

MCQOPTIONS
Saved Bookmarks
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. | |