MCQOPTIONS
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MCQOPTIONS
| 1. |
The lift coefficient for a thin symmetrical airfoil is given by______ |
| A. | c<sub>l</sub> = |
| B. | c<sub>l</sub> = <sup>2</sup> |
| C. | c<sub>l</sub> = 2 |
| D. | c<sub>l</sub> = <sup>2</sup> |
| Answer» D. c<sub>l</sub> = <sup>2</sup> | |