Experimental and numerical investigation of leading edge Krueger flaps at low Reynolds numbers
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2012
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Cranfield University
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Thesis or dissertation
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Abstract
Recent 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.
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© Cranfield University 2012. All rights reserved. No part of this publication may be reproduced without the written permission of the copyright owner.