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Two-Channel Spark Disharge for Flow Control On a Body of Revolution

  • Published:2005-01-10 Issue: Volume: Page:
  • ISSN:
  • Container-title:43rd AIAA Aerospace Sciences Meeting and Exhibit
  • language:
  • Short-container-title:

Author:

Maslov A.1,Zanin B.1,Sidorenko A.1,Postnikov B.1,Fomichev V.1,Budovsky A.1,Malmuth N.2

Affiliation:

1. ITAM

2. Rockwell Scientific

Publisher

American Institute of Aeronautics and Astronautics

Reference4 articles.

1. Plasma Control of Forebody Nose Vortex Symmetry Breaking

2. Skow,A.M.andPeake,D.J.,AGARDLectureSeriesNo.121,"HighAngleofAttackAerodynamics,"AGARD-LS-121,pp. 10-1-10-22, March 1982

3. Ericsson,L.E.andReding,J.P."AerodynamicEffectsofAsymmetricVortexSheddingfromSlenderBodies,"AIAAPaper No. 85-1797, 1985.

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4. Pulsed Discharge Actuators for Rectangular Wing Separation Control;45th AIAA Aerospace Sciences Meeting and Exhibit;2007-01-08

5. Conical Navier-Stokes Modeling of Forebody Vortex Symmetry Plasma Control;45th AIAA Aerospace Sciences Meeting and Exhibit;2007-01-08
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