MCQOPTIONS
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| 1. |
Define Kutta-Joukowski theorem. |
| A. | Lift per unit span on the airfoil |
| B. | Drag per unit span on the airfoil |
| C. | Moment per unit span on the airfoil |
| D. | Thrust per unit span on the airfoil |
| Answer» B. Drag per unit span on the airfoil | |