naca2412

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MATLAB + thin-airfoil-theory study of a 20% chord leading-edge flap on a NACA 2412 airfoil (geometry rotation + flap effectiveness plots).

matlab aerodynamics airfoil flaps thin-airfoil-theory naca2412

Second aerospace project that analyzes airfoil

python aerospace tkinter aerodynamics cyberpunk airfoil-analysis naca2412

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