Panel method problem -- CFD Online Discussion Forums

June 12, 2003, 05:53	Panel method problem	#1
niavarani Guest Posts: n/a	Hi I have a problem in panel method. I have designed an airfoil with EPPLER code. Eppler gives me a cusp airfoil , but when I use panel method to analyze my eppler out put airfoil, I have problem in trailing edge and lower surface of it. Can panel method analyze cusp airfoil or it must be sharp? Thanks

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