NDLI: Modeling the mechanical behavior of ceramic matrix composite materials

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Modeling the mechanical behavior of ceramic matrix composite materials

Content Provider	NASA Technical Reports Server (NTRS)
Author	Jordan, William
Copyright Year	1998
Description	Ceramic matrix composites are ceramic materials, such as SiC, that have been reinforced by high strength fibers, such as carbon. Designers are interested in using ceramic matrix composites because they have the capability of withstanding significant loads while at relatively high temperatures (in excess of 1,000 C). Ceramic matrix composites retain the ceramic materials ability to withstand high temperatures, but also possess a much greater ductility and toughness. Their high strength and medium toughness is what makes them of so much interest to the aerospace community. This work concentrated on two different tasks. The first task was to do an extensive literature search into the mechanical behavior of ceramic matrix composite materials. This report contains the results of this task. The second task was to use this understanding to help interpret the ceramic matrix composite mechanical test results that had already been obtained by NASA. Since the specific details of these test results are subject to the International Traffic in Arms Regulations (ITAR), they are reported in a separate document (Jordan, 1997).
File Size	346048
Page Count	8
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_19990010023
Archival Resource Key	ark:/13960/t3033sf23
Language	English
Publisher Date	1998-09-01
Access Restriction	Open
Subject Keyword	Composite Materials Toughness Ceramic Matrix Composites Creep Properties Fatigue Materials Mechanical Properties Mathematical Models Tensile Properties Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Article

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