Bending boundary layers in laminated-composite circular cylindrical shells
Author:
Affiliation:
1. NASA, Langley Research Center, Hampton, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2000-1660
Reference32 articles.
1. 1Kraus, H., Thin Elastic Shells - An Introduction to the Theoretical Foundations and the Analysis of Their Static and Dynamic Behavior, John Wiley and Sons, Inc., 1967, pp.131-142.
2. Geometric Design of Composite Cylindrical Characterization Specimens
3. On the Theory of Laminated Anisotropic Shells and Plates
4. Analysis of Shells Under Internal Pressure
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