Energy approach to flutter suppression and aeroelastic control

Journal of Guidance, Control, and Dynamics

Volumn 24, Issue 1, 2001, Pages 176-184

  Bendiksen, Oddvar O ^a  

^a UNIVERSITY OF CALIFORNIA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY CONDITIONS; MATHEMATICAL MODELS; SYSTEM STABILITY;

AEROELASTIC CONTROL; AEROELASTIC ENERGY PRINCIPLES; FLUTTER CONTROL; FLUTTER SUPPRESSIONS;

FLUTTER (AERODYNAMICS);

EID: 0034825444     PISSN: 07315090     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.4699     Document Type: Article

References (16)

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3. Frazer, R. A., and Duncan, W. J., "The Flutter of Aeroplane Wings," British Aeronautical Research Council R&M 1155, 1928.
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11. Bendiksen, O. O., "Nonunique Solutions in Transonic Aeroelasticity," Proceedings of the International Forum on Aeroelasticity and Structural Dynamics, Vol. 3, 1997, Confederation of European Aerospace Societies, Rome, pp. 425-435.
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13. Bendiksen, O. O., "Nonlinear Flutter Calculations for Transonic Wings," Proceedings of the International Forum on Aeroelasticity and Structural Dynamics, Vol. 2, 1997, Confederation of European Aerospace Societies, Rome, pp. 105-114.
14. Dowell, E. H., et al., A Modern Course in Aeroelasticity, Kluwer Academic, Dordrecht, The Netherlands, 1995, p. 88.
15. Lin, Y. C., Crawley, E. F., and Heeg, J., "Open- and Closed-Loop Results of a Strain-Actuated Active Aeroelastic Wing," Journal of Aircraft, Vol. 33, No. 5, 1996, pp. 987-994.
16. Bendiksen, O. O., and Hwang, G., "A Flutter Control Concept for Highly Flexible Transonic Wings," AIAA Paper 97-1269, April 1997.