Deakin University
Browse

Reynolds-number dependency of the leading edge vortex on a fast pitch-up flat plate

Version 2 2024-06-04, 05:48
Version 1 2017-04-07, 11:27
conference contribution
posted on 2024-06-04, 05:48 authored by X Zhang, V Chai, JU Schlüter
We 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.

History

Location

Honolulu, Hawaii

Start date

2011-06-27

End date

2011-06-30

ISBN-13

9781624101458

Publication classification

E1.1 Full written paper - refereed

Title of proceedings

AIAA 2011 : Proceedings of the 29th AIAA Applied Aerodynamics Conference 2011

Event

American Institute of Aeronautics and Astronautics. Conference (29th : 2011 : Honolulu, Hawaii)

Publisher

American Institute of Aeronautics and Astronautics

Usage metrics

    Research Publications

    Categories

    No categories selected

    Exports

    RefWorks
    BibTeX
    Ref. manager
    Endnote
    DataCite
    NLM
    DC