Stability of Flat, Simply Supported Corrugated-Core Sandwich Plates Under Combined Loads
Author:
Affiliation:
1. North American Aviation, Inc.,
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
http://arc.aiaa.org/doi/pdf/10.2514/8.8622
Reference6 articles.
1. The Buckling and Bending of Orthotopic Sandwich Panels With All Edges Simply-Supported
2. Analysis of the Elastic and Plastic Stability of Sandwich Plates by the Method of Split Rigidities-I
Cited by 5 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Buckling of Long Orthotropic Plates Including Higher-Order Transverse Shear;Journal of Engineering Mechanics;2000-12
2. Buckling coefficients for fiber-reinforced plastic-faced sandwich plates under combined loading;AIAA Journal;1987-05
3. REFERENCES;Analysis and Design of Structural Sandwich Panels;1969
4. Stability of circumferentially corrugated sandwich cylinders under combined loads;AIAA Journal;1964-12
5. Comments on "Stability of Flat, Simply Supported Corrugated-Core Sandwich Plates Under Combined Loads";Journal of the Aerospace Sciences;1961-03
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