Turbine Aerodynamic Performance Measurement under Non-Adiabatic Conditions

Atkins, N R and Ainsworth, R W (2007) Turbine Aerodynamic Performance Measurement under Non-Adiabatic Conditions. In: American Society of Mechanical Engineers (ASME) Turbo Expo 2007, May 14-17, Montreal, Canada., Montreal, Canada.

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Item Type: Conference or Workshop Item (Paper)
Additional Information: As turbine inlet temperatures are pushed higher for fuel efficiency, the aerodynamic and heat transfer characteristics of turbine design must be modeled/studied in tandem. This paper demonstrates a rigorous methodology to account for heat transfer in the calculation of turbine aerodynamic efficiency. Since publishing, the technique has been used in Rolls-Royce in-house methodology by Dr. John Northall (john.northall@rolls-royce.com) and utilized for work on the TATEF II FP6 European Union collaborative project. The method is likely to be adopted at the Von Karman Institute (Dr G Paniagua - paniagua@vki.ac.be). Selected by conference chair for ASME Journal of Turbomachinery.
Schools and Departments: School of Engineering and Informatics > Engineering and Design
Depositing User: EPrints Services
Date Deposited: 06 Feb 2012 18:35
Last Modified: 03 Apr 2012 14:29
URI: http://sro.sussex.ac.uk/id/eprint/17268
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