Experimental and numerical investigation of leading edge Krueger flaps at low Reynolds numbers

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dc.contributor.advisorLawson, Nicholas J.
dc.contributor.authorMoraris, Vassilis Michael
dc.date.accessioned2013-05-23T13:30:43Z
dc.date.available2013-05-23T13:30:43Z
dc.date.issued2012
dc.description.abstractRecent publications examining the flight of Eagles have shown that leading edge feather deflections occur on the lower surface of the wings in free flight to create a leading edge flap analogous to a Krueger flap system. Such passive high lift devices may be adaptable to the lifting surfaces of unmanned air vehicles (UAVs). This work is aimed to an application of a passive leading edge Krueger device which will deploy during the landing and takeoff stages of a UAV flight. Cont/d.en_UK
dc.identifier.urihttp://dspace.lib.cranfield.ac.uk/handle/1826/7913
dc.language.isoenen_UK
dc.publisherCranfield Universityen_UK
dc.rights© Cranfield University 2012. All rights reserved. No part of this publication may be reproduced without the written permission of the copyright owner.en_UK
dc.titleExperimental and numerical investigation of leading edge Krueger flaps at low Reynolds numbersen_UK
dc.typeThesis or dissertationen_UK
dc.type.qualificationlevelMastersen_UK
dc.type.qualificationnameMPhilen_UK

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