Deformation of a flexible wing using an actuating system for a rolling maneuver without ailerons
Author:
Affiliation:
1. USAF, Research Lab., Wright-Patterson AFB, OH
2. Northrop Grumman Corp., Military Aircraft Div., El Segundo, CA
3. Dayton, Univ., OH
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1998-1802
Reference16 articles.
1. Wing twist and camber for the rolling maneuver of a flexible wing without aileron
2. Hall,J.W."Executive Summary AFTI/F-111 Mission Adaptive Wing"WRDC-TR-89-3083, Sept.1989
3. Adaptive/conformal wing design for future aircraft
4. Miller, G. D. "Active Flexible Wing (AFW) Technology "AFWAL-TR-87-3036,Feb. 1988.
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