Flutter, Postflutter, and Control of a Supersonic Wing Section
Author:
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
Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.4970
Reference26 articles.
1. 1Bolotin, V. V., Nonconservative Problems of the Theory of Elastic Stability, Macmillan, New York, 1963, pp.274-312.
2. 5Dowell, E. H., Aeroelasticity of Plates and Shells, Kluwer Academic, Dordrecht, TheNetherlands,1974, pp.35-49.
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