The control of vortical flow on a delta wing at high angles of attack-Reference-Cited by-同舟云学术

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The control of vortical flow on a delta wing at high angles of attack

Published:1987-08-17 Issue: Volume: Page:
ISSN:
Container-title:5th Applied Aerodynamics Conference
language:
Short-container-title:

Author:

WOOD N.¹,ROBERTS L.¹

Affiliation:

1. Stanford University, CA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1987-2278

Reference9 articles.

1. Jun, Y.U. and Nelson, R.C ' Leading Edge Vortex Dynamics on a Delta Wing Undergoing a Wing Rock Motion' AIAA Paper 87-0332 1987

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. Flow control over a maneuvering delta wing at high angles of attack;AIAA Journal;1996-04

2. Delta wing vortex control via recessed angled spanwise blowing;Journal of Aircraft;1995-07

3. Active control of wing rock using tangential leading-edge blowing;Journal of Aircraft;1994-05

4. Roll moment characteristics of asymmetric tangential leading-edge blowing on a delta wing;Journal of Aircraft;1994-01

5. Vortex control technique for the attenuation of fin buffet;Journal of Aircraft;1993-11

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