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1. |
The NACA LS (1) 04XX airfoils when compared to NACA airfoils with same thickness had higher L/D ratios. For a lift coefficient of 1.0, what was this increase approximately in percentage? |
A. | 80% |
B. | 20% |
C. | 50% |
D. | Less than 10% |
Answer» D. Less than 10% | |