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				| 1. | If an airfoil is designed to provide lift curve slope as 7.8, then find airfoil efficiency. The actual lift curve slope of the airfoil is 7.4. | 
| A. | 94.87% | 
| B. | 45% | 
| C. | 15.6% | 
| D. | 98.7% | 
| Answer» B. 45% | |