Ok trying to explain myself clearer....
this is just a bogus wing as an example... So think of it as the part of the wing where the ailerons are and I've deflected it fully down and I need to understand how this effects the co-efficient of lift for this particular section.
I then analyze the airfoils performance at various angles of attack and reynolds numbers
I then cut-n-paste into a spreadsheet and from there into JSBsim xml file.... but as you can see the copy text is greyed out and I can no longer do this....
Can someone help me understand why ?
Simon