A deployable system is introduced for assisting flight control under certain flight conditions, such as at high angles of attack, whereby two inflatable membranes are located on the forebody portion of an aircraft on opposite sides thereof. The members form control surfaces for effecting lateral control forces if one is inflated and longitudinal control forces if both are inflated.
Aerodynamic surface distension system for high angle of attack forebody vortex control
1994-07-05
Sonstige
Keine Angabe
Englisch
Forebody Vortex Manipulation for Aerodynamic Control of Aircraft at High Angles of Attack
SAE Technical Papers | 1989
|The Impact of Forebody Geometries at High-Angle-of-Attack with Forebody Tangential Blowing
British Library Conference Proceedings | 1998
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