Hybridization of carbon-glass epoxy composites: An approach to achieve low coefficient of thermal expansion at cryogenic temperatures
Data(s) |
01/02/2011
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Resumo |
The paper is based on a study to develop carbon-glass epoxy hybrid composites with desirable thermal properties for applications at cryogenic temperatures. It analyzes the coefficient of thermal expansion of carbon-epoxy and glass-epoxy composite materials and compares it with the properties of carbon-glass epoxy hybrid composites in the temperature range 300 K to 125K. Urethane modified epoxy matrix system is used to make the composite specimens suitable for use even for temperatures as low as 20K. It is noted that the lay-up with 80% of carbon fibers in the total volume fraction of fibers oriented at 30 degrees and 20% of glass fibers oriented at 0 degrees yields near to zero coefficient of thermal expansion as the temperature is lowered from ambient to 125 K. (c) 2010 Elsevier Ltd. All rights reserved. |
Formato |
application/pdf |
Identificador |
http://eprints.iisc.ernet.in/36215/1/Hybridization.pdf Praveen, RS and Jacob, Subhash and Murthy, CRL and Balachandran, P and Rao, YVKS (2011) Hybridization of carbon-glass epoxy composites: An approach to achieve low coefficient of thermal expansion at cryogenic temperatures. In: Cryogenics, 51 (2). pp. 95-104. |
Publicador |
Elsevier Science |
Relação |
http://dx.doi.org/10.1016/j.cryogenics.2010.12.003 http://eprints.iisc.ernet.in/36215/ |
Palavras-Chave | #Aerospace Engineering (Formerly, Aeronautical Engineering) #Centre for Cryogenic Technology |
Tipo |
Journal Article PeerReviewed |