Panel Flow method
I am currently investigating several aerofoil designs and their behaviour
when in close proximity to each other. I am interested to know if I am able
to use your software to simulate the coanda effect, especially with
multi-element wings (3 elements). The type of wing arrangement I am looking
to replicate is an internal wing aircraft. If you are able to advise on
this it would be greatly appreciated.
[Edit: based on an email exchange]