The induced angle of attack in terms of flow parameters for a wing is – McqOptions

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1.	The induced angle of attack in terms of flow parameters for a wing is_____
A.	αi=\(\frac {w}{V_∞}\)
B.	αi=\(\frac {2w}{V_∞}\)
C.	αi=\(\frac {V_∞}{w}\)
D.	αi=\(\frac {w}{V_∞}\)
Answer» B. αi=\(\frac {2w}{V_∞}\)

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