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Thermally-driven microfracture in high temperature metal matrix compositesMicrofracture (fiber/matrix fracture, interphase debonding and interply delamination) in high temperature metal matrix composites (HTMMC), subjected to thermal loading, is computationally simulated. Both unidirectional and crossply SiC/Ti15 composites are evaluated for microfracture driven by thermal loads, using multicell finite element models. Results indicate that under thermal loads alone, microfracture propagation is not as sensitive as it is under mechanical loads.
Document ID
19920005918
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mital, Subodh K.
(Toledo Univ. OH., United States)
Chamis, Christos C.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1991
Subject Category
Composite Materials
Report/Patent Number
E-6657
NASA-TM-105305
NAS 1.15:105305
Report Number: E-6657
Report Number: NASA-TM-105305
Report Number: NAS 1.15:105305
Meeting Information
Meeting: Symposium on the Mechanics of Composites at Elevated and CryogenicTemperatures, ASME Applied Mechanics and Biomechanics Summer Conference
Location: Columbus, OH
Country: United States
Start Date: June 16, 1991
End Date: June 19, 1991
Accession Number
92N15136
Funding Number(s)
PROJECT: RTOP 510-01-0A
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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