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Merged
pcarruscag merged 24 commits into from
Aug 29, 2023
Merged

Develop #46

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e2802f0
Added python script which translates an MLP trained through Tensorflo…
EvertBunschoten Jan 23, 2023
ac88f7e
Fixed bug with importing the SU2 MLP writing tool
EvertBunschoten Jan 23, 2023
3fbbf69
Fixed typo in MLP translation file
EvertBunschoten Jan 27, 2023
389a1da
Merge branch 'develop' of https://github.com/su2code/Tutorials into f…
EvertBunschoten Jan 27, 2023
0b44489
Added to the Readme.md of the MLP tutorial
EvertBunschoten Feb 6, 2023
cdd3ace
Merge branch 'feature_multilayer_perceptron' of https://github.com/su…
EvertBunschoten Feb 6, 2023
bdad995
Added to description and added example MLP input file
EvertBunschoten Feb 16, 2023
3dd1266
remove MUSCL_FLOW=YES from JST cases
pcarruscag Mar 26, 2023
5e66f37
Merge pull request #39 from su2code/cusp_update
pcarruscag Mar 26, 2023
54eda4f
more cases with MUSCL + JST
pcarruscag Mar 27, 2023
9910df2
Merge branch 'cusp_update' into develop
pcarruscag Mar 27, 2023
475b0d8
Merge branch 'develop' of https://github.com/su2code/Tutorials into f…
EvertBunschoten Mar 30, 2023
d749112
Added tutorial for data-driven fluid model under NICFD nozzle
EvertBunschoten Apr 17, 2023
2dd6d7e
Improved formatting of documentation
EvertBunschoten Apr 18, 2023
7d18814
Removed README.md from datadriven tutorial
EvertBunschoten Apr 20, 2023
63d716b
Merge pull request #40 from su2code/feature_multilayer_perceptron
EvertBunschoten Apr 28, 2023
2ec2880
remove config since it is in the code repo
pcarruscag Apr 30, 2023
4672749
Revert "remove config since it is in the code repo"
pcarruscag Apr 30, 2023
c16c67e
use the config in tutorials instead
pcarruscag Apr 30, 2023
0f15049
Merge pull request #41 from su2code/avoid_duplicated_config
pcarruscag Apr 30, 2023
79bffe3
remove USE_SPECIES_STRONG_BC
bigfooted May 30, 2023
12b593e
Merge pull request #42 from su2code/feature_new_flamelet
bigfooted Jun 7, 2023
09e5662
Sst consistency (#44)
pcarruscag Jul 3, 2023
25d54da
add files for QuickStart tutorial (#43)
frx-wintermute Jul 21, 2023
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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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7 changes: 0 additions & 7 deletions design/Inviscid_2D_Unconstrained_NACA0012/inv_NACA0012_basic.cfg
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Original file line number Diff line number Diff line change
Expand Up @@ -133,9 +133,6 @@ MG_DAMP_PROLONGATION= 1.0
% ROE-2ND_ORDER)
CONV_NUM_METHOD_FLOW= JST
%
% Slope limiter (VENKATAKRISHNAN)
SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
%
% 2nd and 4th order artificial dissipation coefficients
JST_SENSOR_COEFF= ( 0.5, 0.02 )
%
Expand All @@ -154,9 +151,6 @@ OBJECTIVE_FUNCTION= DRAG
% ROE-2ND_ORDER)
CONV_NUM_METHOD_ADJFLOW= JST
%
% Slope limiter (VENKATAKRISHNAN, SHARP_EDGES)
SLOPE_LIMITER_ADJFLOW= VENKATAKRISHNAN
%
% 2nd, and 4th order artificial dissipation coefficients
ADJ_JST_SENSOR_COEFF= ( 0.0, 0.02 )
%
Expand Down Expand Up @@ -278,7 +272,6 @@ SURFACE_FILENAME= surface_flow
% Output file surface adjoint coefficient (w/o extension)
SURFACE_ADJ_FILENAME= surface_adjoint
%
%
% Screen output
SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_ENERGY, LIFT, DRAG)
%
Expand Down
4 changes: 2 additions & 2 deletions design/Turbulent_2D_Constrained_RAE2822/turb_SA_RAE2822.cfg
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Original file line number Diff line number Diff line change
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)
Expand All @@ -125,7 +125,7 @@ SLOPE_LIMITER_TURB= VENKATAKRISHNAN
%
% Monotonic Upwind Scheme for Conservation Laws (TVD) in the adjoint flow equations.
% Required for 2nd order upwind schemes (NO, YES)
MUSCL_ADJFLOW= YES
MUSCL_ADJFLOW= NO
%
% Slope limiter (NONE, VENKATAKRISHNAN, BARTH_JESPERSEN, VAN_ALBADA_EDGE,
% SHARP_EDGES, WALL_DISTANCE)
Expand Down
4 changes: 0 additions & 4 deletions design/Unsteady_Shape_Opt_NACA0012/unsteady_naca0012_opt.cfg
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Original file line number Diff line number Diff line change
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 )
%
Expand Down
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
Expand Down
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
Expand Down
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
Expand Down
8 changes: 0 additions & 8 deletions multiphysics/unsteady_fsi_python/Ma0357/fluid.cfg
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Open in desktop
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
8 changes: 0 additions & 8 deletions multiphysics/unsteady_fsi_python/Ma0364/fluid.cfg
View file
Open in desktop
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