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Fundamental aspects of and failure modes in high-temperature compositesFundamental aspects of and attendant failure mechanisms for high temperature composites are summarized. These include: (1) in-situ matrix behavior; (2) load transfer; (3) limits on matrix ductility to survive a given number of cyclic loadings; (4) fundamental parameters which govern thermal stresses; (5) vibration stresses; and (6) impact resistance. The resulting guidelines are presented in terms of simple equations which are suitable for the preliminary assessment of the merits of a particular high temperature composite in a specific application.
Document ID
19900010835
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Chamis, Christos C. (NASA Lewis Research Center Cleveland, OH, United States)
Ginty, Carol A. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1990
Subject Category
Composite Materials
Report/Patent Number
NAS 1.15:102558
NASA-TM-102558
E-5378
Meeting Information
Meeting: International SAMPE Symposium and Exhibition
Location: Anaheim, CA
Country: United States
Start Date: April 2, 1990
End Date: April 5, 1990
Accession Number
90N20151
Funding Number(s)
PROJECT: RTOP 510-01-0A
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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