MCQOPTIONS
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| 1. |
An aircraft is cruising with lift coefficient of 2.5 and thrust loading of 0.6. Find drag coefficient of the aircraft. |
| A. | 1.5 |
| B. | 2.5 |
| C. | 2.6 |
| D. | 2.59 |
| Answer» B. 2.5 | |