Flow Control on a Three Dimensional Forebody Using Pulsed DC Plasma Actuator Operating in Air-Reference-Cited by-同舟云学术

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Flow Control on a Three Dimensional Forebody Using Pulsed DC Plasma Actuator Operating in Air

Published:2008-01-07 Issue: Volume: Page:
ISSN:
Container-title:46th AIAA Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Singh Kunwar¹,Roy Subrata²

Affiliation:

1. Computational Plasma Dynamics Laboratory and Test Facility

2. University of Florida

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2008-1102

Reference25 articles.

1. O.A.S.Kandil,H.HazemandC.H.Liu,AIAA-1992-4426AIAAAtmosphericFlightMechanicsConference,Hilton HeadIsland,SC, 1992, Washington,AIAA,1992, 244.

2. Celik,ZekiZ.Roberts,Leonard,AIAA-1992-4430AIAAAtmosphericFlightMechanicsConference,HiltonHead Island,SC,Washington,AIAA,1992,293.

3. N.Pedreiro,S.M.Rock,Z.Z.CelikandL.Roberts,JournalofAircraft35,69(1998).

4. A. A. Maslov, B. Y. Zanin, A. A. Sidorenko, B. V. Postnikov, V. P. Fomichev, A. D. Budovsky, and N. Malmuth, AIAA-2005-400,43rdAIAAAerospaceSciencesMeetingandExhibit2005,Reno,Nevada.

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