Actuating system for enhancement of rolling maneuver of a wing with 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/10.2514/6.1999-1397
Reference17 articles.
1. Khof N. S.,Eastep, F. E. and Kolonay, R. M."A Method for Enhancement of the Rolling Maneuver of a Flexible Wing0022, AlAA-96-1391 Presented at 37'h,AI&4/ASMEfASCE/AHS/ASClAdaptive Structures, Structural Dynamics, and Materials Conference, Salt Lake City,Ut, April 1996.
2. Hall,J.W."Executive Summary AFTI.@-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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