Optimization of a generic fighter wing incorporating active aeroelastic wing technology

6th Symposium on Multidisciplinary Analysis and Optimization

Volumn , Issue , 1996, Pages 247-257

  Forster, E ^a   Kolonay, R ^a   Venkayya, V ^a   Eastep, F ^b  

^a WRIGHT PATTERSON AIR FORCE BASE   (United States)

^b UNIVERSITY OF DAYTON   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROELASTICITY; AIRCRAFT CONTROL; FINITE ELEMENT METHOD; FLEXIBLE WINGS; FLIGHT CONTROL SYSTEMS; NEWTON-RAPHSON METHOD; SUPERSONIC AIRCRAFT;

ACTIVE AEROELASTIC WINGS; AEROELASTIC CONSTRAINTS; DYNAMIC PRESSURES; MULTIPLE CONTROL SURFACES; OPTIMIZATION STUDIES; PRELIMINARY DESIGN; ROLL PERFORMANCE; STRUCTURAL WEIGHT;

CONTROL SURFACES;

EID: 84983127079     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1996-4010     Document Type: Conference Paper

References (11)

1. Pendleton, E., Griffin, K., Kehoe, M., and Perry, B., “A Flight Research Program for Active Aeroelastic Wing Technology,” AIAA Paper No. 96- 1574-CP, 37th AIAA Structures, Structural Dynamics and Materials Conference, Salt Lake City, UT, April 1996.
2. Miller, G. D., “Active Flexible Wing (AFW) Technology," Air Force Wright Aeronautical Laboratories TR-87-3096, February 1988.
3. Miller, G. D., “An Active Wing MultiDisciplinary Design Optimization Method,” AIAA Paper No. 94-4412-CP, 35th AIAA Structures, Structural Dynamics and Materials Conference, Hilton Head, SC, April 1994.
4. Pendleton, E., Lee, M., and Wasserman, L., “Application of AFW Technology to the Agile Falcon,” Journal of Aircraft Vol. 29, No. 3, May-June 1992.
5. Yurkovich, R., “Optimum Wing Shape for an AFW,” AIAA Paper No. 95-1220-CP, 36th AIAA Structures, Structural Dynamics and Materials Conference, New Orleans, LA, April 1995.
6. Andersen, G., Forster, E., Kolonay, R., and Eastep, F., “A Study of Control Surface Blending for Active Aeroelastic Wing Technology,” AIAA Paper No. 96-1443-CP, 37th AIAA Structures, Structural Dynamics and Materials Conference, Salt Lake City, UT, April 1996.
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8. Ausman, J. D., “Adaptive Multi-Dimensional Integrated Control (AMICS) ASTROS Add-On Documentation,” Interim Report for Wright Laboratories Contract F33615-93-C3615, November 1995.
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10. Johnson, E. H., and Venkayya, V. B., “Automated Structural Optimization System (ASTROS),” Vol. I, Theoretical Manual, Air Force Wright Aeronautical Laboratories TR-88-3028, December 1988.
11. Johnson, E. H., and Neill, D. J., “Automated Structural Optimization System (ASTROS),” Vol. Ill, Applications Manual, Air Force Wright Aeronautical Laboratories TR-88-3028, December 1988.