Post-stall roll control utilizing tangential leading edge blowing is demonstrated in a wind tunnel on a delta wing model that exhibited wing rock. The dampening effect of symmetric blowing alone on wing rock is found to be effective up to a certain maximum amount of blowing. A moderate amount of symmetric blowing was shown to be effective in linearizing the asymmetric blowing static rolling moment responses.
Active control of wing rock of a delta wing at post-stall using tangential leading edge blowing
AIAA, Aerospace Sciences Meeting and Exhibit ; 1993 ; Reno, NV, United States
1993-01-01
Conference paper
No indication
English
Active Control of Wing Rock Using Tangential Leading-Edge Blowing
Online Contents | 1994
|Roll Moment Characteristics of Asymmetric Tangential Leading-Edge Blowing on a Delta Wing
Online Contents | 1994
|