remove jacobian contribution and test case config file options

Author: FlorianDm

SU2_CFD/include/numerics/turbulent/turb_sources.hpp

@@ -363,12 +363,6 @@ class CSourcePieceWise_TurbSST final : public CNumerics {
     /*--- Add terms to the residuals ---*/
     Residual[0] += yinv*Volume*(pk_axi-cdk_axi);
     Residual[1] += yinv*Volume*(pw_axi-cdw_axi);
-  
-    /*--- Add contribution to the jacobian for implicit time integration (ignore to conserve diagonal dominance) ---*/
-    //Jacobian_i[0][0] += yinv*Volume*(sigma_k_i*TurbVar_Grad_i[0][1]/zeta-V_i[2]);
-    //Jacobian_i[0][1] += yinv*Volume*(-sigma_k_i*k*TurbVar_Grad_i[0][1]/(zeta*zeta));
-    //Jacobian_i[1][0] += yinv*Volume*(sigma_w_i*TurbVar_Grad_i[1][1]/zeta);
-    //Jacobian_i[1][1] += yinv*Volume*(-sigma_w_i*k*TurbVar_Grad_i[1][1]/(zeta*zeta)-V_i[2]);
 
   }
 

TestCases/axisymmetric_rans/air_nozzle/air_nozzle.cfg

@@ -132,15 +132,6 @@ MUSCL_FLOW= YES
 % Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
 %                BARTH_JESPERSEN, VAN_ALBADA_EDGE)
 SLOPE_LIMITER_FLOW= NONE
-% 
-%Coefficient for the Venkat's limiter (upwind scheme). A larger values decrease
-%             the extent of limiting, values approaching zero cause
-%             lower-order approximation to the solution (0.05 by default)
-VENKAT_LIMITER_COEFF= 0.05
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
-%           Required for 2nd order upwind schemes (NO, YES)
-MUSCL_TURB= NO
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
@@ -165,24 +156,6 @@ LINEAR_SOLVER_ITER= 10
 %
 % Multi-grid levels (0 = no multi-grid)
 MGLEVEL= 0
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
-MGCYCLE= V_CYCLE
-%
-% Multi-grid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-grid post-smoothing level
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.75
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.75
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
@@ -231,24 +204,9 @@ MESH_FILENAME= nozzle.su2
 % Mesh input file format (SU2, CGNS)
 MESH_FORMAT= SU2
 %
-% Mesh output file
-MESH_OUT_FILENAME= mesh_out.su2
-%
 % Restart flow input file
 SOLUTION_FILENAME= solution_flow.dat
 %
-% Output file convergence history (w/o extension)
-CONV_FILENAME= history
-%
-% Output file restart flow
-RESTART_FILENAME= restart_flow.dat
-%
-% Output file flow (w/o extension) variables
-VOLUME_FILENAME= flow
-%
-% Output file surface flow coefficient (w/o extension)
-SURFACE_FILENAME= surface_flow
-%
 % Writing solution file frequency
 OUTPUT_WRT_FREQ= 1000
 %