Transverse shear stresses and their sensitivity coefficients in multilayered composite panels
Author:
Affiliation:
1. University of Virginia, NASA Langley Research Center, Hampton, Virginia 23681
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.12128
Reference21 articles.
1. Finite Element Solutions for Laminated Thick Plates
2. Alternate Hybrid-Stress Elements for Analysis of Multilayer Composite Plates
3. Hybrid-stress eight-node elements for thin and thick multilayer laminated plates
4. A refined analysis of laminated plates by finite element displacement methods—I. Fundamentals and static analysis
5. Modelling of thick composites using a layerwise laminate theory
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