Postbuckling compressive strength of graphite/epoxy laminated cylindrical panels loaded in compression
Author:
Affiliation:
1. Korea Advanced Institute of Science and Technology, Taejon 305-701, Republic of Korea
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.12428
Reference18 articles.
1. Imperfection sensitivity of axially compressed stringer reinforced cylindrical panels under internal pressure
2. Buckling behavior of laminated composite cylindrical panels under axial compression
3. Nonlinear analysis of axially-loaded laminated cylindrical shells
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