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1. |
The fundamental equation for the thin airfoil theory does not encompass which of the following approximations? |
A. | The angle of attack and slope of the camber line is small |
B. | Camber line induced velocity distribution is the same for chord line |
C. | Vortex sheet is placed at the chord line |
D. | Kutta condition is satisfied at the trailing edge |
Answer» E. | |