MCQOPTIONS
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MCQOPTIONS
| 1. |
What is the total circulation around the symmetric airfoil according to the thin airfoil theory? |
| A. | = <sup>2</sup>cV<sub> </sub> |
| B. | = <sup>2</sup> cV<sub> </sub> |
| C. | =2 cV<sub> </sub> |
| D. | = cV<sub> </sub> |
| Answer» E. | |