

MCQOPTIONS
Saved Bookmarks
1. |
If moment coefficient about aerodynamic centre of wing is -0.216 and lift coefficient of wing is 1.2. Find moment coefficient about cg. Given cg location as Xcg = 0.3. |
A. | -0.156 |
B. | 0.123 |
C. | 0.56 |
D. | -1.56 |
Answer» B. 0.123 | |