Vortex suppression on highly-swept wings by suction boundary-layer control-Reference-Cited by-同舟云学术

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Vortex suppression on highly-swept wings by suction boundary-layer control

Published:1995-01-09 Issue: Volume: Page:
ISSN:
Container-title:33rd Aerospace Sciences Meeting and Exhibit
language:
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Author:

Owens D,Perkins John

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1995-683

Reference20 articles.

1. Thomas,J.L., Taylor, S.L. and Anderson,W.K. "Navier-StokesComputationsof VorticalFlows OverLowAspectRatioWings." AIAA Paper 87-0207.

2. IS. Rao, DhanvadaM. "Exploratory Subsonic Investigation of Vortex-Flap Concept on Arrow WingConfiguration." NASA CP2108,pp. 117-I 74

Cited by 5 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Plasma control of vortex flow on a delta wing at high angles of attack;Experiments in Fluids;2013-08

2. Control of Vortex Breakdown over a Delta Wing Using Forebody Spanwise Slot Blowing;AIAA Journal;2007-01

3. Response of unconfined vortex breakdown to axial pulsing;Physics of Fluids;2006-03

4. Research into vortex breakdown control;Progress in Aerospace Sciences;2001-05

5. Improved performance on highly swept wings by suction boundary-layer control;34th Aerospace Sciences Meeting and Exhibit;1996-01-15

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