Combined effect of matrix cracking and stress-free edge on delamination /

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Bibliographic Details
Author / Creator:	Salpekar, Satish A. (Satish Annaji), 1954-
Imprint:	Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [ St. Louis, MO] : US Army Aviation Systems Command, [1990]
Description:	64 pages : illustrations.
Language:	English
Series:	NASA technical memorandum ; 102591 AVSCOM technical memorandum ; 90-B-002 NASA technical memorandum ; 102591. AVSCOM technical memorandum ; 90-B-002.
Subject:	Composite materials -- Delamination. Crack initiation. Delaminating. Edge loading. Finite element method. Laminates. Strain energy release rate.
Format:	E-Resource Microform U.S. Federal Government Document Book
URL for this record:	http://pi.lib.uchicago.edu/1001/cat/bib/6504497

Hidden Bibliographic Details
Other authors / contributors:	O'Brien, T. Kevin. Langley Research Center. United States. Army Aviation Systems Command.
Notes:	Cover title. "March 1990." Includes bibliographical references (pages 30-32). Available via Internet from the NASA Technical Report Server web site. Address as of 3/1/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900011810%5F1990011810.pdf; current access available via PURL.
GPO item no.:	0830-D (MF) 0830-D (online)
Govt.docs classification:	NAS 1.15:102591

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