Compression Behavior of A= 45 -Dominated Laminates with a Circular Hole or Impact Damage
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.48652
Reference13 articles.
1. 2Rhodes, M. D and Williams, J. G. "Concepts for Improving the Damage Tolerance of Composite Compression Panels," NASA TM-85748, Jan.1984.
2. Strength Predictions of Composite Laminates with Unloaded Fastener Holes
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