su2double SmoothingEps1;          /*!< \brief Parameter for the identity part in gradient smoothing. */
   su2double SmoothingEps2;          /*!< \brief Parameter for the Laplace part in gradient smoothing. */
@@ -5118,7 +5120,7 @@ class CConfig {
    * \brief Get the kind of turbomachinery architecture.
    * \return Kind of turbomachinery architecture.
    */
-  unsigned short GetKind_TurboMachinery(unsigned short val_iZone) const { return Kind_TurboMachinery[val_iZone]; }
+  TURBOMACHINERY_TYPE GetKind_TurboMachinery(unsigned short val_iZone) const { return Kind_TurboMachinery[val_iZone]; }
 
   /*!
    * \brief Get the kind of turbomachinery architecture.
@@ -5233,7 +5235,7 @@ class CConfig {
   void SetnSpanWiseSections(unsigned short nSpan) { nSpanWiseSections = nSpan;}
 
   /*!
-   * \brief set number span-wise sections to compute 3D BC and performance for turbomachinery.
+   * \brief get number span-wise sections to compute 3D BC and performance for turbomachinery.
    */
   unsigned short GetnSpan_iZones(unsigned short iZone) const { return nSpan_iZones[iZone];}
 
@@ -5258,7 +5260,7 @@ class CConfig {
    * \brief get marker kind for Turbomachinery performance calculation.
    * \return kind index.
    */
-  unsigned short GetKind_TurboPerf(unsigned short index);
+  TURBO_PERF_KIND GetKind_TurboPerf(unsigned short val_iZone) const { return Kind_TurboPerf[val_iZone]; };
 
   /*!
    * \brief get outlet bounds name for Turbomachinery performance calculation.

Common/include/geometry/CGeometry.hpp

@@ -772,6 +772,15 @@ class CGeometry {
    */
   inline virtual void GatherInOutAverageValues(CConfig* config, bool allocate) {}
 
+  /*!
+   * \brief Store all the turboperformance in the solver in ZONE_0.
+   * \param[in] donor_geometry  - Solution from the donor mesh.
+   * \param[in] target_geometry - Solution from the target mesh.
+   * \param[in] donorZone       - counter of the donor solution
+   */
+  inline virtual void SetAvgTurboGeoValues(const CConfig* donor_config, CGeometry* donor_geometry,
+                                           unsigned short donorZone){};
+
   /*!
    * \brief Set max length.
    * \param[in] config - Definition of the particular problem.

Common/include/geometry/CPhysicalGeometry.hpp

@@ -408,6 +408,14 @@ class CPhysicalGeometry final : public CGeometry {
    */
   void GatherInOutAverageValues(CConfig* config, bool allocate) override;
 
+  /*!
+   * \brief Store all the turboperformance in the solver in ZONE_0.
+   * \param[in] donor_geometry  - Solution from the donor mesh.
+   * \param[in] target_geometry - Solution from the target mesh.
+   * \param[in] donorZone       - counter of the donor solution
+   */
+  void SetAvgTurboGeoValues(const CConfig* donor_config, CGeometry* donor_geometry, unsigned short donorZone) override;
+
   /*!
    * \brief Set the edge structure of the control volume.
    * \param[in] config - Definition of the particular problem.

Common/include/option_structure.hpp

@@ -1780,19 +1780,33 @@ static const MapType<std::string, SPANWISE_TYPE> SpanWise_Map = {
 /*!
  * \brief Types of mixing process for averaging quantities at the boundaries.
  */
-enum TURBOMACHINERY_TYPE {
-  AXIAL = 1,              /*!< \brief axial turbomachinery. */
-  CENTRIFUGAL = 2,        /*!< \brief centrifugal turbomachinery. */
-  CENTRIPETAL = 3,        /*!< \brief centripetal turbomachinery. */
-  CENTRIPETAL_AXIAL = 4,  /*!< \brief mixed flow turbine. */
-  AXIAL_CENTRIFUGAL = 5   /*!< \brief mixed flow turbine. */
+enum class TURBOMACHINERY_TYPE {
+  AXIAL,              /*!< \brief axial turbomachinery. */
+  CENTRIFUGAL,        /*!< \brief centrifugal turbomachinery. */
+  CENTRIPETAL,        /*!< \brief centripetal turbomachinery. */
+  CENTRIPETAL_AXIAL,  /*!< \brief mixed flow turbine. */
+  AXIAL_CENTRIFUGAL   /*!< \brief mixed flow turbine. */
 };
 static const MapType<std::string, TURBOMACHINERY_TYPE> TurboMachinery_Map = {
-  MakePair("AXIAL", AXIAL)
-  MakePair("CENTRIFUGAL", CENTRIFUGAL)
-  MakePair("CENTRIPETAL",  CENTRIPETAL)
-  MakePair("CENTRIPETAL_AXIAL",  CENTRIPETAL_AXIAL)
-  MakePair("AXIAL_CENTRIFUGAL",  AXIAL_CENTRIFUGAL)
+  MakePair("AXIAL", TURBOMACHINERY_TYPE::AXIAL)
+  MakePair("CENTRIFUGAL", TURBOMACHINERY_TYPE::CENTRIFUGAL)
+  MakePair("CENTRIPETAL",  TURBOMACHINERY_TYPE::CENTRIPETAL)
+  MakePair("CENTRIPETAL_AXIAL",  TURBOMACHINERY_TYPE::CENTRIPETAL_AXIAL)
+  MakePair("AXIAL_CENTRIFUGAL",  TURBOMACHINERY_TYPE::AXIAL_CENTRIFUGAL)
+};
+
+/*!
+ * \brief Types of Turbomachinery performance Type.
+ */
+enum class TURBO_PERF_KIND{
+  TURBINE,            /*!< \brief Turbine Performance. */
+  COMPRESSOR,         /*!< \brief Compressor Performance. */
+  PROPELLOR           /*!< \brief Propellor Performance. */
+};
+static const MapType<std::string, TURBO_PERF_KIND> TurboPerfKind_Map = {
+  MakePair("TURBINE",  TURBO_PERF_KIND::TURBINE)
+  MakePair("COMPRESSOR",  TURBO_PERF_KIND::COMPRESSOR)
+  MakePair("PROPELLOR",  TURBO_PERF_KIND::PROPELLOR)
 };
 
 /*!

Common/src/CConfig.cpp

@@ -1627,6 +1627,9 @@ void CConfig::SetConfig_Options() {
   /*!\brief TURBOMACHINERY_KIND \n DESCRIPTION: types of turbomachinery architecture.
       \n OPTIONS: see \link TurboMachinery_Map \endlink \n Default: AXIAL */
   addEnumListOption("TURBOMACHINERY_KIND",nTurboMachineryKind, Kind_TurboMachinery, TurboMachinery_Map);
+  /*!\brief TURBOMACHINERY_KIND \n DESCRIPTION: types of turbomachynery Performance Calculations.
+    \n OPTIONS: see \link TurboPerfKind_Map \endlink \n Default: TURBINE */
+  addEnumListOption("TURBO_PERF_KIND", nTurboMachineryKind, Kind_TurboPerf, TurboPerfKind_Map);
   /*!\brief MARKER_SHROUD \n DESCRIPTION: markers in which velocity is forced to 0.0.
    * \n Format: (shroud1, shroud2, ...)*/
   addStringListOption("MARKER_SHROUD", nMarker_Shroud, Marker_Shroud);
@@ -4020,6 +4023,11 @@ void CConfig::SetPostprocessing(SU2_COMPONENT val_software, unsigned short val_i
       SU2_MPI::Error("Giles Boundary conditions can only be used with turbomachinery markers", CURRENT_FUNCTION);
     }
 
+    /*--- Check if turbomachinery performance kind is specified with turbo markers ---*/
+    if (GetBoolTurbomachinery() && !(nTurboMachineryKind/nZone == 1)){
+      SU2_MPI::Error("Insufficient TURBO_PERF_KIND options specified with turbomachinery markers", CURRENT_FUNCTION);
+    }
+
     /*--- Check for Boundary condition available for NICFD ---*/
 
     if ((!ideal_gas) && (!noneq_gas)) {
@@ -6906,16 +6914,16 @@ void CConfig::SetOutput(SU2_COMPONENT val_software, unsigned short val_izone) {
 
       default:
         break;
+      }
     }
-  }
-  else {
-    if (Time_Domain) {
-      cout << "Dynamic structural analysis."<< endl;
-      cout << "Time step provided by the user for the dynamic analysis(s): "<< Time_Step << "." << endl;
-    } else {
-      cout << "Static structural analysis." << endl;
+    else {
+      if (Time_Domain) {
+        cout << "Dynamic structural analysis."<< endl;
+        cout << "Time step provided by the user for the dynamic analysis(s): "<< Time_Step << "." << endl;
+      } else {
+        cout << "Static structural analysis." << endl;
+      }
     }
-  }
 
     if ((Kind_Solver == MAIN_SOLVER::EULER) || (Kind_Solver == MAIN_SOLVER::NAVIER_STOKES) || (Kind_Solver == MAIN_SOLVER::RANS) ||
         (Kind_Solver == MAIN_SOLVER::INC_EULER) || (Kind_Solver == MAIN_SOLVER::INC_NAVIER_STOKES) || (Kind_Solver == MAIN_SOLVER::INC_RANS) ||