The counter-rotating pair of vortices formed from aircraft wingtips in flight presents a potential hazard to other aircraft in the form of a sustained rolling moment. Such a trailing vortex pair travels downwards with a self-induced velocity, and may interact with the ground plane at airports. The ground affects both the trajectories of the original vortex pair as well as the development of three-dimensional instabilities in the pair. As the vortex pair approaches the ground plane, it generates a boundary layer on the ground that separates to form opposite-sign, secondary vortices. These secondary vortices impact the trajectories and development of the original vortex pair. The focus of the current paper is not simply the 2D behaviour of the vorticity, but also the development of 3D instabilities. A novel technique has been developed using laser-induced fluorescence to visualise this secondary vorticity in unprecedented detail, revealing new flow phenomena.
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December 2009
Research Article|
December 01 2009
Briefing: Interaction of a counter-rotating vortex pair with the ground Available to Purchase
V. A. Miller;
V. A. Miller
Cornell University
New York, USA
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D. M. Harris;
D. M. Harris
Cornell University
New York, USA
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Charles H. K. Williamson
Charles H. K. Williamson
Cornell University
New York, USA
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Publisher: Emerald Publishing
Revision Received:
August 10 2009
Accepted:
August 11 2009
Online ISSN: 1755-0785
Print ISSN: 1755-0777
© 2009 Thomas Telford Ltd
2009
Proceedings of the Institution of Civil Engineers - Engineering and Computational Mechanics (2009) 162 (4): 181–183.
Article history
Revision Received:
August 10 2009
Accepted:
August 11 2009
Citation
Miller VA, Harris DM, Williamson CHK (2009), "Briefing: Interaction of a counter-rotating vortex pair with the ground". Proceedings of the Institution of Civil Engineers - Engineering and Computational Mechanics, Vol. 162 No. 4 pp. 181–183, doi: https://doi.org/10.1680/eacm.2009.162.4.181
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