 
			 
			MCQOPTIONS
 Saved Bookmarks
				| 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 | |