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Thermal Expansion Behavior of Hot-Pressed Engineered MatricesAdvanced engineered matrix composites (EMCs) require that the coefficient of thermal expansion (CTE) of the engineered matrix (EM) matches those of the fiber reinforcements as closely as possible in order to reduce thermal compatibility strains during heating and cooling of the composites. The present paper proposes a general concept for designing suitable matrices for long fiber reinforced composites using a rule of mixtures (ROM) approach to minimize the global differences in the thermal expansion mismatches between the fibers and the engineered matrix. Proof-of-concept studies were conducted to demonstrate the validity of the concept.
Document ID
20160001712
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Raj, S. V.
(NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
February 10, 2016
Publication Date
February 1, 2016
Subject Category
Composite Materials
Report/Patent Number
NASA/TM-2016-218953
GRC-E-DAA-TN28720
E-19195
Funding Number(s)
WBS: WBS 10949.02.03.02.02.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
engineered matrix
coefficient of thermal expansion
silicon carbide
silicon nitride
engineered matrix composites
silicides
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