Buckling, Vibration, and Flutter Behavior of Laminated Composite Panels with Flaws Subjected to Nonuniform Follower Forces
Author:
Affiliation:
1. Dept. of Aerospace Engineering, IIT Kharagpur, 721302, India.
2. Dept. of Aerospace Engineering, IIT, Kharagpur (corresponding author).
3. Dept. of Aerospace Engineering, Chosun Univ., 375 Seosuk-dong, Dong-gu, Gwanju, Republic of Korea.
Publisher
American Society of Civil Engineers (ASCE)
Subject
Mechanical Engineering,Mechanics of Materials
Link
http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29EM.1943-7889.0000333
Reference27 articles.
1. Stability of a rectangular plate under nonconservative and conservative forces
2. Die Knicklast des einseitig eingespannten, tangential gedrückten Stabes
3. Plate Buckling Due to Follower Edge Forces
4. Dynamic Instability Characteristics of Plates Subjected to Partially Distributed Follower Edge Loading with Damping
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