Effect of Multiscale Endplates on Wing-Tip Vortex-Reference-Cited by-同舟云学术

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Effect of Multiscale Endplates on Wing-Tip Vortex

Published:2021-05 Issue:5 Volume:59 Page:1614-1628
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Gehlert Pascal¹,Cherfane Ziad²,Cafiero Gioacchino³,Vassilicos John Christos⁴

Affiliation:

1. University of Cambridge, Cambridge, England CB2 1PZ, United Kingdom

2. Imperial College London, London, England SW7 2AZ, United Kingdom

3. University of Surrey, Guildford, England GU2 7HX, United Kingdom

4. University of Lille, CNRS, ONERA, Arts et Métiers ParisTech, Centrale Lille, UMR 9014–LMFL—Kampé de Feriet, F-59000 Lille, France

Funder

ERC Advanced Grant awarded to J. C. Vassilicos

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference32 articles.

1. Stability theory for a pair of trailing vortices

2. WidnallS. E.BlissD.ZalayA. “Theoretical and Experimental Study of the Stability of a Vortex Pair,” Aircraft Wake Turbulence and Its Detection, Springer-Verlag, Berlin, 1971, pp. 305–338. 10.1007/978-1-4684-8346-8_19

3. AIRPLANE TRAILING VORTICES

4. Wing tip vortex control using synthetic jets

5. Mid-wake wing tip vortex dynamics with active flow control

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1. Near field evolution of wingtip vortices under synthetic-jet based control;Aerospace Science and Technology;2024-05

2. Manipulation of a turbulent boundary layer using sinusoidal riblets;Journal of Fluid Mechanics;2024-04-08

3. Developments in Wingtip Vorticity Mitigation Techniques: A Comprehensive Review;Aerospace;2023-12-29

4. Drag reduction in a turbulent boundary layer with sinusoidal riblets;Experimental Thermal and Fluid Science;2022-11

5. Deep reinforcement learning for active control of a three-dimensional bluff body wake;Physics of Fluids;2022-10

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