Plate Buckling Due to Follower Edge Forces
Author:
Affiliation:
1. Reimann and Georger, Inc., Buffalo, N. Y.
2. State University of New York, Buffalo, N. Y.
Publisher
ASME International
Subject
Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics
Link
http://asmedigitalcollection.asme.org/appliedmechanics/article-pdf/44/4/768/5876550/768_1.pdf
Cited by 21 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. Dynamic Stability Analysis of Square Isotropic/Laminated Composite Plates With Circular Cutout Subjected to Non-Uniform Follower Edge Load With Damping;Journal of Aerospace Sciences and Technologies;2023-08-14
2. Stability of variable stiffness composite laminates under compressive and shearing follower forces;Composite Structures;2019-10
3. Nonconservative stability of viscoelastic plates subject to triangularly distributed follower loads;Journal of Theoretical and Applied Mechanics;2017-07-15
4. Dynamic Instability Characteristics of Thin Plate Like Beam with Internal Damage Subjected to Follower Load;International Journal of Structural Stability and Dynamics;2015-03-08
5. Buckling, Vibration, and Flutter Behavior of Laminated Composite Panels with Flaws Subjected to Nonuniform Follower Forces;Journal of Engineering Mechanics;2012-04
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