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1. |
A wing alone aircraft has aerodynamic centre pitching moment coefficient of -0.126. If lift coefficient at zero AOA is 0.38 then, find Cm0. Consider Xcg=0.3. |
A. | -0.107 |
B. | -7.89 |
C. | 1.457 |
D. | 0.9845 |
Answer» B. -7.89 | |