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Please use this identifier to cite or link to this item: https://scholarbank.nus.edu.sg/handle/10635/128937
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dc.titleReynolds-number dependency of the leading edge vortex on a fast pitch-up flat plate
dc.contributor.authorZhang, X.
dc.contributor.authorChai, V.
dc.contributor.authorSchlüter, J.U.
dc.date.accessioned2016-10-22T07:46:00Z
dc.date.available2016-10-22T07:46:00Z
dc.date.issued2011
dc.identifier.citationZhang, X.,Chai, V.,Schlüter, J.U. (2011). Reynolds-number dependency of the leading edge vortex on a fast pitch-up flat plate. 29th AIAA Applied Aerodynamics Conference 2011. ScholarBank@NUS Repository.
dc.identifier.isbn9781624101458
dc.identifier.urihttp://scholarbank.nus.edu.sg/handle/10635/128937
dc.description.abstractWe present a numerical study on the influence of the Reynolds-number on the lift enhancing effect of a dynamic leading edge vortex. Our approach is based on a combination of Large-Eddy Simulations and the Immersed Boundary technique. We show the background and validation of this code before applying this approach to a fast pitching plate to determine the influence of the leading edge vortex on the unsteady lift. Our results suggest that an optimal Reynoldsnumber exists that maximizes the benefit of the leading edge vortex. © 2011 by Nanyang Technological University.
dc.sourceScopus
dc.typeConference Paper
dc.contributor.departmentTEMASEK LABORATORIES
dc.description.sourcetitle29th AIAA Applied Aerodynamics Conference 2011
dc.identifier.isiutNOT_IN_WOS
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