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Unformatted text preview: want to make minimal changes to the airfoil_examp code then you will want to transpose x & y after the call to naca4 to make them row vectors as in the examp Also the value of N after the call to naca4 should be equal to the number of panels: N=length(x)-1. Take care. It's easy to mess up the geometry. .. GIGO!...
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This document was uploaded on 01/22/2012.
- Fall '09