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Lift and Drag Coefficients of Airfoil
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0 Geometries 0 Meshes 0 Simulation setups 0 ResultsAbout this project
We will take the Airfoil NACA 0008 and for 3 different Reynolds Number and 5 angles of attach for each Reynold Number determine the lift and drag coefficients of the airfoil.
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mjilani_ug21sm created this project