Heat Transfer in HP Compressor Gas Turbine Internal Air Systems: a Rotating Disc-cone Cavity with Axial Throughflow

Alexiou, A, Hills, N J, Long, C A, Turner, A B and Millward, J A (2000) Heat Transfer in HP Compressor Gas Turbine Internal Air Systems: a Rotating Disc-cone Cavity with Axial Throughflow. Experimental Heat Transfer, 13 No.. pp. 299-328. ISSN 0891-6152

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Item Type: Article
Schools and Departments: School of Engineering and Informatics > Engineering and Design
Depositing User: Christopher Long
Date Deposited: 06 Feb 2012 20:04
Last Modified: 11 Jun 2013 12:32
URI: http://sro.sussex.ac.uk/id/eprint/23923
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