Vortex Core and Its Effects on the Stability of Vortex Flow over Slender Conical Bodies-Reference-Cited by-同舟云学术

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Vortex Core and Its Effects on the Stability of Vortex Flow over Slender Conical Bodies

Published:2005-01-10 Issue: Volume: Page:
ISSN:
Container-title:43rd AIAA Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Cai Jinsheng¹,Tsai Her-Mann¹,Luo Shijun²,Liu Feng²

Affiliation:

1. National University of Singapore

2. University of California, Irvine

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-62

Reference39 articles.

1. Pressures Around an Inclined Ogive Cylinder with Laminar, Transitional, or Turbulent Separation

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1. Leading-Edge Vortex as a High-Lift Mechanism for Large-Aspect-Ratio Wings;AIAA Journal;2020-07

2. Lift Enhancement by a Stationary Leading-Edge Vortex Over a High Aspect Ratio Wing;AIAA Aviation 2019 Forum;2019-06-14

3. Effect of Dorsal Fin on Symmetry of Vortices over Slender Delta Wing;AIAA Journal;2016-08

4. Design of an Optimal Wing-Body Configuration to Delay Onset of Vortex Asymmetry;AIAA Journal;2011-01

5. Euler Solutions of Flow Around a Rectangular Wing with Square Tip;45th AIAA Aerospace Sciences Meeting and Exhibit;2007-01-08

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