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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 | |