ANSYS FLUENT - Tutorial Perfil NACA 2412 - NSIV.IO
ANSYS FLUENT - Tutorial Perfil NACA 2412 - NSIV.IO
Feb 20, 2022
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Consider an NACA 2412 airfoil with a 2-m chord in an airstream with a velocity of 50  m / s at standard sea level conditions. If the lift per unit span is 1353  N / m, what is the angle of attack? | Numerade
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