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

Saved in:
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.
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.
Edge loading.
Finite element method.
Strain energy release rate.
Format: E-Resource Microform U.S. Federal Government Document Book
URL for this record:
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:; current access available via PURL.
GPO item no.:0830-D (MF)
0830-D (online) classification:NAS 1.15:102591