Shock-tube facility for MGD supersonic flow control-Reference-Cited by-同舟云学术

Shock-tube facility for MGD supersonic flow control

Published:2000-06-19 Issue: Volume: Page:
ISSN:
Container-title:21st Aerodynamic Measurement Technology and Ground Testing Conference
language:
Short-container-title:

Author:

Bobashev S.¹,D'yakonova E.¹,Erofeev A.¹,Lapushkina T.¹,Maslennikov V.¹,Poniaev S.¹,Sacharov A.¹,Vasil'eva R.¹,Van Wie D.²

Affiliation:

1. RAS, Physico-Technical Inst., St. Petersburg, Russia

2. Johns Hopkins Univ., APL, Laurel, MD

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2000-2647

Reference8 articles.

1. [I] V.L. Fraishtadt, A.L.Kuranov, and E.G.Sheikin, "Use of MHD Systems in Hypersonic Aircraft" Technical Physics,43,ll,1998,ppl 309-1313.

2. E.P.Gurijanov and P.T.Harsha, AJAX: New Direction in HypersonicTechnology, Paper AIAA-96-4609, 19%.

3. S. V. Bobashev, E. A. D'yakonova, A. V. Erofeev, Proc. Int. Conf. on MHD Power Generation and High Temperature Technology , ·Beijing, PRC,1999, v.II, pp.581-587.

4. Supersonic air-scoop flows of a weakly ionized gas in external electromagnetic field

Cited by 9 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. Shadow method for measuring the average electron density in an ionized gas flow induced by a high-frequency barrier discharge;Journal of Engineering Physics and Thermophysics;2009-03

2. Effect of Magnetohydrodynamics Interaction in Various Parts of Diffuser on Inlet Shocks: Experiment;Journal of Propulsion and Power;2005-09

3. Development and characterization of plasma actuators for high-speed jet control;Experiments in Fluids;2004-08-18

4. Active Control of High Speed Jets Using Localized Arc Filament Plasma Actuators;2nd AIAA Flow Control Conference;2004-06-20

5. Development and Application of Localized Arc Filament Plasma Actuators for Jet Flow and Noise Control;42nd AIAA Aerospace Sciences Meeting and Exhibit;2004-01-05