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1. |
Identify the missing angle given by the question mark for the following camber distribution of a thin airfoil. |
A. | tan-1α |
B. | tan-1-\(\frac {dz}{dx}\) |
C. | tan-1\(\frac {dz}{dx}\) |
D. | tan-1–\(\frac {dz}{dx}\)+α |
Answer» C. tan-1\(\frac {dz}{dx}\) | |