Output details
15 - General Engineering
University of Cambridge
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Article title
Fan Root Aerodynamics for Large Bypass Gas Turbine Engines: Influence on the Engine Performance and 3D Design
Type
D - Journal article
Title of journal
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME
Article number
ARTN 061017
Volume number
134
Issue number
6
First page of article
061017
ISSN of journal
0889-504X
Year of publication
2012
Number of additional authors
1
Additional information
The results of this work have been used by Rolls-Royce in the company's low pressure compression system and have led to a successful redesign of the engine-sector-stators (ESS) for the company’s newest high bypass civil engines (Dr John Bolger, ID_in_audit_file@rolls-royce.com). The Department was recently awarded the TSB project NADIT, and within the project two work packages will follow-up and extend this work (total grant value to Cambridge GBP370k).
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
-
