Heat Transfer in H P Compressor Gas Turbine Internal Air Systems: Measurements from the Peripheral Shroud of a Rotating Cavity with Axial Throughflow

Long, C A, Alexiou, A and Smout, P D (2003) Heat Transfer in H P Compressor Gas Turbine Internal Air Systems: Measurements from the Peripheral Shroud of a Rotating Cavity with Axial Throughflow. In: 2nd International Conference on Heat Transfer, Fluid Mechanics and Thermodynamics, Victoria Falls, Zambia.

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Item Type: Conference or Workshop Item (Paper)
Additional Information: This presents heat transfer measurements from the inner peripheral surface of a rotating test rig representing a gas turbine high pressure compressor internal air system. Tests were carried out at engine-representative operating conditions. The data are correlated by appropriate modification of existing correlations for free convection from a horizontal plate. This work was funded by the EU and a number of gas turbine manufacturers. It is of significant commercial importance, and has been accepted as a standard correlation in design codes. (Contact: Jeff Dixon, Chief of Thermal Systems Group, Rolls Royce plc, Derby DE24 8BJ; email: jeffrey.dixon@rolls-royce.com).
Schools and Departments: School of Engineering and Informatics > Engineering and Design
Depositing User: Christopher Long
Date Deposited: 06 Feb 2012 20:53
Last Modified: 04 Apr 2012 11:27
URI: http://sro.sussex.ac.uk/id/eprint/28582
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