Slender delta wing at high angles of attack - A flow visualization study-Reference-Cited by-同舟云学术

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Slender delta wing at high angles of attack - A flow visualization study

Published:1987-06-08 Issue: Volume: Page:
ISSN:
Container-title:19th AIAA, Fluid Dynamics, Plasma Dynamics, and Lasers Conference
language:
Short-container-title:

Author:

AYOUB A.¹,MCLACHLAN B.²

Affiliation:

1. Stanford University, CA

2. NASA, Ames Research Center, Moffett Field, CA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1987-1230

Reference11 articles.

1. Future fighter technologies

2. Dynamic load measurements with delta wings undergoing self-induced roll oscillations

3. The fluid mechanics of slender wing rock

Cited by 14 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. Leading-Edge Vortex Structure of Nonslender Delta Wings at Low Reynolds Number;AIAA Journal;2003-01

2. The passage toward stall of nonslender delta wings at low Reynolds number;15th AIAA Computational Fluid Dynamics Conference;2001-06-11

3. Insensitivity of Unsteady Vortex Interactions to Reynolds Number;AIAA Journal;2000-05

4. Oscillation of Vortex Breakdown Location and Blowing Control of Time-Averaged Location;AIAA Journal;2000-05

5. Nonlinear Response of Vortex Breakdown over a Pitching Delta Wing;Journal of Aircraft;1999-05

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