Airfoil Generation & making grid over it.
I am writing a code by elliptic grid generation technique for any naca 4 series airfoils given as input. please tell me how to generate the data for any naca 4 series airfoils. thanks in advance.
have a nice week end. r.v.ramkumar July 17.
Re: Airfoil Generation & making grid over it.
You can find the equation for the thickness and camber of NACA 4-digit series airfoils in the "Theory of wing sections" by Abbott and Von Deonhoff. It is not very tough to wirte a computer code for that.
Good luck, Uma
I have written the code but I am getting infinite values in output.any idea why so?
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