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Compression Testing of Textile Composite MaterialsThe applicability of existing test methods, which were developed primarily for laminates made of unidirectional prepreg tape, to textile composites is an area of concern. The issue is whether the values measured for the 2-D and 3-D braided, woven, stitched, and knit materials are accurate representations of the true material response. This report provides a review of efforts to establish a compression test method for textile reinforced composite materials. Experimental data have been gathered from several sources and evaluated to assess the effectiveness of a variety of test methods. The effectiveness of the individual test methods to measure the material's modulus and strength is determined. Data are presented for 2-D triaxial braided, 3-D woven, and stitched graphite/epoxy material. However, the determination of a recommended test method and specimen dimensions is based, primarily, on experimental results obtained by the Boeing Defense and Space Group for 2-D triaxially braided materials. They evaluated seven test methods: NASA Short Block, Modified IITRI, Boeing Open Hole Compression, Zabora Compression, Boeing Compression after Impact, NASA ST-4, and a Sandwich Column Test.
Document ID
19960015568
Acquisition Source
Langley Research Center
Document Type
Contractor Report (CR)
Authors
Masters, John E.
(Lockheed Martin Engineering and Sciences Co. Hampton, VA United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1996
Subject Category
Composite Materials
Report/Patent Number
NASA-CR-198285
NAS 1.26:198285
Accession Number
96N21459
Funding Number(s)
CONTRACT_GRANT: NAS1-19000
PROJECT: RTOP 505-63-50-04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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