Water Tunnel Investigation of Forebody Characteristics at High Angles of Attack
Author:
Affiliation:
1. Linköpings University
2. ENSMA
3. Linköping University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2003-3414
Reference15 articles.
1. Erickson Gary E. and Brandon Jay M. "Low speed experimental study of the vortex flow effects of a fighter having unconventional cross-section", AIAA-85-1798,1985.
2. Roos Frederick W. and Magness Charles L. "Yaw effects on the high-alpha flow field of a chinedforebody",AIAA94-0073,1994.
3. Erickson Gary E. and Brandon Jay M. "On the non-linear aerodynamic and stability characteristics of a generic chine-forebody slender-wing fighter configuration",AIAA-87-2617,1987.
4. Mange, R. L. and Roos, F. W. "The Aerodynamic of a Chined Forebody", AIAA-98-2903,1998.
Cited by 2 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. Influence of artificial tip perturbation on asymmetric vortices flow over a chined fuselage;Chinese Journal of Aeronautics;2015-08
2. Study on flow behavior and structure over chined fuselage at high angle of attack;Science China Technological Sciences;2010-07-15
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