A perturbation method for treating nonlinear panel flutter problems.
Author:
Affiliation:
1. Massachusetts Institute of Technology, Cambridge, Mass.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.5121
Reference8 articles.
1. Theoretical considerations of panel flutter at high supersonic Mach numbers.
2. Bolotin, V. V., Nonconservative Problems of the Theory of Elastic Stability, Macmillan, New York, 1963, pp.274-312.
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