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Compressive strength of fiber reinforced composite materialsResults of an experimental and analytical investigation of the compressive strength of unidirectional boron-epoxy composite material are presented. Observation of fiber coordinates in a boron-epoxy composite indicates that the fibers contain initial curvature. Combined axial compression and torsion tests were conducted on boron-epoxy tubes, and it was shown that the shear modulus is a function of axial compressive stress. An analytical model which includes initial curvature in the fibers and permits an estimate of the effect of curvature on compressive strength is proposed. Two modes of failure which may result from the application of axial compressive stress are analyzed, delamination and shear instability. Based on tests and analysis, failure of boron-epoxy under axial compressive load is due to shear instability.
Document ID
19740022912
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Davis, J. G., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
August 1, 1974
Subject Category
Materials, Nonmetallic
Report/Patent Number
NASA-TM-X-71992
Report Number: NASA-TM-X-71992
Meeting Information
Meeting: ASTM: Composite Reliability Conf.
Location: Las Vegas, NV
Country: United States
Start Date: April 15, 1974
End Date: April 16, 1974
Accession Number
74N31025
Funding Number(s)
PROJECT: RTOP 505-02-41-04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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