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

Description
Item Description:	"March 1990." Cover title. Shipping list number: 90-0860-M. Microform.
Physical Description:	64 pages : illustrations Also 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.
Bibliography:	Includes bibliographical references (pages 30-32).