Stress fields in general composite laminates
Author:
Affiliation:
1. University of Palermo, Palermo 90128, Italy
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.13445
Reference29 articles.
1. Interlaminar Stresses in Composite Laminates Under Uniform Axial Extension
2. Approximate Three-Dimensional Solutions for Symmetric Laminates Under Inplane Loading *
3. Interlaminar stress singularities at a straight free edge in composite laminates
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1. Boundary Element Method for Composite Laminates;Encyclopedia of Continuum Mechanics;2020
2. Boundary Element Method for Composite Laminates;Encyclopedia of Continuum Mechanics;2017-11-07
3. References;Handbook of Structural Life Assessment;2017-04-07
4. A variable kinematic doubly-curved MITC9 shell element for the analysis of laminated composites;Mechanics of Advanced Materials and Structures;2016-04-06
5. Deformation Characteristics of Composite Structures;J APPL COMPUT MECH;2016
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