The influence of lay-up and thickness on composite impact damage andcompression strength-Reference-Cited by-同舟云学术

The influence of lay-up and thickness on composite impact damage andcompression strength

Published:1985-04-15 Issue: Volume: Page:
ISSN:
Container-title:26th Structures, Structural Dynamics, and Materials Conference
language:
Short-container-title:

Author:

GUYNN E.¹,OBRIEN T.²

Affiliation:

1. NASA, Langley Research Center; Kentron International, Inc., Aerospace Technologies Div., Hampton, VA

2. NASA, Langley Research Center; U.S. Army, Research and Technology Laboratories, Hampton, VA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1985-646

Reference10 articles.

1. failure strains than thin laminates impacted at the same energy per unit thickness, which may result from larger delaminations forming i n the interface near the back ply i n thin laminates compared to thick laminates. Epoxy Structural Components Loaded i n Compression. Mechanics of Composite Materials, Z. Hashin and C. T. Herakovich, eds., Pergamon Press, 1982, pp. 283-306. L . Byers, R. A.: Behavior of Damaged

2. 0-00440

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