MCQOPTIONS
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| 1. |
Find location of aerodynamic centre from leading edge if, chord is 10m and airfoil has flow velocity of 0.2 M. |
| A. | 2.5 m |
| B. | 0.2 m |
| C. | 5 m |
| D. | 10 m |
| Answer» B. 0.2 m | |