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Heat transfer in high-pressure compressor gas turbine internal air systems: A rotating disc-cone cavity with axial throughflow

Alexiou, A, Hills, NJ, Long, CA and Turner, AB (2000) Heat transfer in high-pressure compressor gas turbine internal air systems: A rotating disc-cone cavity with axial throughflow EXPERIMENTAL HEAT TRANSFER, 13 (4). pp. 299-328.

Full text not available from this repository.
Item Type: Article
Authors :
NameEmailORCID
Alexiou, AUNSPECIFIEDUNSPECIFIED
Hills, NJn.hills@surrey.ac.ukUNSPECIFIED
Long, CAUNSPECIFIEDUNSPECIFIED
Turner, ABUNSPECIFIEDUNSPECIFIED
Date : 1 October 2000
Uncontrolled Keywords : Science & Technology, Physical Sciences, Technology, Thermodynamics, Engineering, Mechanical, Engineering, ENGINEERING, MECHANICAL, THERMODYNAMICS
Related URLs :
Depositing User : Symplectic Elements
Date Deposited : 17 May 2017 12:28
Last Modified : 17 May 2017 15:04
URI: http://epubs.surrey.ac.uk/id/eprint/835468

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