Output details
15 - General Engineering
University of Cambridge
Article title
The Effect of Leading-Edge Geometry on Wake Interactions in Compressors
Type
D - Journal article
Title of journal
J TURBOMACH
Article number
041013
Volume number
131
Issue number
4
First page of article
041013
ISSN of journal
0889-504X
Year of publication
2009
URL
-
Number of additional authors
2
Additional information
The conference version of the paper was awarded an American Society of Mechanical Engineers IGTI Turbomachinery Committee Best Paper Award 2007. The work confirmed to Rolls Royce that current leading edge geometry of compressor blades had a significant negative impact on performance. Mitsubishi Heavy Industries and Rolls Royce confirm that they have improved leading edge geometry in line with this work. ID_in_audit_file@mhi.co.jp, ID_in_audit_file@rolls-royce.com.
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
-
