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タイトルCompression Testing of Textile Composite Materials
本文(外部サイト)http://hdl.handle.net/2060/19960015568
著者(英)Masters, John E.
著者所属(英)Lockheed Martin Engineering and Sciences Co.
発行日1996-02-01
言語eng
内容記述The 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.
NASA分類Composite Materials
レポートNO96N21459
NASA-CR-198285
NAS 1.26:198285
権利No Copyright


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