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Williams airfoil

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Revision as of 07:59, 19 September 2005 by Praveen (Talk | contribs)
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This test case consists of inviscid flow past the two-element Williams airfoil at a Mach number of 0.15 and zero angle of attack.

Pressure coefficient on airfoil and flap

The pressure coefficient on the main airfoil and flap are compared with the exact potential solution.

Williams airfoil - Main airfoil

Williams airfoil - Flap


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