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Computational simulation of high temperature metal matrix composites cyclic behaviorA procedure was developed and is described which can be used to computationally simulate the cyclic behavior of high temperature metal matrix composites (HTMMC) and its degradation effects on the structural response. This procedure consists of HTMMC mechanics coupled with a multifactor interaction constituent material relationship and with an incremental iterative nonlinear analysis. The procedure is implemented in a computer code that can be used to computationally simulate the thermomechanical behavior of HTMMC starting from the fabrication process and proceeding through thermomechanical cycling, accounting for the interface/interphase region. Results show that combined thermal/mechanical cycling, the interphase, and in situ matrix properties have significant effects on the structural integrity of HTMMC.
Document ID
19890018424
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Chamis, C. C.
(NASA Lewis Research Center Cleveland, OH, United States)
Murthy, P. L. N.
(NASA Lewis Research Center Cleveland, OH, United States)
Hopkins, D. A.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
November 8, 1988
Subject Category
Composite Materials
Report/Patent Number
E-4888
NAS 1.15:102115
NASA-TM-102115
Report Number: E-4888
Report Number: NAS 1.15:102115
Report Number: NASA-TM-102115
Meeting Information
Meeting: ASTM Symposium on Thermal and Mechanical Behavior of Ceramic and Metal Matrix Composites
Location: Atlanta, GA
Country: United States
Start Date: November 7, 1988
End Date: November 8, 1988
Accession Number
89N27795
Funding Number(s)
PROJECT: RTOP 505-63-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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