Suppression of stall on high-camber flap using upper-surface blowing

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dc.contributor.advisor Titarev, Vladimir
dc.contributor.advisor Guo, S. J.
dc.contributor.author Fang, Li
dc.date.accessioned 2011-07-06T15:56:08Z
dc.date.available 2011-07-06T15:56:08Z
dc.date.issued 2011-01
dc.identifier.uri http://dspace.lib.cranfield.ac.uk/handle/1826/5636
dc.description.abstract For many years, high-lift devices of an aeroplane have been employed to enhancing the aerodynamic performance of the wing during take-off and landing. But their complex geometries not only increase the design and manufacture cost, but also result in lower maintainability and reliability. Further more, they have been thought to be a major noise source of civil airliners. As one of the possible solutions, single-slot variable-camber flap design can greatly decrease the system complexity and the design cost of the high-lift system. However, the deteriorated stall behaviour of the flap prevents this concept to obtain its full benefits at high flap deflection angle. Cont/d. en_UK
dc.language.iso en en_UK
dc.publisher Cranfield University en_UK
dc.rights © Cranfield University 2011. All rights reserved. No part of this publication may be reproduced without the written permission of the copyright owner. en_UK
dc.title Suppression of stall on high-camber flap using upper-surface blowing en_UK
dc.type Thesis or dissertation en_UK
dc.type.qualificationlevel Masters en_UK
dc.type.qualificationname Masters by Research en_UK


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