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studentFLUENT - Mesh Library - AIRFOIL
Airfoil flow domain with mesh boundaries displayed.
Two-dimensional mesh files for the following airfoils: Clark-K, Clark-V, Clark-W, Clark-X, Clark-Y, NACA-2411, NACA-2414, NACA-2415, and NACA-32012. The chord length for each airfoil is unity.
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