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Inelastic response of metal matrix composites under biaxial loadingTheoretical predictions and experimental results were obtained for inelastic response of unidirectional and angle ply composite tubes subjected to axial and torsional loading. The composite material consist of silicon carbide fibers in a titanium alloy matrix. This material is known to be susceptible to fiber matrix interfacial damage. A method to distinguish between matrix yielding and fiber matrix interfacial damage is suggested. Biaxial tests were conducted on the two different layup configurations using an MTS Axial/Torsional load frame with a PC based data acquisition system. The experimentally determined elastic moduli of the SiC/Ti system are compared with those predicted by a micromechanics model. The test results indicate that fiber matrix interfacial damage occurs at relatively low load levels and is a local phenomenon. The micromechanics model used is the method of cells originally proposed by Aboudi. Finite element models using the ABACUS finite element program were used to study end effects and fixture specimen interactions. The results to date have shown good correlation between theory and experiment for response prior to damage initiation.
Document ID
19910017981
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Lissenden, C. J.
(Virginia Univ. Charlottesville, VA, United States)
Mirzadeh, F.
(Virginia Univ. Charlottesville, VA, United States)
Pindera, M.-J.
(Virginia Univ. Charlottesville, VA, United States)
Herakovich, C. T.
(Virginia Univ. Charlottesville, VA, United States)
Date Acquired
September 6, 2013
Publication Date
June 30, 1991
Publication Information
Publication: NASA-UVA Light Aerospace Alloy and Structures Technology Program (LA2ST)
Subject Category
Metallic Materials
Accession Number
91N27295
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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