Method for enhancement of the rolling maneuver of a flexible wing

Journal of Aircraft

Volumn 34, Issue 5, 1997, Pages 673-678

  Khot, N S ^a,c,d   Eastep, F E ^b,d,e   Kolonay, R M ^a,c,d  

^a AIR FORCE RESEARCH LABORATORY   (United States)

^b UNIVERSITY OF DAYTON   (United States)

^c Flight Dynamics Directorate   (United States)

^d AIAA   (United States)

^e Dept of Mech and Aerosp Eng ^*

Author keywords

[No Author keywords available]

Indexed keywords

FLEXIBLE STRUCTURES; FLIGHT DYNAMICS; STRAIN;

AILERON TWISTED WINGS; ANTISYMMETRIC CAMBER DISTRIBUTION; ANTISYMMETRIC TWIST DISTRIBUTION; FLEXIBLE WINGS;

WINGS;

EID: 0031224565     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/2.2228     Document Type: Article

References (11)

1. Hall, J. W., "Executive Summary AFTI/F-111 Mission Adaptive Wing," U.S. Air Force Wright Research and Development Center TR-89-3083, Sept. 1989.
2. 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 Sturctures and Materials, Glasgow Scotland, May 1992.
3. Miller, G. D., "Active Flexible Wing (AFW) Technology," Air Force Wright Aeronautical Labs., TR-87-3036, Feb. 1988.
4. Miller, G. D., "An Active Flexible Wing Multi-Disciplinary Design Optimization Method," AIAA 5th Symposium on Multidisciplinary Analysis and Optimization (Panama City, FL), AIAA, Washington, DC, 1994, pp. 1388-1394.
5. 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, Hawaii, Nov. 1990.
6. 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, May 1992.
7. Striz, A. G., Eastep, F. E., and Venkayya, V. B., "Influence of Static and Dynamic Aeroelasticity Constraints on the Optimal Structural Design of Flight Vehicle Structure," Proceedings of the AIAA 32nd Structures, Structural Dynamics, and Materials Conference (Baltimore, MD), AIAA, Washington, DC, 1991, pp. 470-476.
8. 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, May 1973.
9. Johnson, E. H., and Venkayya, V. B., "Automated Structural Optimization System (ASTROS)," Theoretical Manual, Vol. 1, Air Force Wright Aeronautical Labs., TR-88-3028, Dec 1988.
10. Neill, D. J., and Herendeen, D. L., "Automated Structural Optimization System (ASTROS)," Users Manual, Vol. 1, TR-93-3025, March 1993.
11. Harder, R. L., and Desmarais, R. N., "Interpolation Using Surface Splines," Journal of Aircraft, Vol. 9, No. 2, 1972.