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Merged
merged 20 commits into from
Nov 27, 2019
Merged

Tutorial Updates for v7 #24

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5f9d3e3
updating tutorial for new fixed cl mode
jayantmukho Sep 20, 2019
a5b10b1
updating DV definition numbers to be consistent with new definition
jayantmukho Sep 23, 2019
e8077c0
more detail about fixed cl mode
jayantmukho Sep 23, 2019
ef87988
removing last traces of UPDATE_ALPHA
jayantmukho Sep 24, 2019
8ffe582
change some options for better convergence
jayantmukho Sep 24, 2019
a7c2941
added ITER option for oneram6 design
jayantmukho Sep 24, 2019
ad132e8
minor fixes
jayantmukho Sep 24, 2019
5554595
removed ITER option
jayantmukho Sep 24, 2019
eb9a70d
changed options in tutorial page
jayantmukho Sep 24, 2019
0b617df
merge with develop
jayantmukho Oct 15, 2019
69d284d
Merge pull request #16 from su2code/enhancement_fixed_cl
jayantmukho Oct 22, 2019
490be0f
replace DEFORM_LINEAR_ITER by DEFORM_LINEAR_SOLVER_ITER
pcarruscag Oct 24, 2019
d7868cf
Merge pull request #21 from su2code/cleanup_linsol_options
talbring Oct 28, 2019
d198513
Small typos.
economon Oct 31, 2019
88325de
Update for Inc_Heated_Cylinders config files.
oleburghardt Nov 4, 2019
d0bc80b
Remove old solution files (outdated format).
oleburghardt Nov 4, 2019
6628bc2
Add binary solution files for Inc_Heated_Cylinders.
oleburghardt Nov 4, 2019
1811e61
Update to tutorial files and docs Part I.
economon Nov 22, 2019
4a6ff7a
Tutorial updates Part II for v7.
economon Nov 25, 2019
ceaeacc
Two fixes for tutorial regressions.
economon Nov 26, 2019
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13 changes: 7 additions & 6 deletions Inc_Heated_Cylinders/cht_2d_3cylinders.cfg
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Original file line number Diff line number Diff line change
Expand Up @@ -15,21 +15,18 @@
% POISSON_EQUATION)
SOLVER= MULTIPHYSICS
%
% Regime type (COMPRESSIBLE, INCOMPRESSIBLE, FREESURFACE)
% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT, DISCRETE_ADJOINT)
MATH_PROBLEM= DIRECT
%
%
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)
%
%
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)
%
%
TIME_DOMAIN = NO
%
% Number of total iterations
OUTER_ITER = 10000
%
Expand All @@ -38,6 +35,10 @@ MESH_FILENAME= mesh_cht_3cyl.su2
%
% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
MESH_FORMAT= SU2
%
% Output file format
OUTPUT_FILES= (RESTART, TECPLOT, PARAVIEW, SURFACE_TECPLOT, SURFACE_PARAVIEW)


% These are just default parameters so that we can run SU2_DOT_AD, they have no physical meaning for this test case.

Expand All @@ -51,7 +52,7 @@ MESH_FORMAT= SU2
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 Down
16 changes: 3 additions & 13 deletions Inc_Heated_Cylinders/flow_cylinder.cfg
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Expand Up @@ -30,16 +30,10 @@ RESTART_SOL= NO
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
%
% Read binary restart files (YES, NO)
READ_BINARY_RESTART = NO
%
% Write binary restart files (YES, NO)
WRT_BINARY_RESTART = NO
OBJECTIVE_WEIGHT= 1.0
%
% Data written to history file
HISTORY_OUTPUT=(ITER, RMS_RES, HEAT )
HISTORY_OUTPUT= (ITER, RMS_RES, HEAT)

% -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
%
Expand Down Expand Up @@ -199,10 +193,6 @@ SOLUTION_FILENAME= solution_flow.dat
% Restart adjoint input file
SOLUTION_ADJ_FILENAME= solution_adj.dat
%
% Output file format (TECPLOT, TECPLOT_BINARY, PARAVIEW,
% FIELDVIEW, FIELDVIEW_BINARY)
OUTPUT_FORMAT= TECPLOT
%
% Output file convergence history (w/o extension)
CONV_FILENAME= history
%
Expand Down Expand Up @@ -245,7 +235,7 @@ WRT_CON_FREQ= 1
DEFORM_LINEAR_SOLVER= FGMRES
%
% Number of smoothing iterations for mesh deformation
DEFORM_LINEAR_ITER= 200
DEFORM_LINEAR_SOLVER_ITER= 200
%
% Number of nonlinear deformation iterations (surface deformation increments)
DEFORM_NONLINEAR_ITER= 1
Expand Down
16 changes: 3 additions & 13 deletions Inc_Heated_Cylinders/solid_cylinder1.cfg
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Expand Up @@ -28,12 +28,6 @@ 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
%
% Read binary restart files (YES, NO)
READ_BINARY_RESTART = NO
%
% Write binary restart files (YES, NO)
WRT_BINARY_RESTART = NO

% -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
%
Expand All @@ -59,10 +53,10 @@ SOLID_TEMPERATURE_INIT= 350.0
SOLID_DENSITY= 0.000210322
%
% Solid specific heat (J/kg*K)
SPECIFIC_HEAT_CP_SOLID = 1004.703
SPECIFIC_HEAT_CP = 1004.703
%
% Solid thermal conductivity (W/m*K)
THERMAL_CONDUCTIVITY_SOLID= 0.1028
SOLID_THERMAL_CONDUCTIVITY= 0.1028

% ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
%
Expand Down Expand Up @@ -127,10 +121,6 @@ SOLUTION_FILENAME= solution_flow.dat
% Restart adjoint input file
SOLUTION_ADJ_FILENAME= solution_adj.dat
%
% Output file format (TECPLOT, TECPLOT_BINARY, PARAVIEW,
% FIELDVIEW, FIELDVIEW_BINARY)
OUTPUT_FORMAT= TECPLOT
%
% Output file convergence history (w/o extension)
CONV_FILENAME= history
%
Expand Down Expand Up @@ -173,7 +163,7 @@ WRT_CON_FREQ= 1
DEFORM_LINEAR_SOLVER= FGMRES
%
% Number of smoothing iterations for mesh deformation
DEFORM_LINEAR_ITER= 200
DEFORM_LINEAR_SOLVER_ITER= 200
%
% Number of nonlinear deformation iterations (surface deformation increments)
DEFORM_NONLINEAR_ITER= 1
Expand Down
16 changes: 3 additions & 13 deletions Inc_Heated_Cylinders/solid_cylinder2.cfg
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Expand Up @@ -28,12 +28,6 @@ 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
%
% Read binary restart files (YES, NO)
READ_BINARY_RESTART = NO
%
% Write binary restart files (YES, NO)
WRT_BINARY_RESTART = NO

% -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
%
Expand All @@ -59,10 +53,10 @@ SOLID_TEMPERATURE_INIT= 350.0
SOLID_DENSITY= 0.000210322
%
% Solid specific heat (J/kg*K)
SPECIFIC_HEAT_CP_SOLID = 1004.703
SPECIFIC_HEAT_CP = 1004.703
%
% Solid thermal conductivity (W/m*K)
THERMAL_CONDUCTIVITY_SOLID= 0.1028
SOLID_THERMAL_CONDUCTIVITY= 0.1028

% ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
%
Expand Down Expand Up @@ -137,10 +131,6 @@ SOLUTION_FILENAME= solution_flow.dat
% Restart adjoint input file
SOLUTION_ADJ_FILENAME= solution_adj.dat
%
% Output file format (TECPLOT, TECPLOT_BINARY, PARAVIEW,
% FIELDVIEW, FIELDVIEW_BINARY)
OUTPUT_FORMAT= TECPLOT
%
% Output file convergence history (w/o extension)
CONV_FILENAME= history
%
Expand Down Expand Up @@ -183,7 +173,7 @@ WRT_CON_FREQ= 1
DEFORM_LINEAR_SOLVER= FGMRES
%
% Number of smoothing iterations for mesh deformation
DEFORM_LINEAR_ITER= 200
DEFORM_LINEAR_SOLVER_ITER= 200
%
% Number of nonlinear deformation iterations (surface deformation increments)
DEFORM_NONLINEAR_ITER= 1
Expand Down
16 changes: 3 additions & 13 deletions Inc_Heated_Cylinders/solid_cylinder3.cfg
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Expand Up @@ -28,12 +28,6 @@ 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
%
% Read binary restart files (YES, NO)
READ_BINARY_RESTART = NO
%
% Write binary restart files (YES, NO)
WRT_BINARY_RESTART = NO

% -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
%
Expand All @@ -59,10 +53,10 @@ SOLID_TEMPERATURE_INIT= 350.0
SOLID_DENSITY= 0.000210322
%
% Solid specific heat (J/kg*K)
SPECIFIC_HEAT_CP_SOLID = 1004.703
SPECIFIC_HEAT_CP = 1004.703
%
% Solid thermal conductivity (W/m*K)
THERMAL_CONDUCTIVITY_SOLID= 0.1028
SOLID_THERMAL_CONDUCTIVITY= 0.1028

% ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
%
Expand Down Expand Up @@ -137,10 +131,6 @@ SOLUTION_FILENAME= solution_flow.dat
% Restart adjoint input file
SOLUTION_ADJ_FILENAME= solution_adj.dat
%
% Output file format (TECPLOT, TECPLOT_BINARY, PARAVIEW,
% FIELDVIEW, FIELDVIEW_BINARY)
OUTPUT_FORMAT= TECPLOT
%
% Output file convergence history (w/o extension)
CONV_FILENAME= history
%
Expand Down Expand Up @@ -183,7 +173,7 @@ WRT_CON_FREQ= 1
DEFORM_LINEAR_SOLVER= FGMRES
%
% Number of smoothing iterations for mesh deformation
DEFORM_LINEAR_ITER= 200
DEFORM_LINEAR_SOLVER_ITER= 200
%
% Number of nonlinear deformation iterations (surface deformation increments)
DEFORM_NONLINEAR_ITER= 1
Expand Down
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Binary file modified Inc_Heated_Cylinders/solution_flow_1.dat
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Binary file modified Inc_Heated_Cylinders/solution_flow_2.dat
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Binary file modified Inc_Heated_Cylinders/solution_flow_3.dat
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7 changes: 3 additions & 4 deletions Inc_Inviscid_Hydrofoil/inv_naca0012.cfg
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Expand Up @@ -155,11 +155,10 @@ TIME_DISCRE_FLOW= EULER_IMPLICIT
% --------------------------- CONVERGENCE PARAMETERS --------------------------%
% Convergence criteria (CAUCHY, RESIDUAL)
%
CONV_CRITERIA= RESIDUAL
%
CONV_FIELD= RMS_PRESSURE
%
% Min value of the residual (log10 of the residual)
CONV_RESIDUAL_MINVAL= -18
CONV_RESIDUAL_MINVAL= -15
%
% Start Cauchy criteria at iteration number
CONV_STARTITER= 10
Expand Down Expand Up @@ -204,4 +203,4 @@ WRT_SOL_FREQ= 50
WRT_CON_FREQ= 1
%
% Screen output
SCREEN_OUTPUT= (INNER_ITER, RMS_PRESSURE, RMS_VELOCITY-X, LIFT, DRAG)
SCREEN_OUTPUT= (INNER_ITER, WALL_TIME, RMS_PRESSURE, RMS_VELOCITY-X, LIFT, DRAG)
31 changes: 10 additions & 21 deletions Inc_Laminar_Cavity/lam_buoyancy_cavity.cfg
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Expand Up @@ -15,7 +15,6 @@
% POISSON_EQUATION)
SOLVER= INC_NAVIER_STOKES
%
%
% Specify turbulent model (NONE, SA, SA_NEG, SST)
KIND_TURB_MODEL= NONE
%
Expand Down Expand Up @@ -123,11 +122,11 @@ NUM_METHOD_GRAD= GREEN_GAUSS
CFL_NUMBER= 50.0
%
% Adaptive CFL number (NO, YES)
CFL_ADAPT= NO
CFL_ADAPT= YES
%
% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
% CFL max value )
CFL_ADAPT_PARAM= ( 1.5, 0.5, 15.0, 1e10)
CFL_ADAPT_PARAM= ( 0.1, 2.0, 50.0, 1e10)
%
% Maximum Delta Time in local time stepping simulations
MAX_DELTA_TIME= 1E6
Expand All @@ -153,18 +152,18 @@ LINEAR_SOLVER_ILU_FILL_IN= 0
LINEAR_SOLVER_ERROR= 1E-15
%
% Max number of iterations of the linear solver for the implicit formulation
LINEAR_SOLVER_ITER= 10
LINEAR_SOLVER_ITER= 30

% -------------------------- MULTIGRID PARAMETERS -----------------------------%
%
% Multi-Grid Levels (0 = no multi-grid)
MGLEVEL= 2
MGLEVEL= 0
%
% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
MGCYCLE= V_CYCLE
%
% Multi-grid pre-smoothing level
MG_PRE_SMOOTH= ( 1, 1, 1, 1 )
MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
%
% Multi-grid post-smoothing level
MG_POST_SMOOTH= ( 0, 0, 0, 0 )
Expand All @@ -173,10 +172,10 @@ MG_POST_SMOOTH= ( 0, 0, 0, 0 )
MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
%
% Damping factor for the residual restriction
MG_DAMP_RESTRICTION= 0.8
MG_DAMP_RESTRICTION= 0.95
%
% Damping factor for the correction prolongation
MG_DAMP_PROLONGATION= 0.8
MG_DAMP_PROLONGATION= 0.95

% -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
%
Expand All @@ -199,11 +198,10 @@ TIME_DISCRE_FLOW= EULER_IMPLICIT
% --------------------------- CONVERGENCE PARAMETERS --------------------------%
%
% Convergence criteria (CAUCHY, RESIDUAL)
CONV_CRITERIA= RESIDUAL
%
CONV_FIELD= RMS_TEMPERATURE
%
% Min value of the residual (log10 of the residual)
CONV_RESIDUAL_MINVAL= -12
CONV_RESIDUAL_MINVAL= -8
%
% Start convergence criteria at iteration number
CONV_STARTITER= 10
Expand All @@ -213,7 +211,6 @@ CONV_CAUCHY_ELEMS= 100
%
% Epsilon to control the series convergence
CONV_CAUCHY_EPS= 1E-6
%

% ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
%
Expand Down Expand Up @@ -266,12 +263,4 @@ WRT_SOL_FREQ= 100
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)
WRT_SLICE= YES
%
% Geometrical bounds (Y coordinate) for the wing geometry analysis or
% fuselage evaluation (X coordinate).
GEO_BOUNDS= ( 0.499, 0.501)
SCREEN_OUTPUT= (INNER_ITER, WALL_TIME, RMS_PRESSURE, RMS_TEMPERATURE, LIFT, DRAG)
23 changes: 6 additions & 17 deletions Inc_Laminar_Flat_Plate/lam_flatplate.cfg
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Expand Up @@ -135,11 +135,11 @@ NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
CFL_NUMBER= 15.0
%
% Adaptive CFL number (NO, YES)
CFL_ADAPT= NO
CFL_ADAPT= YES
%
% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
% CFL max value )
CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
CFL_ADAPT_PARAM= ( 0.1, 2.0, 1.0, 1e10 )
%
% Number of total iterations
ITER= 99999
Expand All @@ -164,7 +164,7 @@ LINEAR_SOLVER_ITER= 25
% -------------------------- MULTIGRID PARAMETERS -----------------------------%
%
% Multi-Grid Levels (0 = no multi-grid)
MGLEVEL= 3
MGLEVEL= 0
%
% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
MGCYCLE= W_CYCLE
Expand Down Expand Up @@ -209,12 +209,10 @@ TIME_DISCRE_FLOW= EULER_IMPLICIT
% --------------------------- CONVERGENCE PARAMETERS --------------------------%
%
% Convergence criteria (CAUCHY, RESIDUAL)
%
CONV_CRITERIA= RESIDUAL
%
CONV_FIELD= RMS_PRESSURE
%
% Min value of the residual (log10 of the residual)
CONV_RESIDUAL_MINVAL= -14
CONV_RESIDUAL_MINVAL= -16
%
% Start convergence criteria at iteration number
CONV_STARTITER= 10
Expand All @@ -224,7 +222,6 @@ CONV_CAUCHY_ELEMS= 100
%
% Epsilon to control the series convergence
CONV_CAUCHY_EPS= 1E-6
%

% ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
%
Expand Down Expand Up @@ -277,12 +274,4 @@ WRT_SOL_FREQ= 250
WRT_CON_FREQ= 1
%
% Screen output
SCREEN_OUTPUT= (INNER_ITER, RMS_PRESSURE, RMS_VELOCITY-X, LIFT, DRAG)

% ----------------------- GEOMETRY EVALUATION PARAMETERS ----------------------%
%
WRT_SLICE= YES
%
% Geometrical bounds (Y coordinate) for the wing geometry analysis or
% fuselage evaluation (X coordinate).
GEO_BOUNDS= ( 0.304, 0.305)
SCREEN_OUTPUT= (INNER_ITER, WALL_TIME, RMS_PRESSURE, RMS_VELOCITY-X, LIFT, DRAG)
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