I want a bezier code with 8 parameters for aerodynamic profile optimization The 8 parameters will define the full airfoil, top as well as bottom surface as a single curve This code should be usable in xflr5
hey guys I would really like some help regarding analysis of a cylinder in xflr. i tried using circle based airfoils to do analysis in foil design but it never converges. i have seen posts here of cylinder analysis but i have no idea about it. I would appreciate some help. thankyou