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A comparison of graphite/epoxy tape laminates and 2-D braided composites mechanical propertiesA comparison of the mechanical properties of unidirectional composite tape laminates and of two-dimensional triaxially braided composite was conducted. The tape laminate layups were designed to match the percentage of axial fibers and the angle of the bias tows in the braided composite. The materials system used for the laminates is AS4/3501-6 which was chosen as the closest available match to As4/1895 used for the braids. The strength and stiffness properties measured here include tension, open-hole tension, filled-hole tension, compression and open-hole compression, all of these in both the longitudinal and transverse direction. Results show that the longitudinal modulus of both material forms is quite similar, but that the transverse modulus of the braids is lower. In terms of strength, the longitudinal unnotched strength of the braids is lower than that of the laminates, while the transverse strength is significantly lower. For both strength and stiffness, the crimp in the bias tows of the braid is probably the main cause for reduced properties. On the other hand, a very significant increase in open-hole and filled-hole tension strength was observed for the braids compared to the tape laminates. However, this was not observed in compression where all the braid properties are lower than for the laminates.
Document ID
19960010543
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
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
96N17709
Funding Number(s)
CONTRACT_GRANT: NAS1-19247
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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