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On Poisson's ratio for metal matrix composite laminatesThe definition of Poisson's ratio for nonlinear behavior of metal matrix composite laminates is discussed and experimental results for tensile and compressive loading of five different boron-aluminum laminates are presented. It is shown that there may be considerable difference in the value of Poisson's ratio as defined by a total strain or an incremental strain definition. It is argued that the incremental definition is more appropriate for nonlinear material behavior. Results from a (0) laminate indicate that the incremental definition provides a precursor to failure which is not evident if the total strain definition is used.
Document ID
19790001976
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Herakovich, C. T.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Shuart, M. J.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Date Acquired
September 3, 2013
Publication Date
September 1, 1978
Subject Category
Composite Materials
Report/Patent Number
NASA-CR-157779
IR-3
VPI-E-78-26
Report Number: NASA-CR-157779
Report Number: IR-3
Report Number: VPI-E-78-26
Accession Number
79N10147
Funding Number(s)
CONTRACT_GRANT: NGR-47-004-129
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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