MCQOPTIONS
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| 1. |
What is the Kutta Condition in terms of strength (γ) of the thin airfoil? |
| A. | γ = 0 |
| B. | γ(LE) = 0 |
| C. | \(\frac {D\gamma }{Dt}\)=0 |
| D. | γ(TE) = 0 |
| Answer» E. | |