Feature input output

Inc_Inviscid_Hydrofoil/inv_naca0012.cfg

@@ -96,7 +96,7 @@ CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
 %
 % Number of total iterations
-EXT_ITER= 9999
+ITER= 9999
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
@@ -157,24 +157,19 @@ TIME_DISCRE_FLOW= EULER_IMPLICIT
 %
 CONV_CRITERIA= RESIDUAL
 %
-% Residual reduction (order of magnitude with respect to the initial value)
-RESIDUAL_REDUCTION= 10
 %
 % Min value of the residual (log10 of the residual)
-RESIDUAL_MINVAL= -18
+CONV_RESIDUAL_MINVAL= -18
 %
 % Start Cauchy criteria at iteration number
-STARTCONV_ITER= 10
+CONV_STARTITER= 10
 %
 % Number of elements to apply the criteria
-CAUCHY_ELEMS= 50
+CONV_CAUCHY_ELEMS= 50
 %
 % Epsilon to control the series convergence
-CAUCHY_EPS= 1E-6
+CONV_CAUCHY_EPS= 1E-6
 %
-% Function to apply the criteria (LIFT, DRAG, SENS_GEOMETRY, SENS_MACH,
-%                                 DELTA_LIFT, DELTA_DRAG)
-CAUCHY_FUNC_FLOW= DRAG
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
@@ -185,25 +180,28 @@ MESH_FILENAME= mesh_NACA0012_5deg_6814.su2
 MESH_FORMAT= SU2
 %
 % Restart flow input file
-SOLUTION_FLOW_FILENAME= solution_flow.dat
+SOLUTION_FILENAME= solution_flow.dat
 %
-% Output file format (PARAVIEW, TECPLOT)
-OUTPUT_FORMAT= PARAVIEW
+% Output tabular format (CSV, TECPLOT)
+TABULAR_FORMAT= CSV
 %
 % Output file convergence history (w/o extension) 
 CONV_FILENAME= history
 %
 % Output file restart flow
-RESTART_FLOW_FILENAME= restart_flow.dat
+RESTART_FILENAME= restart_flow.dat
 %
 % Output file flow (w/o extension) variables
-VOLUME_FLOW_FILENAME= flow
+VOLUME_FILENAME= flow
 %
 % Output file surface flow coefficient (w/o extension)
-SURFACE_FLOW_FILENAME= surface_flow
+SURFACE_FILENAME= surface_flow
 %
 % Writing solution file frequency
 WRT_SOL_FREQ= 50
 %
 % Writing convergence history frequency
 WRT_CON_FREQ= 1
+% 
+% Screen output
+SCREEN_OUTPUT= (INNER_ITER, RMS_PRESSURE, RMS_VELOCITY-X, LIFT, DRAG)

Inc_Laminar_Cavity/lam_buoyancy_cavity.cfg

@@ -136,7 +136,7 @@ MAX_DELTA_TIME= 1E6
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
 %
 % Number of total iterations
-EXT_ITER= 99999
+ITER= 99999
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
@@ -201,24 +201,19 @@ TIME_DISCRE_FLOW= EULER_IMPLICIT
 % Convergence criteria (CAUCHY, RESIDUAL)
 CONV_CRITERIA= RESIDUAL
 %
-% Residual reduction (order of magnitude with respect to the initial value)
-RESIDUAL_REDUCTION= 8
 %
 % Min value of the residual (log10 of the residual)
-RESIDUAL_MINVAL= -12
+CONV_RESIDUAL_MINVAL= -12
 %
 % Start convergence criteria at iteration number
-STARTCONV_ITER= 10
+CONV_STARTITER= 10
 %
 % Number of elements to apply the criteria
-CAUCHY_ELEMS= 100
+CONV_CAUCHY_ELEMS= 100
 %
 % Epsilon to control the series convergence
-CAUCHY_EPS= 1E-6
+CONV_CAUCHY_EPS= 1E-6
 %
-% Function to apply the criteria (LIFT, DRAG, NEARFIELD_PRESS, SENS_GEOMETRY, 
-% 	      	    		 SENS_MACH, DELTA_LIFT, DELTA_DRAG)
-CAUCHY_FUNC_FLOW= DRAG
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
@@ -232,25 +227,25 @@ MESH_FORMAT= SU2
 MESH_OUT_FILENAME= mesh_out.su2
 %
 % Restart flow input file
-SOLUTION_FLOW_FILENAME= solution_flow.dat
+SOLUTION_FILENAME= solution_flow.dat
 %
 % Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
 %
 % Output file format (PARAVIEW, TECPLOT, STL)
-OUTPUT_FORMAT= PARAVIEW
+TABULAR_FORMAT= CSV
 %
 % Output file convergence history (w/o extension) 
 CONV_FILENAME= history
 %
 % Output file restart flow
-RESTART_FLOW_FILENAME= restart_flow.dat
+RESTART_FILENAME= restart_flow.dat
 %
 % Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
 %
 % Output file flow (w/o extension) variables
-VOLUME_FLOW_FILENAME= flow
+VOLUME_FILENAME= flow
 %
 % Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
@@ -259,7 +254,7 @@ VOLUME_ADJ_FILENAME= adjoint
 GRAD_OBJFUNC_FILENAME= of_grad.dat
 %
 % Output file surface flow coefficient (w/o extension)
-SURFACE_FLOW_FILENAME= surface_flow
+SURFACE_FILENAME= surface_flow
 %
 % Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
@@ -269,7 +264,9 @@ WRT_SOL_FREQ= 100
 %
 % Writing convergence history frequency
 WRT_CON_FREQ= 1
-
+%
+% Screen output
+SCREEN_OUTPUT= (INNER_ITER, RMS_PRESSURE, RMS_VELOCITY-X, LIFT, DRAG)
 % ----------------------- GEOMETRY EVALUATION PARAMETERS ----------------------%
 %
 % Extract a slice using GEO_BOUNDS (works with 2D cartesian grids only)

Inc_Laminar_Flat_Plate/lam_flatplate.cfg

@@ -142,7 +142,7 @@ CFL_ADAPT= NO
 CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
 %
 % Number of total iterations
-EXT_ITER= 99999
+ITER= 99999
 
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
@@ -212,24 +212,19 @@ TIME_DISCRE_FLOW= EULER_IMPLICIT
 %
 CONV_CRITERIA= RESIDUAL
 %
-% Residual reduction (order of magnitude with respect to the initial value)
-RESIDUAL_REDUCTION= 10
 %
 % Min value of the residual (log10 of the residual)
-RESIDUAL_MINVAL= -14
+CONV_RESIDUAL_MINVAL= -14
 %
 % Start convergence criteria at iteration number
-STARTCONV_ITER= 10
+CONV_STARTITER= 10
 %
 % Number of elements to apply the criteria
-CAUCHY_ELEMS= 100
+CONV_CAUCHY_ELEMS= 100
 %
 % Epsilon to control the series convergence
-CAUCHY_EPS= 1E-6
+CONV_CAUCHY_EPS= 1E-6
 %
-% Function to apply the criteria (LIFT, DRAG, NEARFIELD_PRESS, SENS_GEOMETRY, 
-% 	      	    		 SENS_MACH, DELTA_LIFT, DELTA_DRAG)
-CAUCHY_FUNC_FLOW= DRAG
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
@@ -243,25 +238,25 @@ MESH_FORMAT= SU2
 MESH_OUT_FILENAME= mesh_out.su2
 %
 % Restart flow input file
-SOLUTION_FLOW_FILENAME= solution_flow.dat
+SOLUTION_FILENAME= solution_flow.dat
 %
 % Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
 %
 % Output file format (PARAVIEW, TECPLOT, STL)
-OUTPUT_FORMAT= PARAVIEW
+TABULAR_FORMAT= CSV
 %
 % Output file convergence history (w/o extension) 
 CONV_FILENAME= history
 %
 % Output file restart flow
-RESTART_FLOW_FILENAME= restart_flow.dat
+RESTART_FILENAME= restart_flow.dat
 %
 % Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
 %
 % Output file flow (w/o extension) variables
-VOLUME_FLOW_FILENAME= flow
+VOLUME_FILENAME= flow
 %
 % Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
@@ -270,7 +265,7 @@ VOLUME_ADJ_FILENAME= adjoint
 GRAD_OBJFUNC_FILENAME= of_grad.dat
 %
 % Output file surface flow coefficient (w/o extension)
-SURFACE_FLOW_FILENAME= surface_flow
+SURFACE_FILENAME= surface_flow
 %
 % Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
@@ -280,6 +275,9 @@ WRT_SOL_FREQ= 250
 %
 % Writing convergence history frequency
 WRT_CON_FREQ= 1
+%
+% Screen output
+SCREEN_OUTPUT= (INNER_ITER, RMS_PRESSURE, RMS_VELOCITY-X, LIFT, DRAG)
 
 % ----------------------- GEOMETRY EVALUATION PARAMETERS ----------------------%
 %

Inc_Laminar_Step/lam_backwardstep.cfg

@@ -116,7 +116,7 @@ MAX_DELTA_TIME= 1E30
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
 %
 % Number of total iterations
-EXT_ITER= 99999
+ITER= 99999
 
 % ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
 %
@@ -197,24 +197,19 @@ TIME_DISCRE_FLOW= EULER_IMPLICIT
 %
 CONV_CRITERIA= RESIDUAL
 %
-% Residual reduction (order of magnitude with respect to the initial value)
-RESIDUAL_REDUCTION= 12
 %
 % Min value of the residual (log10 of the residual)
-RESIDUAL_MINVAL= -16
+CONV_RESIDUAL_MINVAL= -16
 %
 % Start convergence criteria at iteration number
-STARTCONV_ITER= 10
+CONV_STARTITER= 10
 %
 % Number of elements to apply the criteria
-CAUCHY_ELEMS= 100
+CONV_CAUCHY_ELEMS= 100
 %
 % Epsilon to control the series convergence
-CAUCHY_EPS= 1E-6
+CONV_CAUCHY_EPS= 1E-6
 %
-% Function to apply the criteria (LIFT, DRAG, NEARFIELD_PRESS, SENS_GEOMETRY, 
-% 	      	    		 SENS_MACH, DELTA_LIFT, DELTA_DRAG)
-CAUCHY_FUNC_FLOW= DRAG
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
@@ -228,25 +223,25 @@ MESH_FORMAT= SU2
 MESH_OUT_FILENAME= mesh_out.su2
 %
 % Restart flow input file
-SOLUTION_FLOW_FILENAME= solution_flow.dat
+SOLUTION_FILENAME= solution_flow.dat
 %
 % Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
 %
 % Output file format (PARAVIEW, TECPLOT, STL)
-OUTPUT_FORMAT= PARAVIEW
+TABULAR_FORMAT= CSV
 %
 % Output file convergence history (w/o extension) 
 CONV_FILENAME= history
 %
 % Output file restart flow
-RESTART_FLOW_FILENAME= restart_flow.dat
+RESTART_FILENAME= restart_flow.dat
 %
 % Output file restart adjoint
 RESTART_ADJ_FILENAME= restart_adj.dat
 %
 % Output file flow (w/o extension) variables
-VOLUME_FLOW_FILENAME= flow
+VOLUME_FILENAME= flow
 %
 % Output file adjoint (w/o extension) variables
 VOLUME_ADJ_FILENAME= adjoint
@@ -255,7 +250,7 @@ VOLUME_ADJ_FILENAME= adjoint
 GRAD_OBJFUNC_FILENAME= of_grad.dat
 %
 % Output file surface flow coefficient (w/o extension)
-SURFACE_FLOW_FILENAME= surface_flow
+SURFACE_FILENAME= surface_flow
 %
 % Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
@@ -265,6 +260,9 @@ WRT_SOL_FREQ= 250
 %
 % Writing convergence history frequency
 WRT_CON_FREQ= 1
+%
+% Screen output
+SCREEN_OUTPUT=(INNER_ITER, RMS_PRESSURE, RMS_VELOCITY-X, LIFT, DRAG)
 
 % ----------------------- GEOMETRY EVALUATION PARAMETERS ----------------------%
 %