

MCQOPTIONS
Saved Bookmarks
1. |
A NACA 0012 airfoil has a trailing edge flap. The airfoil is operating at an angle of attack of 5 degrees with un-deflected flap. If the flap is now deflected by 5 degrees downwards, the CL versus α curve |
A. | shifts right and slope increases. |
B. | shifts left and slope increases. |
C. | shifts left and slope stays the same. |
D. | shifts left and slope stays the same. |
Answer» D. shifts left and slope stays the same. | |