Sayma, A I, Kim, M and Smith, N H (2003) Leading-edge shape and aeroengine fan blade performance. Journal of Propulsion and Power, 19 (3). pp. 517-520. ISSN 0748-4658

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Item Type:	Article
Additional Information:	This paper describes the results of numerical predictions of the effect of leading edge erosion on the performance and flutter stability of turbomachinery fan blades. The results has a significant impact on the design of aero-engine fan design at Rolls-Royce by providing an understanding of the impact of the in-service change in the shape of the blade's leading edge on performance and flutter stability. Guide lines were produced to assess the effect of re-profiling the fan blades to recover the loss of performance resulting from in-service leading edge erosion. For more information, contact Nigel Smith from Rolls-Royce: Tel: 01332244978
Schools and Departments:	School of Engineering and Informatics > Engineering and Design
Depositing User:	Naser Sayma
Date Deposited:	06 Feb 2012 21:08
Last Modified:	01 Sep 2012 20:58
URI:	http://sro.sussex.ac.uk/id/eprint/29778

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