continuous adjoint fixes

pcarruscag · pcarruscag · commit d350b08305f4 · 2023-03-26T12:59:32.000+01:00
diff --git a/Common/src/CConfig.cpp b/Common/src/CConfig.cpp
@@ -3567,6 +3567,13 @@ void CConfig::SetPostprocessing(SU2_COMPONENT val_software, unsigned short val_i
       MUSCL_Flow = false;
     }
   }
+  if (MUSCL_AdjFlow && (Kind_ConvNumScheme_AdjFlow == SPACE_CENTERED)) {
+    if (OptionIsSet("MUSCL_ADJFLOW")) {
+      SU2_MPI::Error("Centered schemes do not use MUSCL reconstruction (use MUSCL_ADJFLOW= NO).", CURRENT_FUNCTION);
+    } else {
+      MUSCL_AdjFlow = false;
+    }
+  }
 
   if (!MUSCL_Flow || (Kind_ConvNumScheme_Flow == SPACE_CENTERED)) Kind_SlopeLimit_Flow = LIMITER::NONE;
   if (!MUSCL_AdjFlow || (Kind_ConvNumScheme_AdjFlow == SPACE_CENTERED)) Kind_SlopeLimit_AdjFlow = LIMITER::NONE;
diff --git a/QuickStart/inv_NACA0012.cfg b/QuickStart/inv_NACA0012.cfg
@@ -161,14 +161,6 @@ TIME_DISCRE_FLOW= EULER_IMPLICIT
 % Convective numerical method (JST, LAX-FRIEDRICH, ROE)
 CONV_NUM_METHOD_ADJFLOW= JST
 %
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the adjoint flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
-MUSCL_ADJFLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE,
-%                SHARP_EDGES, WALL_DISTANCE)
-SLOPE_LIMITER_ADJFLOW= NONE
-%
 % Reduction factor of the CFL coefficient in the adjoint problem
 CFL_REDUCTION_ADJFLOW= 0.01
 %
diff --git a/SU2_CFD/src/variables/CFlowVariable.cpp b/SU2_CFD/src/variables/CFlowVariable.cpp
@@ -50,7 +50,7 @@ CFlowVariable::CFlowVariable(unsigned long npoint, unsigned long ndim, unsigned
 
   Primitive.resize(nPoint, nPrimVar) = su2double(0.0);
 
-  if (config->GetMUSCL_Flow() || config->GetViscous()) {
+  if (config->GetMUSCL_Flow() || config->GetViscous() || config->GetContinuous_Adjoint()) {
     Gradient_Primitive.resize(nPoint, nPrimVarGrad, nDim, 0.0);
   }
 
diff --git a/TestCases/cont_adj_euler/oneram6/inv_ONERAM6.cfg b/TestCases/cont_adj_euler/oneram6/inv_ONERAM6.cfg
@@ -85,8 +85,6 @@ TIME_DISCRE_FLOW= EULER_IMPLICIT
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
 %
 CONV_NUM_METHOD_ADJFLOW= JST
-MUSCL_ADJFLOW= YES
-SLOPE_LIMITER_ADJFLOW= NONE
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.02 )
 CFL_REDUCTION_ADJFLOW= 0.5
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
diff --git a/TestCases/cont_adj_rans/naca0012/turb_nasa.cfg b/TestCases/cont_adj_rans/naca0012/turb_nasa.cfg
@@ -72,8 +72,6 @@ TIME_DISCRE_TURB= EULER_IMPLICIT
 %
 OBJECTIVE_FUNCTION= DRAG
 CONV_NUM_METHOD_ADJFLOW= JST
-MUSCL_ADJFLOW= YES
-SLOPE_LIMITER_ADJFLOW= NONE
 ADJ_SHARP_LIMITER_COEFF= 3.0
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.002 )
 CFL_REDUCTION_ADJFLOW= 0.25
diff --git a/TestCases/cont_adj_rans/naca0012/turb_nasa_binary.cfg b/TestCases/cont_adj_rans/naca0012/turb_nasa_binary.cfg
@@ -73,8 +73,6 @@ TIME_DISCRE_TURB= EULER_IMPLICIT
 %
 OBJECTIVE_FUNCTION= DRAG
 CONV_NUM_METHOD_ADJFLOW= JST
-MUSCL_ADJFLOW= YES
-SLOPE_LIMITER_ADJFLOW= NONE
 ADJ_SHARP_LIMITER_COEFF= 3.0
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.002 )
 CFL_REDUCTION_ADJFLOW= 0.25
diff --git a/TestCases/control_surface/inv_ONERAM6_moving.cfg b/TestCases/control_surface/inv_ONERAM6_moving.cfg
@@ -77,8 +77,6 @@ TIME_DISCRE_FLOW= EULER_IMPLICIT
 %
 OBJECTIVE_FUNCTION= DRAG
 CONV_NUM_METHOD_ADJFLOW= JST
-MUSCL_ADJFLOW= YES
-SLOPE_LIMITER_ADJFLOW= NONE
 ADJ_SHARP_LIMITER_COEFF= 3.0
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.04 )
 CFL_REDUCTION_ADJFLOW= 0.5
diff --git a/TestCases/control_surface/inv_ONERAM6_setting.cfg b/TestCases/control_surface/inv_ONERAM6_setting.cfg
@@ -77,8 +77,6 @@ TIME_DISCRE_FLOW= EULER_IMPLICIT
 %
 OBJECTIVE_FUNCTION= DRAG
 CONV_NUM_METHOD_ADJFLOW= JST
-MUSCL_ADJFLOW= YES
-SLOPE_LIMITER_ADJFLOW= NONE
 ADJ_SHARP_LIMITER_COEFF= 3.0
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.04 )
 CFL_REDUCTION_ADJFLOW= 0.5
diff --git a/TestCases/deformation/naca0012/def_NACA0012.cfg b/TestCases/deformation/naca0012/def_NACA0012.cfg
@@ -80,8 +80,6 @@ TIME_DISCRE_FLOW= EULER_IMPLICIT
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
 %
 CONV_NUM_METHOD_ADJFLOW= JST
-MUSCL_ADJFLOW= YES
-SLOPE_LIMITER_ADJFLOW= NONE
 ADJ_JST_SENSOR_COEFF= ( 0.5, 0.02 )
 CFL_REDUCTION_ADJFLOW= 0.5
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
diff --git a/TestCases/deformation/naca0012/surface_file_NACA0012.cfg b/TestCases/deformation/naca0012/surface_file_NACA0012.cfg
@@ -80,8 +80,6 @@ TIME_DISCRE_FLOW= EULER_IMPLICIT
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
 %
 CONV_NUM_METHOD_ADJFLOW= JST
-MUSCL_ADJFLOW= YES
-SLOPE_LIMITER_ADJFLOW= NONE
 ADJ_JST_SENSOR_COEFF= ( 0.5, 0.02 )
 CFL_REDUCTION_ADJFLOW= 0.5
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
diff --git a/TestCases/disc_adj_euler/arina2k/Arina2KRS.cfg b/TestCases/disc_adj_euler/arina2k/Arina2KRS.cfg
@@ -20,7 +20,7 @@ RESTART_SOL= NO
 DISCARD_INFILES= NO
 SYSTEM_MEASUREMENTS= SI
 
-% -------------------- COMPRESSIBLE FREE-STREAM 
+% -------------------- COMPRESSIBLE FREE-STREAM
 %
 MACH_NUMBER= 0.2395
 AOA= 0.0
@@ -94,21 +94,8 @@ OBJECTIVE_WEIGHT = 1.0
 
 % ----------- SLOPE LIMITER AND DISSIPATION SENSOR DEFINITION -----------------%
 %
-MUSCL_FLOW= YES
-SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-MUSCL_TURB= NO
-SLOPE_LIMITER_TURB= VENKATAKRISHNAN
-MUSCL_ADJFLOW= YES
-SLOPE_LIMITER_ADJFLOW= VENKATAKRISHNAN
-MUSCL_ADJTURB= NO
-SLOPE_LIMITER_ADJTURB= VENKATAKRISHNAN
-VENKAT_LIMITER_COEFF= 0.05
-ADJ_SHARP_LIMITER_COEFF= 3.0
-LIMITER_ITER= 999999
 LAX_SENSOR_COEFF= 0.15
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-ADJ_LAX_SENSOR_COEFF= 0.15
-ADJ_JST_SENSOR_COEFF= ( 0.5, 0.02 )
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
diff --git a/TestCases/disc_adj_euler/cylinder3D/inv_cylinder3D.cfg b/TestCases/disc_adj_euler/cylinder3D/inv_cylinder3D.cfg
@@ -17,7 +17,7 @@ MATH_PROBLEM= DISCRETE_ADJOINT
 RESTART_SOL= NO
 DISCARD_INFILES= NO
 SYSTEM_MEASUREMENTS= SI
-REORIENT_ELEMENTS= NO 
+REORIENT_ELEMENTS= NO
 HISTORY_OUTPUT= (ITER, RMS_RES, SENSITIVITY)
 
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
@@ -38,7 +38,7 @@ REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
 MARKER_EULER= (CYLINDER_DOWN, CYLINDER_UP, SIDE, WALL)
-INLET_TYPE= MASS_FLOW 
+INLET_TYPE= MASS_FLOW
 MARKER_INLET= ( IN, 1.22498, 102.089, 1.0, 0.0, 0.0 )
 MARKER_OUTLET= ( OUT, 101325 )
 
@@ -48,33 +48,20 @@ MARKER_PLOTTING = ( CYLINDER_DOWN, CYLINDER_UP )
 MARKER_MONITORING = ( CYLINDER_DOWN, CYLINDER_UP )
 MARKER_DESIGNING = ( CYLINDER_DOWN, CYLINDER_UP )
 MARKER_ANALYZE = ( IN, OUT )
-MARKER_ANALYZE_AVERAGE = AREA 
+MARKER_ANALYZE_AVERAGE = AREA
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
 NUM_METHOD_GRAD= GREEN_GAUSS
 CFL_NUMBER= 10.0
 CFL_ADAPT= NO
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.25, 50.0 )
-OBJECTIVE_FUNCTION= LIFT 
+OBJECTIVE_FUNCTION= LIFT
 
 % ----------- SLOPE LIMITER AND DISSIPATION SENSOR DEFINITION -----------------%
 %
-MUSCL_FLOW= YES
-SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-MUSCL_TURB= NO
-SLOPE_LIMITER_TURB= VENKATAKRISHNAN
-MUSCL_ADJFLOW= YES
-SLOPE_LIMITER_ADJFLOW= VENKATAKRISHNAN
-MUSCL_ADJTURB= NO
-SLOPE_LIMITER_ADJTURB= VENKATAKRISHNAN
-VENKAT_LIMITER_COEFF= 0.05
-ADJ_SHARP_LIMITER_COEFF= 3.0
-LIMITER_ITER= 999999
 LAX_SENSOR_COEFF= 0.15
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-ADJ_LAX_SENSOR_COEFF= 0.15
-ADJ_JST_SENSOR_COEFF= ( 0.5, 0.02 )
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
diff --git a/TestCases/euler/CRM/inv_CRM_JST.cfg b/TestCases/euler/CRM/inv_CRM_JST.cfg
@@ -73,8 +73,6 @@ TIME_DISCRE_FLOW= EULER_IMPLICIT
 %
 OBJECTIVE_FUNCTION= DRAG
 CONV_NUM_METHOD_ADJFLOW= JST
-MUSCL_ADJFLOW= YES
-SLOPE_LIMITER_ADJFLOW= NONE
 ADJ_SHARP_LIMITER_COEFF= 3.0
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.04 )
 CFL_REDUCTION_ADJFLOW= 0.5
diff --git a/TestCases/euler/biparabolic/BIPARABOLIC.cfg b/TestCases/euler/biparabolic/BIPARABOLIC.cfg
@@ -73,8 +73,6 @@ TIME_DISCRE_FLOW= EULER_IMPLICIT
 %
 OBJECTIVE_FUNCTION= EQUIVALENT_AREA
 CONV_NUM_METHOD_ADJFLOW= JST
-MUSCL_ADJFLOW= YES
-SLOPE_LIMITER_ADJFLOW= NONE
 ADJ_SHARP_LIMITER_COEFF= 3.0
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.02 )
 CFL_REDUCTION_ADJFLOW= 0.8
diff --git a/TestCases/euler/naca0012/inv_NACA0012.cfg b/TestCases/euler/naca0012/inv_NACA0012.cfg
@@ -77,8 +77,6 @@ TIME_DISCRE_FLOW= EULER_IMPLICIT
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
 %
 CONV_NUM_METHOD_ADJFLOW= JST
-MUSCL_ADJFLOW= YES
-SLOPE_LIMITER_ADJFLOW= NONE
 ADJ_JST_SENSOR_COEFF= ( 0.5, 0.02 )
 CFL_REDUCTION_ADJFLOW= 0.5
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
diff --git a/TestCases/euler/oneram6/inv_ONERAM6.cfg b/TestCases/euler/oneram6/inv_ONERAM6.cfg
@@ -85,8 +85,6 @@ TIME_DISCRE_FLOW= EULER_IMPLICIT
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
 %
 CONV_NUM_METHOD_ADJFLOW= JST
-MUSCL_ADJFLOW= YES
-SLOPE_LIMITER_ADJFLOW= NONE
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.02 )
 CFL_REDUCTION_ADJFLOW= 0.5
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
diff --git a/TestCases/fixed_cl/naca0012/inv_NACA0012.cfg b/TestCases/fixed_cl/naca0012/inv_NACA0012.cfg
@@ -84,8 +84,6 @@ TIME_DISCRE_FLOW= EULER_IMPLICIT
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
 %
 CONV_NUM_METHOD_ADJFLOW= JST
-MUSCL_ADJFLOW= YES
-SLOPE_LIMITER_ADJFLOW= NONE
 ADJ_JST_SENSOR_COEFF= ( 0.5, 0.02 )
 CFL_REDUCTION_ADJFLOW= 0.5
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
diff --git a/TestCases/fixed_cl/naca0012/inv_NACA0012_ContAdj.cfg b/TestCases/fixed_cl/naca0012/inv_NACA0012_ContAdj.cfg
@@ -85,8 +85,6 @@ TIME_DISCRE_FLOW= EULER_IMPLICIT
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
 %
 CONV_NUM_METHOD_ADJFLOW= JST
-MUSCL_ADJFLOW= YES
-SLOPE_LIMITER_ADJFLOW= NONE
 ADJ_JST_SENSOR_COEFF= ( 0.5, 0.02 )
 CFL_REDUCTION_ADJFLOW= 0.5
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
diff --git a/TestCases/harmonic_balance/HB.cfg b/TestCases/harmonic_balance/HB.cfg
@@ -75,8 +75,6 @@ TIME_DISCRE_FLOW= EULER_IMPLICIT
 %
 OBJECTIVE_FUNCTION= DRAG
 CONV_NUM_METHOD_ADJFLOW= JST
-MUSCL_ADJFLOW= YES
-SLOPE_LIMITER_ADJFLOW= NONE
 ADJ_SHARP_LIMITER_COEFF= 3.0
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.02 )
 CFL_REDUCTION_ADJFLOW= 0.6
diff --git a/TestCases/nonequilibrium/invwedge/invwedge_lax.cfg b/TestCases/nonequilibrium/invwedge/invwedge_lax.cfg
@@ -47,9 +47,6 @@ LINEAR_SOLVER_ITER= 5
 % -----------------------------------------------------------------------%
 %
 CONV_NUM_METHOD_FLOW= LAX-FRIEDRICH
-MUSCL_FLOW= YES
-SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-VENKAT_LIMITER_COEFF= 0.05
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
@@ -63,11 +60,11 @@ CONV_CAUCHY_EPS= 1E-10
 %
 MESH_FILENAME= invwedge.su2
 MESH_FORMAT= SU2
-SOLUTION_FILENAME= restart_flow.dat  
-TABULAR_FORMAT= TECPLOT 
+SOLUTION_FILENAME= restart_flow.dat
+TABULAR_FORMAT= TECPLOT
 CONV_FILENAME= convergence
 RESTART_FILENAME= restart_flow.dat
 VOLUME_FILENAME= soln_volume
-SURFACE_FILENAME= soln_surface     
+SURFACE_FILENAME= soln_surface
 OUTPUT_WRT_FREQ= 100
 OUTPUT_FILES= (RESTART_ASCII, PARAVIEW_ASCII)
diff --git a/TestCases/optimization_euler/pitching_naca64a010/pitching_NACA64A010.cfg b/TestCases/optimization_euler/pitching_naca64a010/pitching_NACA64A010.cfg
@@ -105,8 +105,6 @@ TIME_DISCRE_FLOW= EULER_IMPLICIT
 %
 OBJECTIVE_FUNCTION= DRAG
 CONV_NUM_METHOD_ADJFLOW= JST
-MUSCL_ADJFLOW= YES
-SLOPE_LIMITER_ADJFLOW= NONE
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.02 )
 CFL_REDUCTION_ADJFLOW= 0.5
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
diff --git a/TestCases/optimization_euler/pitching_oneram6/pitching_ONERAM6.cfg b/TestCases/optimization_euler/pitching_oneram6/pitching_ONERAM6.cfg
@@ -97,8 +97,6 @@ TIME_DISCRE_FLOW= EULER_IMPLICIT
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
 %
 CONV_NUM_METHOD_ADJFLOW= JST
-MUSCL_ADJFLOW= YES
-SLOPE_LIMITER_ADJFLOW= NONE
 ADJ_SHARP_LIMITER_COEFF= 3.0
 ADJ_JST_SENSOR_COEFF= ( 0.5, 0.02 )
 CFL_REDUCTION_ADJFLOW= 0.25
diff --git a/TestCases/optimization_euler/steady_inverse_design/inv_NACA0012.cfg b/TestCases/optimization_euler/steady_inverse_design/inv_NACA0012.cfg
@@ -80,8 +80,6 @@ TIME_DISCRE_FLOW= EULER_IMPLICIT
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
 %
 CONV_NUM_METHOD_ADJFLOW= JST
-MUSCL_ADJFLOW= YES
-SLOPE_LIMITER_ADJFLOW= NONE
 ADJ_JST_SENSOR_COEFF= ( 0.5, 0.02 )
 CFL_REDUCTION_ADJFLOW= 0.5
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
diff --git a/TestCases/optimization_rans/pitching_naca64a010/turb_NACA64A010.cfg b/TestCases/optimization_rans/pitching_naca64a010/turb_NACA64A010.cfg
@@ -104,8 +104,6 @@ TIME_DISCRE_TURB= EULER_IMPLICIT
 %
 OBJECTIVE_FUNCTION= DRAG
 CONV_NUM_METHOD_ADJFLOW= JST
-MUSCL_ADJFLOW= YES
-SLOPE_LIMITER_ADJFLOW= NONE
 ADJ_SHARP_LIMITER_COEFF= 3.0
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.01 )
 CFL_REDUCTION_ADJFLOW= 0.9
diff --git a/TestCases/optimization_rans/pitching_oneram6/turb_ONERAM6.cfg b/TestCases/optimization_rans/pitching_oneram6/turb_ONERAM6.cfg
@@ -103,8 +103,6 @@ TIME_DISCRE_TURB= EULER_IMPLICIT
 %
 OBJECTIVE_FUNCTION= DRAG
 CONV_NUM_METHOD_ADJFLOW= JST
-MUSCL_ADJFLOW= YES
-SLOPE_LIMITER_ADJFLOW= NONE
 ADJ_SHARP_LIMITER_COEFF= 3.0
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.02 )
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
diff --git a/TestCases/polar/naca0012/inv_NACA0012.cfg b/TestCases/polar/naca0012/inv_NACA0012.cfg
@@ -80,8 +80,6 @@ TIME_DISCRE_FLOW= EULER_IMPLICIT
 
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
 CONV_NUM_METHOD_ADJFLOW= JST
-MUSCL_ADJFLOW= YES
-SLOPE_LIMITER_ADJFLOW= NONE
 ADJ_JST_SENSOR_COEFF= ( 0.5, 0.02 )
 CFL_REDUCTION_ADJFLOW= 0.5
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
diff --git a/TestCases/py_wrapper/flatPlate_unsteady_CHT/unsteady_CHT_FlatPlate_Conf.cfg b/TestCases/py_wrapper/flatPlate_unsteady_CHT/unsteady_CHT_FlatPlate_Conf.cfg
@@ -115,21 +115,8 @@ SENS_REMOVE_SHARP= NO
 
 % ----------- SLOPE LIMITER AND DISSIPATION SENSOR DEFINITION -----------------%
 %
-MUSCL_FLOW= YES
-SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-MUSCL_TURB= NO
-SLOPE_LIMITER_TURB= VENKATAKRISHNAN
-MUSCL_ADJFLOW= YES
-SLOPE_LIMITER_ADJFLOW= VENKATAKRISHNAN
-MUSCL_ADJTURB= NO
-SLOPE_LIMITER_ADJTURB= VENKATAKRISHNAN
-VENKAT_LIMITER_COEFF= 0.05
-ADJ_SHARP_LIMITER_COEFF= 3.0
-LIMITER_ITER= 999999
 LAX_SENSOR_COEFF= 0.15
 JST_SENSOR_COEFF= ( 0.5, 0.02 )
-ADJ_LAX_SENSOR_COEFF= 0.15
-ADJ_JST_SENSOR_COEFF= ( 0.5, 0.02 )
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
diff --git a/TestCases/rans/naca0012/turb_NACA0012_sst_multigrid_restart.cfg b/TestCases/rans/naca0012/turb_NACA0012_sst_multigrid_restart.cfg
@@ -119,8 +119,6 @@ CFL_REDUCTION_TURB= 1.0
 
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
 CONV_NUM_METHOD_ADJFLOW= JST
-MUSCL_ADJFLOW= YES
-SLOPE_LIMITER_ADJFLOW= NONE
 ADJ_JST_SENSOR_COEFF= ( 0.5, 0.02 )
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
 CFL_REDUCTION_ADJFLOW= 0.8
diff --git a/TestCases/rans/rae2822/turb_SA_RAE2822.cfg b/TestCases/rans/rae2822/turb_SA_RAE2822.cfg
@@ -75,8 +75,6 @@ TIME_DISCRE_TURB= EULER_IMPLICIT
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
 OBJECTIVE_FUNCTION= DRAG
 CONV_NUM_METHOD_ADJFLOW= JST
-MUSCL_ADJFLOW= YES
-SLOPE_LIMITER_ADJFLOW= NONE
 ADJ_SHARP_LIMITER_COEFF= 3.0
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.01 )
 CFL_REDUCTION_ADJFLOW= 0.75
diff --git a/TestCases/rotating/naca0012/rot_NACA0012.cfg b/TestCases/rotating/naca0012/rot_NACA0012.cfg
@@ -86,8 +86,6 @@ TIME_DISCRE_FLOW= EULER_IMPLICIT
 %
 OBJECTIVE_FUNCTION= DRAG
 CONV_NUM_METHOD_ADJFLOW= JST
-MUSCL_ADJFLOW= YES
-SLOPE_LIMITER_ADJFLOW= NONE
 ADJ_SHARP_LIMITER_COEFF= 3.0
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.02 )
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
diff --git a/TestCases/unsteady/pitching_naca64a010_euler/pitching_NACA64A010.cfg b/TestCases/unsteady/pitching_naca64a010_euler/pitching_NACA64A010.cfg
@@ -101,8 +101,6 @@ TIME_DISCRE_FLOW= EULER_IMPLICIT
 %
 OBJECTIVE_FUNCTION= DRAG
 CONV_NUM_METHOD_ADJFLOW= JST
-MUSCL_ADJFLOW= YES
-SLOPE_LIMITER_ADJFLOW= NONE
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.02 )
 CFL_REDUCTION_ADJFLOW= 0.5
 TIME_DISCRE_ADJFLOW= EULER_IMPLICIT
diff --git a/TestCases/unsteady/pitching_naca64a010_rans/turb_NACA64A010.cfg b/TestCases/unsteady/pitching_naca64a010_rans/turb_NACA64A010.cfg
@@ -106,8 +106,6 @@ TIME_DISCRE_TURB= EULER_IMPLICIT
 %
 OBJECTIVE_FUNCTION= DRAG
 CONV_NUM_METHOD_ADJFLOW= JST
-MUSCL_ADJFLOW= YES
-SLOPE_LIMITER_ADJFLOW= NONE
 ADJ_SHARP_LIMITER_COEFF= 3.0
 ADJ_JST_SENSOR_COEFF= ( 0.0, 0.01 )
 CFL_REDUCTION_ADJFLOW= 0.9

Original file line number	Diff line number	Diff line change
`@@ -3567,6 +3567,13 @@ void CConfig::SetPostprocessing(SU2_COMPONENT val_software, unsigned short val_i`
`3567`	`3567`	`MUSCL_Flow = false;`
`3568`	`3568`	`}`
`3569`	`3569`	`}`
	`3570`	`+ if (MUSCL_AdjFlow && (Kind_ConvNumScheme_AdjFlow == SPACE_CENTERED)) {`
	`3571`	`+ if (OptionIsSet("MUSCL_ADJFLOW")) {`
	`3572`	`+ SU2_MPI::Error("Centered schemes do not use MUSCL reconstruction (use MUSCL_ADJFLOW= NO).", CURRENT_FUNCTION);`
	`3573`	`+ } else {`
	`3574`	`+ MUSCL_AdjFlow = false;`
	`3575`	`+ }`
	`3576`	`+ }`
`3570`	`3577`
`3571`	`3578`	`if (!MUSCL_Flow \|\| (Kind_ConvNumScheme_Flow == SPACE_CENTERED)) Kind_SlopeLimit_Flow = LIMITER::NONE;`
`3572`	`3579`	`if (!MUSCL_AdjFlow \|\| (Kind_ConvNumScheme_AdjFlow == SPACE_CENTERED)) Kind_SlopeLimit_AdjFlow = LIMITER::NONE;`
Original file line number	Diff line number	Diff line change
`@@ -50,7 +50,7 @@ CFlowVariable::CFlowVariable(unsigned long npoint, unsigned long ndim, unsigned`
`50`	`50`
`51`	`51`	`Primitive.resize(nPoint, nPrimVar) = su2double(0.0);`
`52`	`52`
`53`		`- if (config->GetMUSCL_Flow() \|\| config->GetViscous()) {`
	`53`	`+ if (config->GetMUSCL_Flow() \|\| config->GetViscous() \|\| config->GetContinuous_Adjoint()) {`
`54`	`54`	`Gradient_Primitive.resize(nPoint, nPrimVarGrad, nDim, 0.0);`
`55`	`55`	`}`
`56`	`56`
Original file line number	Diff line number	Diff line change
`@@ -85,8 +85,6 @@ TIME_DISCRE_FLOW= EULER_IMPLICIT`
`85`	`85`	`% ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%`
`86`	`86`	`%`
`87`	`87`	`CONV_NUM_METHOD_ADJFLOW= JST`
`88`		`-MUSCL_ADJFLOW= YES`
`89`		`-SLOPE_LIMITER_ADJFLOW= NONE`
`90`	`88`	`ADJ_JST_SENSOR_COEFF= ( 0.0, 0.02 )`
`91`	`89`	`CFL_REDUCTION_ADJFLOW= 0.5`
`92`	`90`	`TIME_DISCRE_ADJFLOW= EULER_IMPLICIT`
Original file line number	Diff line number	Diff line change
`@@ -72,8 +72,6 @@ TIME_DISCRE_TURB= EULER_IMPLICIT`
`72`	`72`	`%`
`73`	`73`	`OBJECTIVE_FUNCTION= DRAG`
`74`	`74`	`CONV_NUM_METHOD_ADJFLOW= JST`
`75`		`-MUSCL_ADJFLOW= YES`
`76`		`-SLOPE_LIMITER_ADJFLOW= NONE`
`77`	`75`	`ADJ_SHARP_LIMITER_COEFF= 3.0`
`78`	`76`	`ADJ_JST_SENSOR_COEFF= ( 0.0, 0.002 )`
`79`	`77`	`CFL_REDUCTION_ADJFLOW= 0.25`
Original file line number	Diff line number	Diff line change
`@@ -73,8 +73,6 @@ TIME_DISCRE_TURB= EULER_IMPLICIT`
`73`	`73`	`%`
`74`	`74`	`OBJECTIVE_FUNCTION= DRAG`
`75`	`75`	`CONV_NUM_METHOD_ADJFLOW= JST`
`76`		`-MUSCL_ADJFLOW= YES`
`77`		`-SLOPE_LIMITER_ADJFLOW= NONE`
`78`	`76`	`ADJ_SHARP_LIMITER_COEFF= 3.0`
`79`	`77`	`ADJ_JST_SENSOR_COEFF= ( 0.0, 0.002 )`
`80`	`78`	`CFL_REDUCTION_ADJFLOW= 0.25`
Original file line number	Diff line number	Diff line change
`@@ -77,8 +77,6 @@ TIME_DISCRE_FLOW= EULER_IMPLICIT`
`77`	`77`	`%`
`78`	`78`	`OBJECTIVE_FUNCTION= DRAG`
`79`	`79`	`CONV_NUM_METHOD_ADJFLOW= JST`
`80`		`-MUSCL_ADJFLOW= YES`
`81`		`-SLOPE_LIMITER_ADJFLOW= NONE`
`82`	`80`	`ADJ_SHARP_LIMITER_COEFF= 3.0`
`83`	`81`	`ADJ_JST_SENSOR_COEFF= ( 0.0, 0.04 )`
`84`	`82`	`CFL_REDUCTION_ADJFLOW= 0.5`
Original file line number	Diff line number	Diff line change
`@@ -80,8 +80,6 @@ TIME_DISCRE_FLOW= EULER_IMPLICIT`
`80`	`80`	`% ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%`
`81`	`81`	`%`
`82`	`82`	`CONV_NUM_METHOD_ADJFLOW= JST`
`83`		`-MUSCL_ADJFLOW= YES`
`84`		`-SLOPE_LIMITER_ADJFLOW= NONE`
`85`	`83`	`ADJ_JST_SENSOR_COEFF= ( 0.5, 0.02 )`
`86`	`84`	`CFL_REDUCTION_ADJFLOW= 0.5`
`87`	`85`	`TIME_DISCRE_ADJFLOW= EULER_IMPLICIT`