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Merged
pcarruscag merged 24 commits into from
Aug 16, 2021
Merged

Develop #17

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4e23045
Add unsteady CHT tutorial files.
TobiKattmann Mar 4, 2021
7b4df74
Make necessary changes to run the case.
TobiKattmann Mar 4, 2021
3f45ca0
Change unsteady CHT Testcase options.
TobiKattmann Mar 18, 2021
507fc80
Adapt to new cfg options of 1226.
TobiKattmann Mar 18, 2021
56aedab
Merge pull request #12 from su2code/unsteady_cht_tutorial
TobiKattmann Mar 18, 2021
ac2a3d9
Remove unused CONV_CRITERIA from all tutorials.
TobiKattmann Mar 19, 2021
36145c6
Merge pull request #13 from su2code/remove_convcriteria
TobiKattmann Mar 19, 2021
aa1eaa6
Update fluid.cfg
Nicola-Fonzi Apr 5, 2021
3da975f
Update fluid.cfg
Nicola-Fonzi Apr 5, 2021
56c0e05
Update fluid.cfg
Nicola-Fonzi Apr 5, 2021
c3cd8f2
Update fluid.cfg
Nicola-Fonzi Apr 5, 2021
d06c159
Update fluid.cfg
Nicola-Fonzi Apr 5, 2021
b3ee198
Merge pull request #14 from su2code/fix_unsteadyFsiPythonCfg
Nicola-Fonzi Apr 16, 2021
88bcff6
Revert premature cfg-option name change that failed reg tests.
TobiKattmann Jun 11, 2021
f9908d5
Update solid.cfg
Nicola-Fonzi Jun 23, 2021
e012f59
Update solid.cfg
Nicola-Fonzi Jun 23, 2021
e982305
Update solid.cfg
Nicola-Fonzi Jun 23, 2021
1017dcc
Update solid.cfg
Nicola-Fonzi Jun 23, 2021
32a24e2
Update solid.cfg
Nicola-Fonzi Jun 23, 2021
07419e5
Merge pull request #15 from su2code/update_fsi_python
Nicola-Fonzi Jun 27, 2021
c6edb17
Fix failing reg test due to changed option name.
TobiKattmann Jul 20, 2021
8ac5df9
Change steady-cht cfg to match the incomp2D in Testcases. Tutorial wa…
TobiKattmann Jul 20, 2021
f4536d6
Change KT_CONSTANT to THERMAL_CONDUCTIVITY_CONSTANT.
TobiKattmann Jul 29, 2021
93c742f
Merge pull request #16 from su2code/feature_heatcoeff_BC
TobiKattmann Jul 31, 2021
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3 changes: 0 additions & 3 deletions compressible_flow/ActuatorDisk_VariableLoad/propeller_variable_load.cfg
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Expand Up @@ -184,9 +184,6 @@ TIME_DISCRE_TURB= EULER_IMPLICIT
% Maximum number of iterations
ITER= 1500
%
% Convergence criteria (CAUCHY, RESIDUAL)
CONV_CRITERIA= RESIDUAL
%
% Min value of the residual (log10 of the residual)
CONV_RESIDUAL_MINVAL= -8
%
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7 changes: 1 addition & 6 deletions compressible_flow/NICFD_nozzle/NICFD_nozzle.cfg
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Expand Up @@ -104,7 +104,7 @@ MU_CONSTANT= 1.21409E-05
CONDUCTIVITY_MODEL= CONSTANT_CONDUCTIVITY
%
% Molecular Thermal Conductivity that would be constant (0.0257 by default)
KT_CONSTANT= 0.030542828
THERMAL_CONDUCTIVITY_CONSTANT= 0.030542828

% -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
%
Expand Down Expand Up @@ -204,11 +204,6 @@ CFL_REDUCTION_TURB= 1.0
% Number of total iterations
ITER= 1000
%
% Convergence criteria (CAUCHY, RESIDUAL)
%
CONV_CRITERIA= RESIDUAL
%
%
% Min value of the residual (log10 of the residual)
CONV_RESIDUAL_MINVAL= -24
%
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5 changes: 0 additions & 5 deletions compressible_flow/UQ_NACA0012/turb_NACA0012_uq.cfg
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Expand Up @@ -177,11 +177,6 @@ CFL_REDUCTION_TURB= 1.0

% --------------------------- CONVERGENCE PARAMETERS --------------------------%
%
% Convergence criteria (CAUCHY, RESIDUAL)
%
CONV_CRITERIA= CAUCHY
%
%
% Min value of the residual (log10 of the residual)
CONV_RESIDUAL_MINVAL= -9
%
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5 changes: 0 additions & 5 deletions compressible_flow/UQ_NACA0012/turb_NACA0012_uq_1c.cfg
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Expand Up @@ -194,11 +194,6 @@ CFL_REDUCTION_TURB= 1.0

% --------------------------- CONVERGENCE PARAMETERS --------------------------%
%
% Convergence criteria (CAUCHY, RESIDUAL)
%
CONV_CRITERIA= CAUCHY
%
%
% Min value of the residual (log10 of the residual)
CONV_RESIDUAL_MINVAL= -9
%
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5 changes: 0 additions & 5 deletions compressible_flow/UQ_NACA0012/turb_NACA0012_uq_2c.cfg
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Expand Up @@ -194,11 +194,6 @@ CFL_REDUCTION_TURB= 1.0

% --------------------------- CONVERGENCE PARAMETERS --------------------------%
%
% Convergence criteria (CAUCHY, RESIDUAL)
%
CONV_CRITERIA= CAUCHY
%
%
% Min value of the residual (log10 of the residual)
CONV_RESIDUAL_MINVAL= -9
%
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5 changes: 0 additions & 5 deletions compressible_flow/UQ_NACA0012/turb_NACA0012_uq_3c.cfg
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Expand Up @@ -194,11 +194,6 @@ CFL_REDUCTION_TURB= 1.0

% --------------------------- CONVERGENCE PARAMETERS --------------------------%
%
% Convergence criteria (CAUCHY, RESIDUAL)
%
CONV_CRITERIA= CAUCHY
%
%
% Min value of the residual (log10 of the residual)
CONV_RESIDUAL_MINVAL= -9
%
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5 changes: 0 additions & 5 deletions compressible_flow/UQ_NACA0012/turb_NACA0012_uq_p1c1.cfg
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Expand Up @@ -194,11 +194,6 @@ CFL_REDUCTION_TURB= 1.0

% --------------------------- CONVERGENCE PARAMETERS --------------------------%
%
% Convergence criteria (CAUCHY, RESIDUAL)
%
CONV_CRITERIA= CAUCHY
%
%
% Min value of the residual (log10 of the residual)
CONV_RESIDUAL_MINVAL= -9
%
Expand Down
5 changes: 0 additions & 5 deletions compressible_flow/UQ_NACA0012/turb_NACA0012_uq_p1c2.cfg
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Expand Up @@ -194,11 +194,6 @@ CFL_REDUCTION_TURB= 1.0

% --------------------------- CONVERGENCE PARAMETERS --------------------------%
%
% Convergence criteria (CAUCHY, RESIDUAL)
%
CONV_CRITERIA= CAUCHY
%
%
% Min value of the residual (log10 of the residual)
CONV_RESIDUAL_MINVAL= -9
%
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2 changes: 0 additions & 2 deletions compressible_flow/Unsteady_NACA0012/unsteady_naca0012.cfg
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Expand Up @@ -145,8 +145,6 @@ TIME_DISCRE_TURB= EULER_IMPLICIT
%
% --------------------------- CONVERGENCE PARAMETERS --------------------------%
%
% Convergence criteria (CAUCHY, RESIDUAL)
CONV_CRITERIA = RESIDUAL
% Field to apply Cauchy Criterion to
CONV_FIELD= REL_RMS_DENSITY
% Min value of the residual (log10 of the residual)
Expand Down
4 changes: 0 additions & 4 deletions design/Inviscid_2D_Unconstrained_NACA0012/inv_NACA0012_basic.cfg
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Expand Up @@ -221,10 +221,6 @@ DEFORM_LINEAR_SOLVER_ERROR= 1E-14
DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME

% --------------------------- CONVERGENCE PARAMETERS --------------------------%
% Convergence criteria (CAUCHY, RESIDUAL)
%
CONV_CRITERIA= RESIDUAL
%
%
% Min value of the residual (log10 of the residual)
CONV_RESIDUAL_MINVAL= -13
Expand Down
3 changes: 0 additions & 3 deletions design/Inviscid_3D_Constrained_ONERAM6/inv_ONERAM6_adv.cfg
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Expand Up @@ -173,9 +173,6 @@ GEO_MODE= FUNCTION

% --------------------------- CONVERGENCE PARAMETERS --------------------------&
%
% Convergence criteria (CAUCHY, RESIDUAL)
CONV_CRITERIA= RESIDUAL
%
% Min value of the residual (log10 of the residual)
CONV_RESIDUAL_MINVAL= -12
%
Expand Down
5 changes: 0 additions & 5 deletions design/Multi_Objective_Shape_Design/inv_wedge_ROE_multiobj_combo.cfg
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Expand Up @@ -217,11 +217,6 @@ MARKER_ANALYZE_AVERAGE = AREA

% --------------------------- CONVERGENCE PARAMETERS --------------------------%
%
% Convergence criteria (CAUCHY, RESIDUAL)
%
CONV_CRITERIA= RESIDUAL
%
%
% Min value of the residual (log10 of the residual)
CONV_RESIDUAL_MINVAL= -11
%
Expand Down
3 changes: 0 additions & 3 deletions design/Turbulent_2D_Constrained_RAE2822/turb_SA_RAE2822.cfg
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Expand Up @@ -219,9 +219,6 @@ GEO_MODE= FUNCTION

% --------------------------- CONVERGENCE PARAMETERS --------------------------%
%
% Convergence criteria (CAUCHY, RESIDUAL)
CONV_CRITERIA= RESIDUAL
%
% Min value of the residual (log10 of the residual)
CONV_RESIDUAL_MINVAL= -12
%
Expand Down
2 changes: 0 additions & 2 deletions design/Unsteady_Shape_Opt_NACA0012/unsteady_naca0012_opt.cfg
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Expand Up @@ -158,8 +158,6 @@ TIME_DISCRE_TURB= EULER_IMPLICIT
%
% --------------------------- CONVERGENCE PARAMETERS --------------------------%
%
% Convergence criteria (CAUCHY, RESIDUAL)
CONV_CRITERIA = RESIDUAL
% Field to apply Cauchy Criterion to
CONV_FIELD= REL_RMS_DENSITY
% Min value of the residual (log10 of the residual)
Expand Down
2 changes: 1 addition & 1 deletion incompressible_flow/Inc_Laminar_Cavity/lam_buoyancy_cavity.cfg
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Expand Up @@ -77,7 +77,7 @@ MU_CONSTANT= 1.716e-5
CONDUCTIVITY_MODEL= CONSTANT_CONDUCTIVITY
%
% Molecular Thermal Conductivity that would be constant (0.0257 by default)
KT_CONSTANT= 0.0246295028571
THERMAL_CONDUCTIVITY_CONSTANT= 0.0246295028571

% ----------------------- BODY FORCE DEFINITION -------------------------------%
%
Expand Down
1 change: 0 additions & 1 deletion incompressible_flow/Inc_Streamwise_Periodic/sp_pinArray_2d_dp_hf_tp.cfg
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Expand Up @@ -102,7 +102,6 @@ TIME_DISCRE_TURB= EULER_IMPLICIT
%
% --------------------------- CONVERGENCE PARAMETERS --------------------------%
%
CONV_CRITERIA= RESIDUAL
CONV_FIELD= RMS_TEMPERATURE
CONV_RESIDUAL_MINVAL= -4.07
CONV_STARTITER= 10
Expand Down
1 change: 0 additions & 1 deletion incompressible_flow/Inc_Streamwise_Periodic/sp_pinArray_2d_mf_hf.cfg
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Expand Up @@ -107,7 +107,6 @@ TIME_DISCRE_TURB= EULER_IMPLICIT
%
% --------------------------- CONVERGENCE PARAMETERS --------------------------%
%
CONV_CRITERIA= RESIDUAL
CONV_FIELD= RMS_TEMPERATURE
CONV_RESIDUAL_MINVAL= -10.9
CONV_STARTITER= 10
Expand Down
66 changes: 16 additions & 50 deletions multiphysics/steady_cht/cht_2d_3cylinders.cfg
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Expand Up @@ -5,10 +5,9 @@
% Author: O. Burghardt, T. Economon %
% Institution: Chair for Scientific Computing, TU Kaiserslautern %
% Date: August 8, 2019 %
% File Version 6.0.1 "Falcon" %
% File Version 7.1.1 "Blackbird" %
% %
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%

%
% Physical governing equations (EULER, NAVIER_STOKES,
% WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
Expand All @@ -18,67 +17,34 @@ SOLVER= MULTIPHYSICS
% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT, DISCRETE_ADJOINT)
MATH_PROBLEM= DIRECT
%
% Restart solution (NO, YES)
RESTART_SOL= NO
%
% Configuration file list, one for each physical zone
CONFIG_LIST= (flow_cylinder.cfg, solid_cylinder1.cfg, solid_cylinder2.cfg, solid_cylinder3.cfg)
CONFIG_LIST = (flow_cylinder.cfg, solid_cylinder1.cfg, solid_cylinder2.cfg, solid_cylinder3.cfg)
%
%
% Definition of the interface
MARKER_ZONE_INTERFACE= (cylinder_outer1, cylinder_inner1, cylinder_outer2, cylinder_inner2, cylinder_outer3, cylinder_inner3)
%
%
MARKER_CHT_INTERFACE= (cylinder_outer1, cylinder_inner1, cylinder_outer2, cylinder_inner2, cylinder_outer3, cylinder_inner3)
%
% Objective function in gradient evaluation (DRAG, LIFT, SIDEFORCE, MOMENT_X,
% MOMENT_Y, MOMENT_Z, EFFICIENCY,
% EQUIVALENT_AREA, NEARFIELD_PRESSURE,
% FORCE_X, FORCE_Y, FORCE_Z, THRUST,
% TORQUE, TOTAL_HEATFLUX,
% MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
% INVERSE_DESIGN_HEATFLUX, SURFACE_TOTAL_PRESSURE,
% SURFACE_MASSFLOW, SURFACE_STATIC_PRESSURE, SURFACE_MACH)
% For a weighted sum of objectives: separate by commas, add OBJECTIVE_WEIGHT and MARKER_MONITORING in matching order.
OBJECTIVE_FUNCTION= TOTAL_HEATFLUX
%
% List of weighting values when using more than one OBJECTIVE_FUNCTION. Separate by commas and match with MARKER_MONITORING.
OBJECTIVE_WEIGHT= 1.0
CHT_COUPLING_METHOD= DIRECT_TEMPERATURE_ROBIN_HEATFLUX
%
%
TIME_DOMAIN = NO
%
% Number of total iterations
OUTER_ITER = 15000
OUTPUT_WRT_FREQ = 15000
% Number of total iterations (15000 for suitable results)
OUTER_ITER = 11
%
% Mesh input file
MESH_FILENAME= mesh_cht_3cyl_ffd.su2
MESH_OUT_FILENAME= mesh_cht_3cyl_out.su2
%
% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
MESH_FORMAT= SU2
%
% Output file format
OUTPUT_FILES= (RESTART, TECPLOT, PARAVIEW, SURFACE_TECPLOT, SURFACE_PARAVIEW)
%
% Multizone convergence criteria
CONV_RESIDUAL_MINVAL= -20

% -------------------- FREE-FORM DEFORMATION PARAMETERS -----------------------%
%
% Tolerance of the Free-Form Deformation point inversion
FFD_TOLERANCE= 1E-12
%
% Maximum number of iterations in the Free-Form Deformation point inversion
FFD_ITERATIONS= 500
%
% FFD box definition: 3D case (FFD_BoxTag, X1, Y1, Z1, X2, Y2, Z2, X3, Y3, Z3, X4, Y4, Z4,
% X5, Y5, Z5, X6, Y6, Z6, X7, Y7, Z7, X8, Y8, Z8)
% 2D case (FFD_BoxTag, X1, Y1, 0.0, X2, Y2, 0.0, X3, Y3, 0.0, X4, Y4, 0.0,
% 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)
FFD_DEFINITION= (MAIN_BOX, -0.1, -0.6, 0.0, 1.1, -0.6, 0.0, 1.1, 0.6, 0.0, -0.1, 0.6, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)
%
% FFD box degree: 3D case (x_degree, y_degree, z_degree)
% 2D case (x_degree, y_degree, 0)
FFD_DEGREE= ( 24, 1, 0)
OUTPUT_FILES= (RESTART, PARAVIEW_MULTIBLOCK)
%
% Surface continuity at the intersection with the FFD (1ST_DERIVATIVE, 2ND_DERIVATIVE)
FFD_CONTINUITY= 2ND_DERIVATIVE
% These are just default parameters so that we can run SU2_DOT_AD, they have no physical meaning for this test case.

% ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
%
Expand All @@ -87,10 +53,10 @@ FFD_CONTINUITY= 2ND_DERIVATIVE
% FFD_CONTROL_POINT, FFD_CAMBER, FFD_THICKNESS, FFD_TWIST
% FFD_CONTROL_POINT_2D, FFD_CAMBER_2D, FFD_THICKNESS_2D, FFD_TWIST_2D,
% HICKS_HENNE, SURFACE_BUMP)
DV_KIND= FFD_CONTROL_POINT_2D
DV_KIND= HICKS_HENNE
%
% Marker of the surface in which we are going apply the shape deformation
DV_MARKER= (cylinder_outer1, cylinder_inner1, cylinder_outer2, cylinder_inner2, cylinder_outer3, cylinder_inner3)
DV_MARKER= ( cylinder_outer1, cylinder_inner1, cylinder_outer2, cylinder_inner2, cylinder_outer3, cylinder_inner3 )
%
% Parameters of the shape deformation
% - NO_DEFORMATION ( 1.0 )
Expand All @@ -112,7 +78,7 @@ DV_MARKER= (cylinder_outer1, cylinder_inner1, cylinder_outer2, cylinder_inner2,
% - FFD_TWIST_2D ( FFD_BoxTag, x_Orig, y_Orig )
% - HICKS_HENNE ( Lower Surface (0)/Upper Surface (1)/Only one Surface (2), x_Loc )
% - SURFACE_BUMP ( x_Start, x_End, x_Loc )
DV_PARAM= ( MAIN_BOX, 12, 1, 0.0, 1.0 )
DV_PARAM= (0.0, 0.5)
%
% Value of the shape deformation
DV_VALUE= 0.1
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