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Interphase layer optimization for metal matrix composites with fabrication considerationsA methodology is presented to reduce the final matrix microstresses for metal matrix composites by concurrently optimizing the interphase characteristics and fabrication process. Application cases include interphase tailoring with and without fabrication considerations for two material systems, graphite/copper and silicon carbide/titanium. Results indicate that concurrent interphase/fabrication optimization produces significant reductions in the matrix residual stresses and strong coupling between interphase and fabrication tailoring. The interphase coefficient of thermal expansion and the fabrication consolidation pressure are the most important design parameters and must be concurrently optimized to further reduce the microstresses to more desirable magnitudes.
Document ID
19910020967
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Morel, M.
(Sverdrup Technology, Inc., Brook Park OH., United States)
Saravanos, D. A.
(Case Western Reserve Univ. Cleveland, OH., United States)
Chamis, C. 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-6457
NASA-TM-105166
NAS 1.15:105166
Report Number: E-6457
Report Number: NASA-TM-105166
Report Number: NAS 1.15:105166
Meeting Information
Meeting: International SAMPE Symposium and Exhibition
Location: San Diego, CA
Country: United States
Start Date: April 15, 1991
End Date: April 18, 1991
Accession Number
91N30281
Funding Number(s)
PROJECT: RTOP 510-10-50
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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