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Evaluation of the impact response of textile compositesAn evaluation of the impact damage resistance and impact damage tolerance of stitched and unstitched uniweaves, 2-D braids, and 3-D weaves was conducted. Uniweave laminates were tested at four thicknesses to determine the sensitivity of the tests to this parameter. Several braid and weave parameters were also varied to establish their velocity (large mass) impacts and then loaded in tension or compression to measure residual strength. Experimental results indicate that stitching significantly improves the uniweaves' damage resistance. The 2-D braids and 3-D weaves offered less damage resistance than the stitched materials. Stitching also improved the compression after impact (CAI) and tension after impact (TAI) strengths of the uniweave materials.
Document ID
19960012496
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Portanova, M. A.
(Lockheed Martin Engineering and Sciences Co. Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
December 1, 1995
Subject Category
Composite Materials
Report/Patent Number
NASA-CR-198265
NIPS-96-08487
NAS 1.26:198265
Report Number: NASA-CR-198265
Report Number: NIPS-96-08487
Report Number: NAS 1.26:198265
Accession Number
96N18733
Funding Number(s)
PROJECT: RTOP 505-63-50-04
CONTRACT_GRANT: NAS1-19000
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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