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Ceramic matrix composites properties/microstresses with complete and partial interphase bondA multilevel substructuring technique which includes a unique fiber substructuring concept is used for the analysis of continuous fiber reinforced ceramic matrix composites. This technique has four levels of substructuring--from laminate to ply, to supply, and then to fiber. A stand-alone computer code CEMCAN (Ceramic Matrix Composites Analyzer), incorporating this technique and specifically for the simulation of ceramic matrix composites behavior, is currently under development at NASA Lewis Research Center in Cleveland, Ohio. The thermal and mechanical properties, along with the microstresses, for a SiC/RBSN (silicon carbide fiber and reaction bonded silicon nitride matrix) composite at different fiber volume ratios and varying degrees of interfacial bond around the fiber circumference are computed. Values predicted by CEMCAN computer code are shown to bound the experimentally measured values. Results also show that transverse tensile strength test can be a sensitive test method to assess interfacial conditions.
Document ID
19930019882
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mital, Subodh K.
(Toledo Univ. OH., United States)
Murthy, Pappu L. N.
(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
May 1, 1993
Subject Category
Composite Materials
Report/Patent Number
NAS 1.15:106136
NASA-TM-106136
E-7816
Report Number: NAS 1.15:106136
Report Number: NASA-TM-106136
Report Number: E-7816
Meeting Information
Meeting: International SAMPE Symposium/Exhibition
Location: Anaheim, CA
Country: United States
Start Date: May 10, 1993
End Date: May 13, 1993
Accession Number
93N29071
Funding Number(s)
PROJECT: RTOP 510-01-50
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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