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

Bibliographic Details
Main Author:	Salpekar, Satish A. (Satish Annaji), 1954-
Corporate Authors:	Langley Research Center, United States. Army Aviation Systems Command
Other Authors:	O'Brien, T. Kevin
Format:	Government Document Microform Book
Language:	English
Published:	Hampton, Va. : [St. Louis, Mo.] : National Aeronautics and Space Administration, Langley Research Center ; US Army Aviation Systems Command, [1990]
Series:	AVSCOM technical memorandum ; 90-B-002. NASA technical memorandum ; 102591.
Subjects:	Composite materials > Delamination. Crack initiation. Delaminating. Edge loading. Finite element method. Laminates. Strain energy release rate.
Online Access:	https://purl.fdlp.gov/GPO/LPS67326

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