Method for calculating the interlaminar stresses in symmetric laminates containing a circular hole
Author:
Affiliation:
1. National Chung-Hsing University, Taichung, Taiwan 40227, Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.10900
Reference20 articles.
1. Interlaminar Stresses in Composite Laminates Under Uniform Axial Extension
2. Some New Results on Edge Effect in Symmetric Composite Laminates
3. Boundary-Layer Effects in Composite Laminates: Part 1—Free-Edge Stress Singularities
4. Boundary-Layer Effects in Composite Laminates: Part 2—Free-Edge Stress Solutions and Basic Characteristics
5. An Efficient Method for the Calculation of Interlaminar Stresses in Composite Materials
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