DocumentCode
3207853
Title
Experiment investigation of plasma plume deflection with MHD
Author
Sun Baigang ; Li Feng ; Yang Hui ; Liu Yongbo ; Liu Xiangbin ; Lin Jiuhui
Author_Institution
Dept. Name of Organ., Beijing Univ. of Aeronaut. & Astronaut., Beijing, China
Volume
1
fYear
2011
fDate
29-31 July 2011
Abstract
This article presents a compositive MHD method to control high-velocity Plasma flows generate by alkali salts in combustion gas, demonstrates that MHD system can make the jet plume to deflect, and realizes the aeroengine thrust-vector purpose. Bases on analyzing and applying the MHD mathematical model, establish the MHD experiment system of plasma control, under the specific condition of experiment, with the analysis of physical-chemistry, puts some metal salt compound of low ionization energy into the combustion gas, gets the low temperature plasma flows, effectively realizes the MHD control of plasma jet plume deflection and thrust-vector, researches the ionization characteristic of the metal salt and combustion gas.
Keywords
aerospace control; aerospace engines; aerospace propulsion; combustion; ionisation; plasma jets; plasma magnetohydrodynamics; plasma simulation; MHD control; MHD mathematical model; MHD system; aeroengine thrust-vector; alkali salts; combustion gas; compositive MHD method; high-velocity plasma flows; ionization characteristic; ionization energy; low temperature plasma flows; metal salt compound; physical-chemistry analysis; plasma control; plasma jet plume deflection; Conductors; Electromagnetics; Equations; Ionization; Magnetic properties; Magnetohydrodynamics; Sun; Aero-engine; Ionization; MHD; Plasma; Plume Deflection;
fLanguage
English
Publisher
ieee
Conference_Titel
Electronics and Optoelectronics (ICEOE), 2011 International Conference on
Conference_Location
Dalian, Liaoning
Print_ISBN
978-1-61284-275-2
Type
conf
DOI
10.1109/ICEOE.2011.6013067
Filename
6013067
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