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Update .cfg files to comply with SU2 v 7.2.1 #3

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65 changes: 65 additions & 0 deletions .gitignore
Original file line number Diff line number Diff line change
Expand Up @@ -3,3 +3,68 @@
*.vtk
*.out
*log*
mms/dg_navierstokes/unit_quad/SU2_DG_n8_p1.su2
mms/dg_navierstokes/unit_quad/SU2_DG_n4_p5.su2
mms/dg_navierstokes/unit_quad/SU2_DG_n8_p2.su2
mms/dg_navierstokes/unit_quad/SU2_DG_n8_p4.su2
mms/dg_navierstokes/unit_quad/SU2_DG_n8_p3.su2
mms/dg_navierstokes/unit_quad/SU2_DG_n8_p5.su2
rans/bump_in_channel_2d/.DS_Store
mms/ns_dg_fvm_time/.DS_Store
mms/fvm_navierstokes/surface_flow.vtu
mms/fvm_navierstokes/slope_rms_rhov.png
mms/fvm_navierstokes/slope_rms_rhou.png
mms/fvm_navierstokes/slope_rms_rhoe.png
mms/fvm_navierstokes/slope_rms_rho.png
mms/fvm_navierstokes/slope_max_rhov.png
mms/fvm_navierstokes/slope_max_rhou.png
mms/fvm_navierstokes/slope_max_rhoe.png
mms/fvm_navierstokes/slope_max_rho.png
mms/fvm_navierstokes/restart_flow.dat
mms/fvm_navierstokes/history.csv
mms/fvm_navierstokes/flow.vtu
mms/fvm_navierstokes/accuracy_rms_rhov.png
mms/fvm_navierstokes/accuracy_rms_rhou.png
mms/fvm_navierstokes/accuracy_rms_rhoe.png
mms/fvm_navierstokes/accuracy_rms_rho.png
mms/fvm_navierstokes/accuracy_max_rhov.png
mms/fvm_navierstokes/accuracy_max_rhou.png
mms/fvm_navierstokes/accuracy_max_rhoe.png
mms/fvm_navierstokes/accuracy_max_rho.png
mms/fvm_incomp_navierstokes/surface_flow.vtu
mms/fvm_incomp_navierstokes/square.su2
mms/fvm_incomp_navierstokes/slope_rms_u.png
mms/fvm_incomp_navierstokes/slope_rms_v.png
mms/fvm_incomp_navierstokes/slope_rms_p.png
mms/fvm_incomp_navierstokes/slope_max_v.png
mms/fvm_incomp_navierstokes/slope_max_u.png
mms/fvm_incomp_navierstokes/slope_max_p.png
mms/fvm_incomp_navierstokes/restart_flow.dat
mms/fvm_incomp_navierstokes/lam_mms_wls.cfg
mms/fvm_incomp_navierstokes/history.csv
mms/fvm_incomp_navierstokes/flow.vtu
mms/fvm_incomp_navierstokes/accuracy_rms_v.png
mms/fvm_incomp_navierstokes/accuracy_rms_u.png
mms/fvm_incomp_navierstokes/accuracy_rms_p.png
mms/fvm_incomp_navierstokes/accuracy_max_v.png
mms/fvm_incomp_navierstokes/accuracy_max_u.png
mms/fvm_incomp_navierstokes/accuracy_max_p.png
mms/fvm_incomp_euler/surface_flow.vtu
mms/fvm_incomp_euler/square.su2
mms/fvm_incomp_euler/slope_rms_v.png
mms/fvm_incomp_euler/slope_rms_u.png
mms/fvm_incomp_euler/slope_rms_p.png
mms/fvm_incomp_euler/slope_max_v.png
mms/fvm_incomp_euler/slope_max_u.png
mms/fvm_incomp_euler/slope_max_p.png
mms/fvm_incomp_euler/restart_flow.dat
mms/fvm_incomp_euler/history.csv
mms/fvm_incomp_euler/flow.vtu
mms/fvm_incomp_euler/accuracy_rms_v.png
mms/fvm_incomp_euler/accuracy_rms_u.png
mms/fvm_incomp_euler/accuracy_rms_p.png
mms/fvm_incomp_euler/accuracy_max_v.png
mms/fvm_incomp_euler/accuracy_max_u.png
mms/fvm_incomp_euler/accuracy_max_p.png
mms/dg_navierstokes/unit_quad/UnitQuadStructured_8X8_nPoly3.su2
mms/dg_navierstokes/unit_quad/surface_flow.vtu
39 changes: 22 additions & 17 deletions mms/dg_navierstokes/unit_quad/fem_UnitQuad_nPoly1.cfg
Original file line number Diff line number Diff line change
Expand Up @@ -6,7 +6,7 @@
% FEM_EULER, FEM_NAVIER_STOKES,
% WAVE_EQUATION, HEAT_EQUATION, LINEAR_ELASTICITY,
% POISSON_EQUATION)
PHYSICAL_PROBLEM= FEM_NAVIER_STOKES
SOLVER= FEM_NAVIER_STOKES
%
% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
MATH_PROBLEM= DIRECT
Expand Down Expand Up @@ -83,10 +83,10 @@ MARKER_CUSTOM= ( BottomBoundary, LeftBoundary, RightBoundary, TopBoundary )
% ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
%
% Courant-Friedrichs-Lewy condition of the finest grid
CFL_NUMBER= 0.05
CFL_NUMBER= 0.03
%
% Number of total iterations
EXT_ITER= 200000
ITER= 20000
%
% Runge-Kutta alpha coefficients
RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
Expand Down Expand Up @@ -115,26 +115,26 @@ TIME_DISCRE_FEM_FLOW= RUNGE-KUTTA_EXPLICIT
% --------------------------- CONVERGENCE PARAMETERS --------------------------%
%
% Convergence criteria (CAUCHY, RESIDUAL)
CONV_CRITERIA= RESIDUAL
%CONV_CRITERIA= RESIDUAL
%
% Residual reduction (order of magnitude with respect to the initial value)
RESIDUAL_REDUCTION= 6
%RESIDUAL_REDUCTION= 6
%
% Min value of the residual (log10 of the residual)
RESIDUAL_MINVAL= -8
CONV_RESIDUAL_MINVAL= -8
%
% Start Cauchy 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, SENS_GEOMETRY, SENS_MACH,
% DELTA_LIFT, DELTA_DRAG)
CAUCHY_FUNC_FLOW= DRAG
%CAUCHY_FUNC_FLOW= DRAG

% ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
% Mesh input file
Expand All @@ -147,25 +147,27 @@ MESH_FORMAT= SU2
MESH_OUT_FILENAME= mesh_out.su2
%
% Restart flow input file
SOLUTION_FLOW_FILENAME= restart_flow.dat
SOLUTION_FILENAME= restart_flow.dat
%
% Restart adjoint input file
SOLUTION_ADJ_FILENAME= solution_adj.dat
%
% Output tabular format (CSV, TECPLOT)
TABULAR_FORMAT= CSV
% Output file format (TECPLOT, PARAVIEW, TECPLOT_BINARY)
OUTPUT_FORMAT= PARAVIEW_BINARY
%OUTPUT_FORMAT= PARAVIEW_BINARY
%
% 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
Expand All @@ -174,13 +176,16 @@ 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
%
% Writing solution file frequency
WRT_SOL_FREQ= 25000
OUTPUT_WRT_FREQ= 25000
%
% Writing convergence history frequency
WRT_CON_FREQ= 100
%WRT_CON_FREQ= 100
%
% Screen output
SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_ENERGY, LIFT, DRAG)
39 changes: 22 additions & 17 deletions mms/dg_navierstokes/unit_quad/fem_UnitQuad_nPoly2.cfg
Original file line number Diff line number Diff line change
Expand Up @@ -6,7 +6,7 @@
% FEM_EULER, FEM_NAVIER_STOKES,
% WAVE_EQUATION, HEAT_EQUATION, LINEAR_ELASTICITY,
% POISSON_EQUATION)
PHYSICAL_PROBLEM= FEM_NAVIER_STOKES
SOLVER= FEM_NAVIER_STOKES
%
% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
MATH_PROBLEM= DIRECT
Expand Down Expand Up @@ -83,10 +83,10 @@ MARKER_CUSTOM= ( BottomBoundary, LeftBoundary, RightBoundary, TopBoundary )
% ------------- COMMON PARAMETERS TO DEFINE THE NUMERICAL METHOD --------------%
%
% Courant-Friedrichs-Lewy condition of the finest grid
CFL_NUMBER= 0.05
CFL_NUMBER= 0.03
%
% Number of total iterations
EXT_ITER= 200000
ITER= 200000
%
% Runge-Kutta alpha coefficients
RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
Expand Down Expand Up @@ -115,26 +115,26 @@ TIME_DISCRE_FEM_FLOW= RUNGE-KUTTA_EXPLICIT
% --------------------------- CONVERGENCE PARAMETERS --------------------------%
%
% Convergence criteria (CAUCHY, RESIDUAL)
CONV_CRITERIA= RESIDUAL
%CONV_CRITERIA= RESIDUAL
%
% Residual reduction (order of magnitude with respect to the initial value)
RESIDUAL_REDUCTION= 6
%RESIDUAL_REDUCTION= 6
%
% Min value of the residual (log10 of the residual)
RESIDUAL_MINVAL= -8
CONV_RESIDUAL_MINVAL= -8
%
% Start Cauchy 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, SENS_GEOMETRY, SENS_MACH,
% DELTA_LIFT, DELTA_DRAG)
CAUCHY_FUNC_FLOW= DRAG
%CAUCHY_FUNC_FLOW= DRAG

% ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
% Mesh input file
Expand All @@ -147,25 +147,27 @@ MESH_FORMAT= SU2
MESH_OUT_FILENAME= mesh_out.su2
%
% Restart flow input file
SOLUTION_FLOW_FILENAME= restart_flow.dat
SOLUTION_FILENAME= restart_flow.dat
%
% Restart adjoint input file
SOLUTION_ADJ_FILENAME= solution_adj.dat
%
% Output tabular format (CSV, TECPLOT)
TABULAR_FORMAT= CSV
% Output file format (TECPLOT, PARAVIEW, TECPLOT_BINARY)
OUTPUT_FORMAT= PARAVIEW_BINARY
%OUTPUT_FORMAT= PARAVIEW_BINARY
%
% 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
Expand All @@ -174,13 +176,16 @@ 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
%
% Writing solution file frequency
WRT_SOL_FREQ= 25000
OUTPUT_WRT_FREQ= 25000
%
% Writing convergence history frequency
WRT_CON_FREQ= 100
%WRT_CON_FREQ= 100
%
% Screen output
SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_ENERGY, LIFT, DRAG)
23 changes: 13 additions & 10 deletions mms/dg_navierstokes/unit_quad/fem_UnitQuad_nPoly3.cfg
Original file line number Diff line number Diff line change
Expand Up @@ -6,7 +6,7 @@
% FEM_EULER, FEM_NAVIER_STOKES,
% WAVE_EQUATION, HEAT_EQUATION, LINEAR_ELASTICITY,
% POISSON_EQUATION)
PHYSICAL_PROBLEM= FEM_NAVIER_STOKES
SOLVER= FEM_NAVIER_STOKES
%
% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
MATH_PROBLEM= DIRECT
Expand Down Expand Up @@ -121,16 +121,16 @@ CONV_CRITERIA= RESIDUAL
RESIDUAL_REDUCTION= 6
%
% Min value of the residual (log10 of the residual)
RESIDUAL_MINVAL= -8
CONV_RESIDUAL_MINVAL= -8
%
% Start Cauchy 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, SENS_GEOMETRY, SENS_MACH,
% DELTA_LIFT, DELTA_DRAG)
Expand All @@ -147,7 +147,7 @@ MESH_FORMAT= SU2
MESH_OUT_FILENAME= mesh_out.su2
%
% Restart flow input file
SOLUTION_FLOW_FILENAME= restart_flow.dat
SOLUTION_FILENAME= restart_flow.dat
%
% Restart adjoint input file
SOLUTION_ADJ_FILENAME= solution_adj.dat
Expand All @@ -159,13 +159,13 @@ OUTPUT_FORMAT= PARAVIEW_BINARY
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
Expand All @@ -174,13 +174,16 @@ 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
%
% Writing solution file frequency
WRT_SOL_FREQ= 25000
OUTPUT_WRT_FREQ= 25000
%
% Writing convergence history frequency
WRT_CON_FREQ= 100
%
% Screen output
SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_ENERGY, LIFT, DRAG)
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