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Fix CUSTOM_OBJFUNC and TAVG_CUSTOM_OBJFUNC missing from historyMap #2747

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Fix CUSTOM_OBJFUNC and TAVG_CUSTOM_OBJFUNC missing from historyMap #2747

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14 changes: 14 additions & 0 deletions SU2_PY/SU2/io/historyMap.py
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Original file line number Diff line number Diff line change
Expand Up @@ -310,6 +310,20 @@
"HEADER": "ComboObj",
"TYPE": "COEFFICIENT",
},
# Steady adjoint fix
"CUSTOM_OBJFUNC": {
"DESCRIPTION": "Custom objective function.",
"GROUP": "COMBO",
"HEADER": "ComboObj",
"TYPE": "COEFFICIENT",
},
# Unsteady adjoint fix
"TAVG_CUSTOM_OBJFUNC": {
"DESCRIPTION": "weighted time average value",
"GROUP": "TAVG_COMBO",
"HEADER": "tavg[ComboObj]",
"TYPE": "TAVG_COEFFICIENT",
},
"DEFORM_ITER": {
"DESCRIPTION": "Linear solver iterations for the mesh " "deformation",
"GROUP": "DEFORM",
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9 changes: 7 additions & 2 deletions TestCases/optimization_euler/steady_naca0012/inv_NACA0012_basic.cfg
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Expand Up @@ -130,10 +130,15 @@ OUTPUT_WRT_FREQ= 250

% --------------------- OPTIMAL SHAPE DESIGN DEFINITION -----------------------%
%
OPT_OBJECTIVE= DRAG * 0.001
CUSTOM_OUTPUTS= 'P50_avg : AreaAvg{pow(PRESSURE,50)}[airfoil]; P_pnorm50 : Function{pow(P50_avg, 1.0/50.0)}'
CUSTOM_OBJFUNC= 'P_pnorm50'
OBJECTIVE_FUNCTION= CUSTOM_OBJFUNC
OPT_OBJECTIVE= CUSTOM_OBJFUNC * 1.0
OPT_CONSTRAINT= NONE
OPT_ITERATIONS= 100
OPT_ITERATIONS= 2
OPT_ACCURACY= 1E-6
OPT_BOUND_UPPER= 0.1
OPT_BOUND_LOWER= -0.1
DEFINITION_DV= ( 30, 1.0 | airfoil | 0, 0.05 ); ( 30, 1.0 | airfoil | 0, 0.10 ); ( 30, 1.0 | airfoil | 0, 0.15 ); ( 30, 1.0 | airfoil | 0, 0.20 ); ( 30, 1.0 | airfoil | 0, 0.25 ); ( 30, 1.0 | airfoil | 0, 0.30 ); ( 30, 1.0 | airfoil | 0, 0.35 ); ( 30, 1.0 | airfoil | 0, 0.40 ); ( 30, 1.0 | airfoil | 0, 0.45 ); ( 30, 1.0 | airfoil | 0, 0.50 ); ( 30, 1.0 | airfoil | 0, 0.55 ); ( 30, 1.0 | airfoil | 0, 0.60 ); ( 30, 1.0 | airfoil | 0, 0.65 ); ( 30, 1.0 | airfoil | 0, 0.70 ); ( 30, 1.0 | airfoil | 0, 0.75 ); ( 30, 1.0 | airfoil | 0, 0.80 ); ( 30, 1.0 | airfoil | 0, 0.85 ); ( 30, 1.0 | airfoil | 0, 0.90 ); ( 30, 1.0 | airfoil | 0, 0.95 ); ( 30, 1.0 | airfoil | 1, 0.05 ); ( 30, 1.0 | airfoil | 1, 0.10 ); ( 30, 1.0 | airfoil | 1, 0.15 ); ( 30, 1.0 | airfoil | 1, 0.20 ); ( 30, 1.0 | airfoil | 1, 0.25 ); ( 30, 1.0 | airfoil | 1, 0.30 ); ( 30, 1.0 | airfoil | 1, 0.35 ); ( 30, 1.0 | airfoil | 1, 0.40 ); ( 30, 1.0 | airfoil | 1, 0.45 ); ( 30, 1.0 | airfoil | 1, 0.50 ); ( 30, 1.0 | airfoil | 1, 0.55 ); ( 30, 1.0 | airfoil | 1, 0.60 ); ( 30, 1.0 | airfoil | 1, 0.65 ); ( 30, 1.0 | airfoil | 1, 0.70 ); ( 30, 1.0 | airfoil | 1, 0.75 ); ( 30, 1.0 | airfoil | 1, 0.80 ); ( 30, 1.0 | airfoil | 1, 0.85 ); ( 30, 1.0 | airfoil | 1, 0.90 ); ( 30, 1.0 | airfoil | 1, 0.95 )
RESTART_SOL= NO
READ_BINARY_RESTART= NO
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