Time-Delayed Feedback Control for Flutter of Supersonic Aircraft Wing
Author:
Publisher
Springer Netherlands
Link
http://link.springer.com/content/pdf/10.1007/978-94-007-2069-5_100.pdf
Reference13 articles.
1. Fung, Y.C.: An Introduction to the Theory of Aeroelasticity. Dover Publications, New York (1993)
2. Woolston, D.S., Runyan, H.L., Andrew, R.E.Y.: An investigation of effects of certain types of structural nonlinearities on wing and control surface flutter. J. Aeronaut. Sci. 24, 57–63 (1957)
3. Shen, S.F.: An approximate analysis of non-linear flutter problems. J. Aerosp. Sci. 26, 25–32 (1959)
4. Jr McIntosh, S.C., Jr Reed, R.E., Rodden, W.P.: Experimental and theoretical study of nonlinear flutter. J. Aircr. 18, 1057–1063 (1981)
5. Yang, Z.C., Zhao, L.C.: Analysis of limit cycle flutter of an wing section in incompressible flow. J. Sound Vib. 123, 1–13 (1998)
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