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Microfracture in high temperature metal matrix crossply laminatesMicrofracture (fiber/matrix fracture, interphase debonding, and inter-ply delamination) in high temperature metal matrix composites (HTMMC), subjected to both mechanical and thermal loading, is computationally simulated. A crossply 0.3 fiber volume ratio SiC/Ti15 composite with 0/90/0 lay-up is evaluated for microfracture using a multicell finite element model. A computational simulation procedure based on strain energy release rates is used to predict the fracture process and establish the hierarchy of fracture modes. Microfracture results for various loading cases are presented and discussed.
Document ID
19910015884
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mital, Subodh K.
(NASA Lewis Research Center Cleveland, 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
NAS 1.15:104381
E-6201
NASA-TM-104381
ICOMP-91-8
Report Number: NAS 1.15:104381
Report Number: E-6201
Report Number: NASA-TM-104381
Report Number: ICOMP-91-8
Meeting Information
Meeting: Winter Annual Meeting and Symposium on Failure Mechanisms in High Temperature Composites
Location: Atlanta, GA
Country: United States
Start Date: December 1, 1991
End Date: December 6, 1991
Sponsors: AME
Accession Number
91N25198
Funding Number(s)
PROJECT: RTOP 510-10-50
CONTRACT_GRANT: NASA ORDER C-99066-G
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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