Aerodynamic performance of bypass engine with nozzle exit area change by warped chevrons

Sloan, B, Wang, J, Spence, S, Raghunathan, S and Riordan, D (2010) Aerodynamic performance of bypass engine with nozzle exit area change by warped chevrons. Proceedings of the Institution of Mechanical Engineers, Part G, Journal of Aerospace Engineering, 224(6), pp. 731-743. ISSN (print) 0954-4100

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Item Type: Article
Research Area: Mechanical, aeronautical and manufacturing engineering
Faculty, School or Research Centre: Faculty of Engineering (until 2011)
Depositing User: Automatic Import Agent
Date Deposited: 11 Jul 2011 10:04
Last Modified: 10 Jun 2013 10:32
URI: http://eprints.kingston.ac.uk/id/eprint/18480

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