1.

Identify the missing angle given by the question mark for the following camber distribution of a thin airfoil.

A. tan-1⁡α
B. tan-1⁡-\(\frac {dz}{dx}\)
C. tan-1\(\frac {dz}{dx}\)
D. tan-1–\(\frac {dz}{dx}\)+α
Answer» C. tan-1\(\frac {dz}{dx}\)


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