feature request xfoil:XYCM for airfoildb generation

[Marco]

Hi,

I am working on a Spratt controllwing, for this it is necessary to change xfoils default moment reference location (XYCM 0.25 0.00) to a different value.

could you please add

line 1840

xycm = kwargs.get("xycm", [0.25, 0.00])

line 1929

commands += ['XYCM',
                         str(xycm[0]),
                         str(xycm[1])]

to the airfoil.py code for me?

thanks, marco

[Cory]

Hi Marco

I can do that. I'll let you know when I have that added.

Thanks

Cory

[Cory]

Hi Marco

I have this added, along with being able to specify the camber line solver termination tolerance. Let me know if you have any issues.

Thanks

Cory