Fatigue debonding characterization in composite skin/stringer configurations /

Bibliographic Details
Main Authors:	Cvitkovich, Michael (Author), O'Brien, T. Kevin (Author), Minguet, Pierre Jacques (Author)
Corporate Author:	United States. Army Materiel Command
Format:	Government Document eBook
Language:	English
Published:	Hampton, Virginia : Alexandria, Virginia : National Aeronautics and Space Administration, Langley Research Center ; U.S. Army Materiel Command, April 1997.
Series:	NASA technical memorandum ; 110331. ARL-TR (Aberdeen Proving Ground, Md.) ; 1342.
Subjects:	Fatigue tests. Debonding (materials) Composite structures. Flanges. Skin (structural member) Bonded joints. Crack initiation. Delaminating. Graphite-epoxy composites. Resin matrix composites.
Online Access:	https://purl.fdlp.gov/GPO/gpo65166

Description
Item Description:	"April 1997." Technical memo., Prepared in collaboration with the Boeing Defense and Space Group, Philadelphia, PA. Errata: Page 13, Table 2: Column 2 heading should read E sub 22 GPa. "Performing organization: NASA Langley Research Center"--Report documentation page.
Physical Description:	1 online resource (33 pages) : illustrations.
Bibliography:	Includes bibliographical references (page 12).