tune settings of translating naca

Author: pcarruscag

TestCases/py_wrapper/translating_NACA0012/config.cfg

@@ -43,18 +43,18 @@ MARKER_DEFORM_MESH= ( airfoil )
 % DISCRETIZATION METHODS
 %
 CONV_NUM_METHOD_FLOW= ROE
-MUSCL_FLOW= NO
+MUSCL_FLOW= YES
 NUM_METHOD_GRAD= GREEN_GAUSS
 SLOPE_LIMITER_FLOW= VENKATAKRISHNAN_WANG
 VENKAT_LIMITER_COEFF= 0.1
 
 % SOLUTION ACCELERATION
 %
-CFL_NUMBER= 1000
+CFL_NUMBER= 10
 CFL_ADAPT= NO
 %
 MGLEVEL= 3
-MGCYCLE= W_CYCLE
+MGCYCLE= V_CYCLE
 MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
 MG_POST_SMOOTH= ( 0, 0, 0, 0 )
 MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
@@ -63,19 +63,19 @@ MG_DAMP_PROLONGATION= 0.7
 
 %
 LINEAR_SOLVER= FGMRES
-LINEAR_SOLVER_PREC= ILU
-LINEAR_SOLVER_ERROR= 1.0e-6
-LINEAR_SOLVER_ITER= 25
+LINEAR_SOLVER_PREC= LU_SGS
+LINEAR_SOLVER_ERROR= 0.1
+LINEAR_SOLVER_ITER= 5
 
 % CONVERGENCE PARAMETERS
 %
-ITER= 2500
+ITER= 500
 CONV_FIELD= RMS_DENSITY
 CONV_RESIDUAL_MINVAL= -9
 
 % INPUT/OUTPUT
 %
 MESH_FILENAME= ../../euler/naca0012/mesh_NACA0012_inv.su2
 MESH_FORMAT= SU2
-SCREEN_OUTPUT= (INNER_ITER, RMS_RES, LIFT, DRAG, MOMENT_X, MOMENT_Y, MOMENT_Z, LINSOL_RES, LINSOL_ITER)
+SCREEN_OUTPUT= (INNER_ITER, RMS_RES, LIFT, DRAG, MOMENT_X, MOMENT_Y, MOMENT_Z, LINSOL)
 HISTORY_OUTPUT= (INNER_ITER, RMS_RES, AERO_COEFF)