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				| 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 | |