Potential bug in airfoil optimization #231
Description
The translation from problem configuration to mach aero input appears to pass the Reynolds number to the mach input:
self.__design_to_simulator_input( starting_point, reynolds=args.reynolds, mach=args.reynolds, temperature=args.temperature, filename=filename )
Additionally the output returns the initial angle of attack instead of the optimized value (but returns the optimized coordinates). Is this intended?
return {"coords": opt_coords, "angle_of_attack": starting_point["angle_of_attack"]}, optisteps_history
This is in the optimization() function of engibench/problems/airfoil/v0.py