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Output details

15 - General Engineering

University of Cambridge

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Article title

Heat Transfer in Turbine Hub Cavities Adjacent to the Main Gas Path

Type
D - Journal article
Title of journal
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME
Article number
ARTN 021025
Volume number
135
Issue number
2
First page of article
021025
ISSN of journal
0889-504X
Year of publication
2013
Number of additional authors
4
Additional information

Winner of ASME Turbo-Expo 2010 Heat Transfer Committee Best Paper Award. This work led to a step change in the confidence with which coupled fluid-solid predictions can be made. The Rolls-Royce Trent 1000 development experienced significant challenges because of uncertainties in thermomechanical modelling. The reduction in uncertainty gained through the validation presented here has led to wider take-up of the methods within Rolls-Royce (ID_in_audit_file@rolls-royce.com) as well as exploitation by other partners of a recent EU FP6 consortium (TATEF II): Siemens; Avio; Turbomeca; SNECMA; Alstom; ITP and MTU.

Interdisciplinary
-
Cross-referral requested
-
Research group
None
Proposed double-weighted
No
Double-weighted statement
-
Reserve for a double-weighted output
No
Non-English
No
English abstract
-