Reynolds-number dependency of the leading edge vortex on a fast pitch-up flat plate
Version 2 2024-06-04, 05:48Version 2 2024-06-04, 05:48
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conference contribution
posted on 2024-06-04, 05:48 authored by X Zhang, V Chai, JU SchlüterWe 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.
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Location
Honolulu, HawaiiStart date
2011-06-27End date
2011-06-30ISBN-13
9781624101458Publication classification
E1.1 Full written paper - refereedTitle of proceedings
AIAA 2011 : Proceedings of the 29th AIAA Applied Aerodynamics Conference 2011Event
American Institute of Aeronautics and Astronautics. Conference (29th : 2011 : Honolulu, Hawaii)Publisher
American Institute of Aeronautics and AstronauticsUsage metrics
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