MCQOPTIONS
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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. | |