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somethnextra · 10-03-2007, 09:41 AM

Shaker is right. Take a look at Abbott and Von Doenhoff data. The thickness of an airfoil affects post stall characteristics. That is, after the airfoil reaches max lift/aoa. For a given airfoil of varying thickness both are the same.

10-03-2007, 09:41 AM	#6 (permalink)
somethnextra doin' it Join Date: Mar 2006 Location: Milton, FL Age: 23 Posts: 28	Re: Leading Edge shape Shaker is right. Take a look at Abbott and Von Doenhoff data. The thickness of an airfoil affects post stall characteristics. That is, after the airfoil reaches max lift/aoa. For a given airfoil of varying thickness both are the same.