Optimization of flexible wing without ailerons for rolling maneuver

Journal of Aircraft

Volumn 37, Issue 5, 2000, Pages 892-897

  Khot, N S ^a   Appa, K ^b   Eastep, F E ^c  

^a AIR FORCE RESEARCH LABORATORY   (United States)

^b NORTHROP GRUMMAN CORPORATION   (United States)

^c UNIVERSITY OF DAYTON   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; AERODYNAMIC LOADS; DEFORMATION; MANEUVERABILITY; MATHEMATICAL MODELS; MODAL ANALYSIS; OPTIMAL CONTROL SYSTEMS; STRAIN MEASUREMENT; WEIGHT CONTROL;

AILERONS; ANTISYMMETRIC TWIST; CAMBER DEFORMATION; FLEXIBLE ROLL RATE; FLEXIBLE WING; ROLLING MANEUVER;

WINGS;

EID: 0034275307     PISSN: 00218669     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.2687     Document Type: Article

References (13)

1. Khot, N. S., Eastep, F. E., and Kolonay, R. M., "Method for Enhancement of the Rolling Maneuver of a Flexible Wing," AIAA Paper 96-1391, April 1996.
2. Khot, N.S., Eastep, F. E., and Kolonay, R. M., "Wing Twist and Camber for the Rolling Maneuver of a Flexible Wing Without Ailerons," AIAA Paper 97-1268, April 1997.
3. Hall, J. W., "Executive Summary AFTI/F-111 Mission Adaptive Wing," WRDC-TR-89-3083, Sept. 1989.
4. Austin, F., Knowles, G. J., Jung, W. G., Tung, E. C., and Sheedy, E. M., "Adaptive/Conformed Wing Design for Future Aircraft," 1st European Conf. on Smart Structures and Materials, Glasgow, Scotland, U.K., May 1992.
5. Miller, G. D., "Active Flexible Wing (AFW) Technology," Air Force Wright Aeronautical Labs., AFWAL-TR-87-3036, Wright-Patterson AFB, OH, Feb. 1988.
6. Miller, G. D., "Active Flexible Wing Multidisciplinary Design Optimization Method," AIAA Paper 94-4412-CP, Sept. 1994.
7. Lazarus, K. B., Crawley, E. F., and Bohlmann, J. D., "Static Aeroelastic Control Using Strain Actuated Adaptive Structures," 1st Joint U.S./Japan Conf. on Adaptive Structures, Maui, HI, Nov. 1990.
8. Beauchamp, C. H., Nadolink, R. H., Dickinson, S. C., and Dean, L. M., "Shape Memory Alloy Adjustable Camber (SMAAC) Control Surfaces," 1st European Conf. on Smart Structures and Materials, Glasgow, Scotland, U.K., May 1992.
9. Kudva, J., Appa, K., Martin, C., Sendeekyj, G., and Harris, T., "Design, Fabrication, and Testing of the DARPA/WL Smart Wing Wind-Tunnel Model," AIAA Paper, 97-1198, April 1997.
10. Appa, K., Ausman, J., and Khot, N. S., "Feasibility Assessment and Optimization Study of Smart Actuation Systems for Enhanced Aircraft Maneuver Performance," WL-TR-97-3083, Wright-Patterson AFB, OH, July 1997.
11. Woodward, F. A., "An Improved Method for the Aerodynamic Analysis of Wing-Body-Tail Configurations in Subsonic and Supersonic Flow, Part I - Theory and Application," NASA CR-2228, Vol. 1, May 1973.
12. Neill, D. J., and Herendeen, D. L., "Automated Structural Optimization System (ASTROS)" Vol. I Users Manual, Air Force Wright Aeronautical Labs., AFWAL-TR-93-3025, Wright-Patterson AFB, OH, March 1993.
13. ASTROS User's Reference Manual for Version 20, Universal Analytics Inc., Torrance, CA, 1997.