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Effects of preform architecture on modulus and strength of 2-D triaxially braided textile compositesLaminates formed using braided fibrous preforms have been extensively investigated during the course of the past few years as alternatives to unidirectional prepreg tape systems. This paper focused on one aspect of that work. It defined the role of the fibrous preform architecture in controlling a laminate's mechanical properties. The presentation was divided into four sections as the outline listed above illustrates. The presentation began with a brief introduction which defined the objectives of the study and detailed the materials studied. This was followed by a review of empirical test results. The materials' moduli and strengths were measured in both tension and compression. Their shear moduli were also experimentally determined. The review of the empirical data comprised the bulk of the presentation. A comparison of the experimental data to results predicted analytically was then presented. The presentation concluded with a few summary remarks. The specimens studied in this investigation featured 2-D triaxially braided AS4 graphite fiber preforms impregnated with Shell 1895 epoxy resin.
Document ID
19960010542
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Masters, John E.
(Lockheed Engineering and Sciences Co. Hampton, VA, United States)
Naik, Rajiv
(Analytical Services and Materials, Inc. Hampton, VA., United States)
Minguet, Pierre J.
(Boeing Defense and Space Group Philadelphia, PA., United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1995
Publication Information
Publication: NASA, Langley Research Center Mechanics of Textile Composites Conference
Subject Category
Composite Materials
Accession Number
96N17708
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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