Nonlinear stress-strain and strength response of axisymmetric bimodulus composite material shells
Author:
Affiliation:
1. General Motors Research Laboratories, Warren, Michigan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.8318
Reference15 articles.
1. Models for Fibrous Composites With Different Properties in Tension and Compression
2. Bending and extension of cross-ply laminates with different moduli in tension and compression
3. Cross-Ply Elliptic Plates of Bimodulus Material
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