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owaisali10 / MATLAB-code-for-a-4-digit-NACA-airfoil

Performance characteristics of a 4-digit NACA airfoil. Kuethe and Chow Vortex Panel Method, Thin airfoil method and the Finite Wing Method is used. The resulting values are also compared.

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Performance characteristics of a 4-digit NACA airfoil. Kuethe and Chow Vortex Panel Method, Thin airfoil method and the Finite Wing Method is used. The resulting values are also compared.

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