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Output details

15 - General Engineering

University of Oxford

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Article title

Effect of Simulated Combustor Temperature Nonuniformity on HP Vane and End Wall Heat Transfer: An Experimental and Computational Investigation

Type
D - Journal article
Title of journal
J ENG GAS TURB POWER
Article number
031901
Volume number
133
Issue number
3
First page of article
-
ISSN of journal
0742-4795
Year of publication
2011
URL
-
Number of additional authors
2
Additional information

The results presented in this paper are the first accurate experimental heat transfer measurements on nozzle guide vanes to have been performed in the presence of engine realistic temperature distortions representing the combustor. The research directly contributed to the case for significant follow on research in the Oxford Turbine Research Facility. Grants secured because of this research include: SILOET (Rolls-Royce/TSB) £500k; SAMULET (Rolls-Royce/TSB) £400k; SEOTDF (Rolls-Royce) £141k; LEMCOTEC (GKN/Rolls-Royce/EU 7th Framework) £588k; FACTOR (GKN/Rolls-Royce/EU 7th Framework) £330k; IP Vane Heat Transfer (GKN/Swedish Government) £107k.

Interdisciplinary
-
Cross-referral requested
-
Research group
G - Thermodynamics and Fluids
Proposed double-weighted
No
Double-weighted statement
-
Reserve for a double-weighted output
No
Non-English
No
English abstract
-