Aeroelastic Response of Nonlinear Wing Sections Using a Functional Series Technique-Reference-Cited by-同舟云学术

Aeroelastic Response of Nonlinear Wing Sections Using a Functional Series Technique

Published:2002-05 Issue:5 Volume:40 Page:813-824
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Marzocca Piergiovanni¹,Librescu Liviu¹,Silva Walter A.²

Affiliation:

1. Virginia Polytechnic Institute and State University, Blacksburg, Virginia 24061-0219

2. NASA Langley Research Center, Hampton, Virginia 23681-2199

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/2.1735

Reference41 articles.

1. 1Volterra, V., Theory of Functionals and of Integral and Integro-Differential Equations, Dover, New York, 1959, pp.1-39.

2. 2Wiener, N., Selected Papers of Norbert Wiener Including Generalized Harmonic Analysis and Tauberian Theorems, Society for Industrial and Applied Mathematics and MIT Press, Cambridge, MA, 1964, pp.17-33.

3. 4Schetzen, M., The Volterra and Wiener Theories of Nonlinear Systems, Wiley-Interscience, New York, 1980, pp.1-122, 145-198.

4. 5Boyd, S. P. “Volterra Series, Engineering Fundamentals,” Ph.D. Dissertation, Dept. of Electrical Engineering and Computer Sciences,Univ. of California, Berkeley, CA,1985.

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