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1. |
The skin-friction drag coefficient for turbulent flow on the bottom surface of an airfoil, with chord length being 1m is _____ (Reynolds number at the trailing edge Rec=32×105) |
A. | 0.074 |
B. | 0.0037 |
C. | 0.027 |
D. | 0.0074 |
Answer» C. 0.027 | |