missing file

Author: pcarruscag

TestCases/user_defined_functions/lam_flatplate.cfg

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+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+%                                                                              %
+% SU2 configuration file                                                       %
+% Case description: Test custom objective function.                            %
+% File Version 7.2.1 "Blackbird"                                               %
+%                                                                              %
+%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
+%
+SOLVER= NAVIER_STOKES
+KIND_TURB_MODEL= NONE
+RESTART_SOL= NO
+%
+% "COMBO" is the name and group of the output for the objective function
+% (regardless of definition).
+SCREEN_OUTPUT= INNER_ITER, RMS_DENSITY, RMS_ENERGY, LINSOL_RESIDUAL, FORCE_Z,\
+               SURFACE_MASSFLOW, SURFACE_TOTAL_TEMPERATURE, COMBO
+HISTORY_OUTPUT = ITER, AERO_COEFF, FLOW_COEFF, FLOW_COEFF_SURF, COMBO
+OBJECTIVE_FUNCTION= CUSTOM_OBJFUNC
+% Here we define how the custom objective is computed from other outputs. For 
+% example, force in the z direction (computed for all MARKER_MONITORING and part
+% of AERO_COEFF) plus the absolute value of massflow across the second surface
+% ([1]) in MARKER_ANALYZE, scaled by a factor of 1000. It is also possible to
+% use "per surface" values from MARKER_MONITORING (use the dry-run mode to see
+% the names of available outputs, e.g. SU2_CFD -d lam_flatplate.cfg).
+% For multizone problems the CUSTOM_OBJFUNC should be defined for each zone
+% individually (with the outputs of that zone), the total for the problem is
+% the sum over zones, see disc_adj_fsi/Airfoil_2d.
+CUSTOM_OBJFUNC= '1e3 * (FORCE_Z + fabs(SURFACE_MASSFLOW[1]))'
+
+% -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
+%
+MACH_NUMBER= 0.1
+INIT_OPTION= TD_CONDITIONS
+FREESTREAM_OPTION= TEMPERATURE_FS
+FREESTREAM_TEMPERATURE= 297.62
+REYNOLDS_NUMBER= 600
+REYNOLDS_LENGTH= 0.02
+
+% ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
+%
+REF_ORIGIN_MOMENT_X = 0.00
+REF_ORIGIN_MOMENT_Y = 0.00
+REF_ORIGIN_MOMENT_Z = 0.00
+REF_LENGTH= 0.02
+REF_AREA= 0.02
+%
+FLUID_MODEL= IDEAL_GAS
+GAMMA_VALUE= 1.4
+GAS_CONSTANT= 287.87
+VISCOSITY_MODEL= CONSTANT_VISCOSITY
+MU_CONSTANT= 0.001
+
+% -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
+%
+MARKER_HEATFLUX= ( y_minus, 0.0 )
+%
+MARKER_SYM= ( y_plus )
+MARKER_PERIODIC= ( x_minus, x_plus, 0,0,0, 0,0,0, 0.01,0,0 )
+%
+MARKER_INLET= ( z_minus, 300.0, 100000.0, 0.0, 0.0, 1.0 )
+MARKER_OUTLET= ( z_plus, 99000.0 )
+%
+MARKER_PLOTTING= ( y_minus )
+MARKER_MONITORING= ( y_minus )
+MARKER_ANALYZE= ( z_minus, z_plus )
+
+% ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
+%
+NUM_METHOD_GRAD= GREEN_GAUSS
+CFL_NUMBER= 1e4
+CFL_ADAPT= NO
+TIME_DISCRE_FLOW= EULER_IMPLICIT
+
+% ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
+%
+LINEAR_SOLVER= FGMRES
+LINEAR_SOLVER_PREC= ILU
+LINEAR_SOLVER_ERROR= 0.2
+LINEAR_SOLVER_ITER= 5
+
+% -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
+%
+CONV_NUM_METHOD_FLOW= ROE
+USE_VECTORIZATION= YES
+MUSCL_FLOW= YES
+SLOPE_LIMITER_FLOW= NONE
+
+% --------------------------- CONVERGENCE PARAMETERS --------------------------%
+%
+CONV_RESIDUAL_MINVAL= -11
+CONV_STARTITER= 0
+INNER_ITER= 1000
+
+% ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
+%
+MESH_FORMAT= BOX
+MESH_BOX_LENGTH= (0.01, 0.01, 0.1)
+MESH_BOX_SIZE= (9, 17, 65)
+