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Karman-Pohlhausen-Approach-of-solving-the-boundary-layer-over-an-arbitrary-airfoil
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Source-Vortex-Panel-Method-Potential-Flow-implementation
Source-Vortex-Panel-Method-Potential-Flow-implementation PublicThis project will be discussing one method of evaluating the potential flow (Ideal flow) over 3 airfoils; NACA 0006, NACA 0012, NACA 0018. Computing the Coefficient of lift of the airfoil at 0 angl…
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