Response and failure analysis of a graphite-epoxy laminate containing terminating internal plies
Author:
Affiliation:
1. Johns Hopkins University, Laurel, MD
2. Virginia Polytechnic Institute and State University, Blacksburg, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1985-608
Reference7 articles.
1. Adams, D.F., Ramkumar, R.L., and Walrath, D.Z. "Analysis of Porous Laminates in the Presence of Ply Drop-offs and Fastener Holes," Northrop Technical Report NOR 84-113, Northrop Corporation,Hawthorne, CA90250, an 3 theUniversity of Wyoming, Laramie, Wyoming 82071. May 1984.
2. Knight. M. "Three Dimensional Elastic Moduli of Gra.phite/poxyCompositesrVJournal of Composite Materials, Vol.16, 1982, pp.153-153.
3. Jones, Robert M., Mechanics of Composite Materials, Scripta Book Company, Washington, D.C., 1975, pp.40-41and p. 51. C. Case 2 Lay-Up with Nonsymmetrlc Condltions
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