Response of a Nonlinear Flat Panel to Periodic and Randomly-Varying Loadings
Author:
Affiliation:
1. The Boeing Company,
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
http://arc.aiaa.org/doi/pdf/10.2514/8.9688
Reference17 articles.
1. The Non-Linear Boundary Value Problem of the Buckled Plate
2. Non-linear bending of a circular plate under normal pressure
3. Timoshenko, S., Theory of Elastic Stability, pp.321-323; McGraw-Hill Book Co., Inc., New York, 1936.
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