Nonlinear Panel Response by a Monte Carlo Approach
Author:
Affiliation:
1. Columbia University, New York, N.Y.
2. Princeton University, Princeton, N.J.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.49320
Reference15 articles.
1. Nonlinear oscillations of a fluttering plate.
2. Nonlinear oscillations of a fluttering plate. II.
3. Transmission of Noise from a Turbulent Boundary Layer through a Flexible Plate into a Closed Cavity
4. Panel flutter - A review of the aeroelastic stability of plates and shells
5. Nonlinear Panel Response from a Turbulent Boundary Layer
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