GitHub - 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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Name		Name	Last commit message	Last commit date
Latest commit History 14 Commits
MECH_6121_Project.pdf		MECH_6121_Project.pdf
Panel method Kuethe and Chow-Foundations-of-Aerodynamics.pdf		Panel method Kuethe and Chow-Foundations-of-Aerodynamics.pdf
Performance Characteristics of a NACA 4 digit airfoil.m		Performance Characteristics of a NACA 4 digit airfoil.m

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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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