Output details
15 - General Engineering
University of Cambridge
Article title
A Study of Fan-Distortion Interaction Within the NASA Rotor 67 Transonic Stage
Type
D - Journal article
Title of journal
Journal of Turbomachinery
Article number
051011
Volume number
134
Issue number
5
First page of article
-
ISSN of journal
0889-504X
Year of publication
2012
URL
-
Number of additional authors
2
Additional information
The research in this paper involved collaborations with both NASA and Rolls-Royce plc. The paper has been useful to NASA in the design of coupled inlets and fan systems to minimise fan-distortion interaction. [Contact: Tony Strazisar, ID_in_audit_file@nasa.gov]. As a result of this research Rolls-Royce funded an Industrial CASE award for a follow-on PhD studentship and invited Cambridge to participate in the Distributed Propulsion project, DEAP, funded by the Technology Strategy Board (Project No. 101286, grant value GBP109k). [Contact: 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
-
