Hi,
I'm quite new using OpenVSP and VSPAero, and I would like to model a plain flap for a future mesh for CFD. I know that there is a control group function in VSPAero but it seems that it doesn't change the geometry indeed, as it takes it into account when VLM is calculated only.
How can I model a flap? The wing is quite simple, from a UAV, a rectangular wing without any twist and AR approximately 10.
Thanks,
Agustin