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Fatigue damage development of various CFRP-laminatesThe chronic strength and fatigue behavior of a woven carbon-fiber reinforced laminate in a balanced eight-shaft satin weave style was compared to nonwoven laminates with an equivalent cross-ply layup. Half the fibers were arranged in the direction of the load and the other half perpendicular to it. Two types of nonwoven laminates consisting of continuous fibers and aligned discontinuous fibers, both produced from carbon fiber prepregs, were studied. The cross-ply laminate with continuous fiber showed the best characteristics with regard to both static strength and fatigue. The similarities and differences in damage mechanisms in the laminates are described.
Document ID
19880013561
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Schulte, K.
(NASA Headquarters Washington, DC United States)
Baron, CH.
(NASA Headquarters Washington, DC United States)
Date Acquired
September 5, 2013
Publication Date
May 1, 1988
Publication Information
ISSN: 0049-8688
Subject Category
Composite Materials
Report/Patent Number
NASA-TT-20247
NAS 1.77:20247
Accession Number
88N22945
Funding Number(s)
CONTRACT_GRANT: NASW-4307
Distribution Limits
Public
Copyright
Public Use Permitted.
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