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Delamination behavior of quasi-isotropic graphite epoxy laminates subjected to tension and torsion loads / J.A. Hinkley and T. K. O'Brien.

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Format:
Book
Government document
Author/Creator:
Hinkley, Jeffrey A., author.
O'Brien, T. Kevin, author.
Contributor:
American Helicopter Society
Langley Research Center, issuing body.
Series:
NASA technical memorandum ; 104181.
NASA/TM ; 104181
Language:
English
Subjects (All):
Composite materials--Delamination.
Composite materials.
Physical Description:
1 online resource (approximately 18 pages) : illustrations.
Place of Publication:
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, January 1992.
Notes:
"AVSCOM-TR-91-B-018."
"January 1992."
"Paper presented at the American Helicopter Society Specialists' Meeting Williamsburg, Virginia, October 29, 1991."
Includes bibliographical references (page 8).
Description based on online resource, PDF version; title from title page (NASA, viewed on Jan. 6, 2022).
Other Format:
Microfiche version: Hinkley, Jeffrey A. Delamination behavior of quasi-isotropic graphite epoxy laminates subjected to tension and torsion loads.
OCLC:
1291211331

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