Experiment Investigation of Plasma Plume Deflection with MHD

摘要：

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.

关键词： component Plasma,MHD Aero-engine Ionization Plume Deflection

作者: SUN Baigang LI Feng YANG Hui LIU Yongbo LIU Xiangbin LIN Jiuhui

作者单位: School of Jet Propulsion ,dept name of organization Beijing University of Aeronautics and Astronauti the 1st Flying Academy of Airforce, Harbin, China Aviation University of Air Force, Changchun, China

会议类型: 国际会议

会议名称: 2011 International Conference on Electronics and Optoelectronics(2011电子学与光电子学国际会议 ICEOE 2011)

会议地点: 大连

会议语种:英文

页码: 142-145

在线出版日期: 2011-07-29（万方平台首次上网日期，不代表论文的发表时间）