

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 | |