Output details
12 - Aeronautical, Mechanical, Chemical and Manufacturing Engineering
University of Bath
Article title
Aerothermal investigations of tip leakage flow in axial flow turbines-part III: TIP cooling
Type
D - Journal article
Title of journal
Journal of Turbomachinery: Transactions of the ASME
Article number
011008
Volume number
131
Issue number
1
First page of article
-
ISSN of journal
0889-504X
Year of publication
2009
Number of additional authors
6
Additional information
This paper received the 2008 Best Paper Award from the ASME Heat Transfer Committee. It is the first to show the thermodynamic benefit of injecting coolant into the separation bubble on the tip of a turbine blade. The output was a collaboration between the Universities of Bath and Cambridge, as well as European Gas Turbines (now Siemens) and Alstom Power. The research was funded by the EPSRC (GR/N33997/01; GR/N33980/01, £178k). The paper also led to a research project in Framework 5 (AITEB) at Cambridge.
Interdisciplinary
-
Cross-referral requested
-
Research group
D - Aero, Thermo and Energy Engineering
Proposed double-weighted
No
Double-weighted statement
-
Reserve for a double-weighted output
No
Non-English
No
English abstract
-
