'Microblowing' for high-angle-of-attack vortex flow control on a fighter aircraft-Reference-Cited by-同舟云学术

'Microblowing' for high-angle-of-attack vortex flow control on a fighter aircraft

Published:1996-01-15 Issue: Volume: Page:
ISSN:
Container-title:34th Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Roos Frederick¹

Affiliation:

1. McDonnell Douglas Corp., Saint Louis, MO

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1996-543

Reference9 articles.

1. Skow,A.M.andErickson,G.E. "Modern Fighter Aircraft Design for High-Angle-of-Attack Maneuvering,"in HighAngle-of-AttackAerodynamics. AGARDLS-121.March 1982.

2. Tobak,M., Degani,D.,andZilliac,G.G. "OntheOrigin and Behaviorof AsymmetricVortices,"inHigh Angleof Attack Technology.NASA CP-3149,Vol.I, 1992.

3. Roos,F.W.andMagness,C.L."Bluntness andBlowing for Flowfield Asymmetry ControlonSlender Forebodies,"AIAA PaperNo.93-3409, August 1993.

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