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remove MUSCL_FLOW=YES from JST cases #39

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Merged
pcarruscag merged 1 commit into from
Mar 26, 2023
Merged

remove MUSCL_FLOW=YES from JST cases #39

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15 changes: 1 addition & 14 deletions compressible_flow/Turbulent_ONERAM6/turb_ONERAM6.cfg
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Original file line number Diff line number Diff line change
Expand Up @@ -185,22 +185,9 @@ MG_DAMP_PROLONGATION= 0.7

% -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
%
% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
% TURKEL_PREC, MSW)
% Convective numerical method
CONV_NUM_METHOD_FLOW= JST
%
% Spatial numerical order integration (1ST_ORDER, 2ND_ORDER, 2ND_ORDER_LIMITER)
MUSCL_FLOW= YES
%
% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
% BARTH_JESPERSEN, VAN_ALBADA_EDGE)
SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
%
% 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
%
% 2nd and 4th order artificial dissipation coefficients for
% the JST method ( 0.5, 0.02 by default )
JST_SENSOR_COEFF= ( 0.5, 0.02 )
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2 changes: 1 addition & 1 deletion design/Turbulent_2D_Constrained_RAE2822/turb_SA_RAE2822.cfg
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Expand Up @@ -109,7 +109,7 @@ OBJECTIVE_FUNCTION= DRAG
%
% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
% Required for 2nd order upwind schemes (NO, YES)
MUSCL_FLOW= YES
MUSCL_FLOW= NO
%
% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
% BARTH_JESPERSEN, VAN_ALBADA_EDGE)
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4 changes: 0 additions & 4 deletions design/Unsteady_Shape_Opt_NACA0012/unsteady_naca0012_opt.cfg
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Expand Up @@ -136,10 +136,6 @@ LINEAR_SOLVER_ITER= 5
% TURKEL_PREC, MSW)
CONV_NUM_METHOD_FLOW= JST
%
% Spatial numerical order integration (1ST_ORDER, 2ND_ORDER, 2ND_ORDER_LIMITER)
%
% MUSCL_FLOW= YES
%
% 1st, 2nd and 4th order artificial dissipation coefficients
JST_SENSOR_COEFF= ( 0.5, 0.01 )
%
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10 changes: 1 addition & 9 deletions multiphysics/unsteady_fsi_python/Ma01/fluid.cfg
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Original file line number Diff line number Diff line change
Expand Up @@ -121,18 +121,10 @@ LINEAR_SOLVER_ITER= 10
%
% -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
%
% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
% Convective numerical method (JST, LAX-FRIEDRICH, ROE, AUSM, HLLC,
% TURKEL_PREC, MSW)
CONV_NUM_METHOD_FLOW= JST
%
% Spatial numerical order integration (1ST_ORDER, 2ND_ORDER, 2ND_ORDER_LIMITER)
%
% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
% Required for 2nd order upwind schemes (NO, YES)
MUSCL_FLOW= YES
% Slope limiter (VENKATAKRISHNAN, MINMOD)
SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
%
JST_SENSOR_COEFF= ( 0.5, 0.01 )
% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
TIME_DISCRE_FLOW= EULER_IMPLICIT
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8 changes: 0 additions & 8 deletions multiphysics/unsteady_fsi_python/Ma02/fluid.cfg
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Original file line number Diff line number Diff line change
Expand Up @@ -125,14 +125,6 @@ LINEAR_SOLVER_ITER= 10
% TURKEL_PREC, MSW)
CONV_NUM_METHOD_FLOW= JST
%
% Spatial numerical order integration (1ST_ORDER, 2ND_ORDER, 2ND_ORDER_LIMITER)
%
% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
% Required for 2nd order upwind schemes (NO, YES)
MUSCL_FLOW= YES
% Slope limiter (VENKATAKRISHNAN, MINMOD)
SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
%
JST_SENSOR_COEFF= ( 0.5, 0.01 )
% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
TIME_DISCRE_FLOW= EULER_IMPLICIT
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8 changes: 0 additions & 8 deletions multiphysics/unsteady_fsi_python/Ma03/fluid.cfg
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Original file line number Diff line number Diff line change
Expand Up @@ -125,14 +125,6 @@ LINEAR_SOLVER_ITER= 10
% TURKEL_PREC, MSW)
CONV_NUM_METHOD_FLOW= JST
%
% Spatial numerical order integration (1ST_ORDER, 2ND_ORDER, 2ND_ORDER_LIMITER)
%
% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
% Required for 2nd order upwind schemes (NO, YES)
MUSCL_FLOW= YES
% Slope limiter (VENKATAKRISHNAN, MINMOD)
SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
%
JST_SENSOR_COEFF= ( 0.5, 0.01 )
% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
TIME_DISCRE_FLOW= EULER_IMPLICIT
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8 changes: 0 additions & 8 deletions multiphysics/unsteady_fsi_python/Ma0357/fluid.cfg
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Original file line number Diff line number Diff line change
Expand Up @@ -125,14 +125,6 @@ LINEAR_SOLVER_ITER= 10
% TURKEL_PREC, MSW)
CONV_NUM_METHOD_FLOW= JST
%
% Spatial numerical order integration (1ST_ORDER, 2ND_ORDER, 2ND_ORDER_LIMITER)
%
% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
% Required for 2nd order upwind schemes (NO, YES)
MUSCL_FLOW= YES
% Slope limiter (VENKATAKRISHNAN, MINMOD)
SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
%
JST_SENSOR_COEFF= ( 0.5, 0.01 )
% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
TIME_DISCRE_FLOW= EULER_IMPLICIT
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8 changes: 0 additions & 8 deletions multiphysics/unsteady_fsi_python/Ma0364/fluid.cfg
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Original file line number Diff line number Diff line change
Expand Up @@ -125,14 +125,6 @@ LINEAR_SOLVER_ITER= 10
% TURKEL_PREC, MSW)
CONV_NUM_METHOD_FLOW= JST
%
% Spatial numerical order integration (1ST_ORDER, 2ND_ORDER, 2ND_ORDER_LIMITER)
%
% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
% Required for 2nd order upwind schemes (NO, YES)
MUSCL_FLOW= YES
% Slope limiter (VENKATAKRISHNAN, MINMOD)
SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
%
JST_SENSOR_COEFF= ( 0.5, 0.01 )
% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
TIME_DISCRE_FLOW= EULER_IMPLICIT
Expand Down