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The interlaminar fracture toughness of woven graphite/epoxy compositesThe interlaminar fracture toughness of 2-D graphite/epoxy woven composites was determined as a function of stacking sequence, thickness, and weave pattern. Plain, oxford, 5-harness satin, and 8-harness satin weaves of T300/934 material were evaluated by the double cantilever beam test. The fabric material had a G (sub Ic) ranging from 2 to 8 times greater than 0 degrees unidirectional T300/934 tape material. The interlaminar fracture toughness of a particular weave style was dependent on whether the stacking sequence was symmetric or asymmetric and, in some cases, on the fabric orientation.
Document ID
19900000863
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Funk, Joan G.
(NASA Langley Research Center Hampton, VA, United States)
Deaton, Jerry W.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
November 1, 1989
Subject Category
Composite Materials
Report/Patent Number
NAS 1.60:2950
NASA-TP-2950
L-16629
Report Number: NAS 1.60:2950
Report Number: NASA-TP-2950
Report Number: L-16629
Accession Number
90N10179
Funding Number(s)
PROJECT: RTOP 505-63-01-06
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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