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Fix option names in config_template.cfg that SU2 does not accept #2904

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Fix option names in config_template.cfg that SU2 does not accept #2904

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34 changes: 9 additions & 25 deletions config_template.cfg
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Original file line number Diff line number Diff line change
Expand Up @@ -418,7 +418,7 @@ ITER_DCL_DALPHA= 500
EVAL_DOF_DCX= NO
%
% Damping factor for thrust BC (actuator disk).
NETTHRUST_DBCTHRUST= 1.0
DNETTHRUST_DBCTHRUST= 1.0
%
% parameter for the definition of a complex objective function
DCD_DCL_VALUE= 0.0
Expand Down Expand Up @@ -664,15 +664,12 @@ MOVE_MOTION_ORIGIN = 0

% ------------------------- BUFFET SENSOR DEFINITION --------------------------%
%
% Compute the Kenway-Martins separation sensor for buffet-onset detection
% If BUFFET objective/constraint is specified, the objective is given by
% the integrated sensor normalized by reference area
% The Kenway-Martins separation sensor for buffet-onset detection is computed
% on Navier-Stokes markers. If BUFFET objective/constraint is specified, the
% objective is given by the integrated sensor normalized by reference area
Comment on lines +667 to +669

@ManasBagul23 ManasBagul23 Sep 17, 2026

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The Python side (the key injected in SU2_PY/SU2/io/config.py) is fixed in #2905, so the two PRs together cover both places.

%
% See doi: 10.2514/1.J055172
%
% Evaluate buffet sensor on Navier-Stokes markers (NO, YES)
BUFFET_MONITORING= NO
%
% Sharpness coefficient for the buffet sensor Heaviside function
BUFFET_K= 10.0
%
Expand Down Expand Up @@ -871,9 +868,6 @@ HB_PRECONDITION= NO
% Omega_HB = 2*PI*frequency - frequencies for Harmonic Balance method
OMEGA_HB= (0,1.0,-1.0)
%
% Determines if the single-zone driver is used. (deprecated)
SINGLEZONE_DRIVER= NO
%
% Determines if the special output is written out
SPECIAL_OUTPUT= NO

Expand Down Expand Up @@ -1013,7 +1007,7 @@ CONTROLLING_VARIABLE_SOURCE_NAMES= (ProdRateTot_PV, NULL)
% Method used to ignite the solution:
% FLAME_FRONT : the flame is initialized using a plane, defined by a point and a normal. On one side, the solution is initialized
% using 'burnt' conditions and on the other side 'unburnt' conditions. The normal points in the direction of the 'burnt'
% condition. The 'burnt' condition is defined as the value of the progress variable for which the temperature exceeds the IGNITION_TEMPERATURE.
% condition. The 'burnt' condition is defined as the value of the progress variable for which the temperature exceeds the FLAME_INIT_IGNITION.
% SPARK : the solution is ignited through application of a set of source terms within a specified region for a set number
% of solver iterations. This artificial spark can be applied after a certain number of iterations has passed, allowing for
% the flow to evolve before igniting the mixture.
Expand Down Expand Up @@ -1047,6 +1041,8 @@ FLAME_INIT= (0.004, 0.0, 0.0, 1.0, 0.0, 0.0, 0.2e-3, 1.0)
% in the flamelet data space.
% The SPARK_REACTION_RATES are applied within the spark region when the local temperature is below the
% flame ignition temperature.
% With THICKENED_FLAME_CORRECTION, flame thickness calculations are performed when the maximum temperature
% in the flow solution exceeds this value.
FLAME_INIT_IGNITION= 5000.0

% SPARK initialization
Expand All @@ -1068,10 +1064,6 @@ SPARK_REACTION_RATES= (1000, 0, 0)
% than the flame thickness.
THICKENED_FLAME_CORRECTION= YES

% Flame ignition temperature
% Flame thickness calculations are performed when the maximum temperature in the flow solution exceeds this value.
IGNITION_TEMPERATURE= 1100.0

%
% --------------------- INVERSE DESIGN SIMULATION -----------------------------%
%
Expand Down Expand Up @@ -1809,11 +1801,6 @@ MG_STARTUP_STAGNATION= 0.99
% 0 disables the criterion, as MG_STARTUP_STAGNATION= 0 does (default 5).
MG_STARTUP_STAGNATION_ITER= 5

% -------------------------- MESH SMOOTHING -----------------------------%
%
% Before each computation, implicitly smooth the nodal coordinates
SMOOTH_GEOMETRY= 0

% -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
%
% Convective numerical method (JST, JST_KE, JST_MAT, LAX-FRIEDRICH, ROE, AUSM,
Expand Down Expand Up @@ -2101,9 +2088,6 @@ USE_ACCURATE_TURB_JACOBIANS= NO
%
% --------------------- HEAT NUMERICAL METHOD DEFINITION ----------------------%
%
% Value of the thermal diffusivity
THERMAL_DIFFUSIVITY= 1.0
%
% Convective numerical method for the heat equation (only SCALAR_UPWIND)
CONV_NUM_METHOD_HEAT= SCALAR_UPWIND
%
Expand Down Expand Up @@ -2280,7 +2264,7 @@ DV_UNORDERED_SENS_FILENAME= unordered_sensitivity.dat
HOLD_GRID_FIXED= NO
%
% Coordinates of the box where the grid will be deformed (Xmin, Ymin, Zmin, Xmax, Ymax, Zmax)
HOLD_GRID_FIXED_COORDS= (-1e15, -1e15, -1e15, 1e15, 1e15, 1e15)
HOLD_GRID_FIXED_COORD= (-1e15, -1e15, -1e15, 1e15, 1e15, 1e15)
%
% Design variable for FEA problems
% options: NONE, YOUNG_MODULUS, POISSON_RATIO, DENSITY, DEAD_WEIGHT, ELECTRIC_FIELD
Expand Down Expand Up @@ -2350,7 +2334,7 @@ DEFORM_LIMIT = 1E6
DEFORM_ELASTICITY_MODULUS= 2e11
%
% Poisson ratio for constant stiffness FEA method of grid deformation
DEFORM_POISSON_RATIO= 0.3
DEFORM_POISSONS_RATIO= 0.3
%
% Size of the layer of highest stiffness for wall distance-based mesh stiffness
DEFORM_STIFF_LAYER_SIZE= 0.0
Expand Down