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Consider a NACA 2412 airfoil with a 64 cm chord in an airstream with a velocity...

Consider a NACA 2412 airfoil with a 64 cm chord in an airstream with a velocity of 70m/s at standard sea level conditions. If the lift per unit span is 1254 N/m, obtain the following quantities:

b) Lift coefficient

c) Angle of Attack

d) Drag per unit span

e) moment per unit span about the aerodynamic center

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Expert Solution

genius_generous answered 2 years ago
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