On Panel Flutter in the Presence of a Boundary Layer
Author:
Affiliation:
1. University of California, Los Angeles
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
http://arc.aiaa.org/doi/pdf/10.2514/8.7949
Reference14 articles.
1. On the Aerodynamic Instability of Thin Panels
2. Supersonic Flutter of a Cylindrical Shell
3. Ward, G. N., Linearized Theory of Steady High Speed Flow, Cambridge University Press, pp.224-227, 1955.
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