1.

The induced angle of attack in terms of flow parameters for a wing is_____

A. <sub>i</sub>= ( frac {w}{V_ } )
B. <sub>i</sub>= ( frac {2w}{V_ } )
C. <sub>i</sub>= ( frac {V_ }{w} )
D. <sub>i</sub>= ( frac {w}{V_ } )
Answer» B. <sub>i</sub>= ( frac {2w}{V_ } )


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