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15 - General Engineering

University of Oxford

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Output 17 of 354 in the submission

Article title

A Novel Technique for Assessing Turbine Cooling System Performance

Type

D - Journal article

DOI

10.1115/1.4001232

Title of journal

J TURBOMACH

Article number

031013

Volume number

133

Issue number

First page of article

ISSN of journal

0889-504X

Year of publication

2011

URL

Number of additional authors

Additional information

This research led to a new experimental method for assessing turbine cooling system performance which promises to significantly lower test costs and reduce the need for hot engine testing of jet-engines and industrial gas turbines. The technique is new in that it allows the overall performance of real engine components to be assessed. A joint Rolls-Royce/TSB grant for £895k has been awarded to develop a facility to demonstrate the technique on whole-engine nozzle-guide-vane rings.

Interdisciplinary

Cross-referral requested

Research group

G - Thermodynamics and Fluids

Proposed double-weighted

Double-weighted statement

Reserve for a double-weighted output

Non-English

English abstract