MCQOPTIONS
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| 1. |
Cambered wing has minimum drag coefficient of 0.05 and constant K of 0.023. If CL is 0.8 then find the value of CD. Given minimum drag occurs at CL of 0.1. |
| A. | 0.06127 |
| B. | 6.1 |
| C. | 61.2 |
| D. | 0.6721 |
| Answer» B. 6.1 | |