Output details
15 - General Engineering
Kingston University
Article title
Aerodynamic performance of bypass engine with nozzle exit area change by warped chevrons
Type
D - Journal article
Title of journal
Proceedings of the Institution of Mechanical Engineers, Part G, Journal of Aerospace Engineering
Article number
-
Volume number
224
Issue number
6
First page of article
731
ISSN of journal
0954-4100
Year of publication
2010
Number of additional authors
4
Additional information
Three methods were proposed and examined in this work, using a CFD code to demonstrate the potential improvement in engine thrust and the reduction of the impact on the environment. This paper was awarded the 2010 Kenneth Harris James Prize by the Space Division of the IMechE and the 2010 George Stephenson Prize by the IMechE for innovation and contribution to the area. Pratt & Whitney has implemented the translating nozzle technology which is one of the methods examined in this work.
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
-
