Discrete analysis of stiffened composite cylindrical shells
Author:
Affiliation:
1. Georgia Institute of Technology, Atlanta, Georgia
2. Chevron Oil Field Research Company, La Habra, California
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.9162
Reference7 articles.
1. Orthogonally stiffened cylindrical shells subjected to internal pressure
2. Imperfection sensitivity of axially compressed stringer reinforced cylindrical panels under internal pressure
3. Buckling of elastic-plastic cylindrical panel under axial compression
4. Vibration of simply supported cylindrical shells with longitudinal stiffeners
5. Stability of discretely stringer-stiffened cylindrical shells.
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