Modification of static-wing tip vortex via a slender half-delta wing-Reference-Cited by-同舟云学术

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Modification of static-wing tip vortex via a slender half-delta wing

Published:2013-11 Issue: Volume:43 Page:1-14
ISSN:0889-9746
Container-title:Journal of Fluids and Structures
language:en
Short-container-title:Journal of Fluids and Structures

Author:

Lee T.,Pereira J.

Publisher

Elsevier BV

Subject

Mechanical Engineering

Reference24 articles.

1. Study of the reverse delta wing;Altaf;Journal of Aircraft,2011

2. Transport aircraft wake influenced by oscillating winglet flaps;Breitsamter;Journal of Aircraft,2009

3. Quantitative low-speed wake surveys;Brune;Journal of Aircraft,1994

4. The structure and induced drag of a tip vortex;Birch;Journal of Aircraft,2004

5. Duraisamy, K., Baeder, J.D., 2003. Control of Tip Vortex Structure Using Steady and Oscillatory Blowing. AIAA Paper 2003-3407.

Cited by 10 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. On the influence of spanwise deformation on lift coefficient and trailing vortices properties at low Reynolds number;Physics of Fluids;2024-03-01

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

3. Effect of a Rotating and Swept Wingtip on Streamwise Gust Alleviation;AIAA Journal;2021-03

4. Effect of a Directionally Porous Wing Tip on Tip Vortex;Journal of Applied Fluid Mechanics;2020-03-01

5. The Lift Force Produced by an Unsteady Translating Plate with a Rotating Tip;AIAA Scitech 2020 Forum;2020-01-05

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