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Effects of Fiber/Matrix Interface and its Composition on Mechanical Properties of Hi Nicalon/Celsian CompositesFiber-reinforced ceramic matrix composites (CMC) are prospective candidate materials for high temperature structural applications in aerospace, energy conservation, power generation, nuclear, petrochemical, and other industries. At NASA Lewis, we are investigating celsian matrix composites reinforced with various types of silicon carbide fibers. The objective of the present study was to investigate the effects of fiber/matrix interface and its composition on the mechanical properties of silicon carbide (Hi-Nicalon) fiber-reinforced celsian matrix composites.
Document ID
Document Type
Preprint (Draft being sent to journal)
Bansal, Narottam P.
(NASA Lewis Research Center Cleveland, OH United States)
Eldridge, Jeffrey I.
(NASA Lewis Research Center Cleveland, OH United States)
Date Acquired
August 19, 2013
Publication Date
January 1, 1998
Subject Category
Composite Materials
Meeting Information
Composite Materials(Paris)
Funding Number(s)
PROJECT: RTOP 523-21-13
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