3-D analysis of laser measurements of vortex bursting on a chined forebody fighter configuration-Reference-Cited by-同舟云学术

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3-D analysis of laser measurements of vortex bursting on a chined forebody fighter configuration

Published:1990-08-17 Issue: Volume: Page:
ISSN:
Container-title:Flight Simulation Technologies Conference and Exhibit
language:
Short-container-title:

Author:

CORNELIUS KENNETH¹

Affiliation:

1. Wright State University, Dayton, OH

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1990-3020

Reference19 articles.

1. Control of forebody vortex orientation to alleviate side forces

Cited by 7 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. Vortical Structures over a Generic Tailless Chined Forebody–Delta Wing;AIAA Journal;2024-02

2. Analysis of rolled delta wing flows using effective sweep and attack angles;Journal of Aircraft;1995-09

3. Experimental study of pneumatic control of forebody vortices at high alpha;Journal of Aircraft;1994-01

4. Simple numerical criterion for vortex breakdown;AIAA Journal;1994-01

5. A simple numerical criterion for vortex breakdown;30th Aerospace Sciences Meeting and Exhibit;1992-01-06

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