Nonlinear Panel Response from a Turbulent Boundary Layer
Author:
Affiliation:
1. Columbia University, New York
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.50242
Reference12 articles.
1. Bolotin, V. V., Nonconservative Problems of the Theory of Elastic Stability, Pergamon Press, New York, 1963, pp.280-289.
2. Wall-pressure fluctuations associated with subsonic turbulent boundary layer flow
3. Breathing Vibrations of a Partially Filled Cylindrical Tank—Linear Theory
4. Generalized aerodynamic forces on a flexible plate undergoing transient motion
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