@inproceedings{320c5af5e6fa446caee4814f8d779329,
title = "Numerical investigation of plasma plume deflection with MHD control",
abstract = "At present, NASA is engaged in research to develop Plasma flow control technology on aeronautic and astronautic scopes. This article presents a compositive MHD(magnetohydrodynamics) method to control high-velocity Plasma flow 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. By analyzing and applying the MHD mathematical model, the author performs the numerical simulation of plasma flows-field with the MHD condition,shows that the jet plume in plasma state can deflect with MHD.",
keywords = "Aero-engine, Ionization degree, MHD, Plasma, Plume deflection",
author = "Sun Baigang and Yang Hui and Liu Yongbo and Liu Xiangbin and Li Feng and Wang Jingyu and Mu Yandong",
year = "2012",
doi = "10.4028/www.scientific.net/AMR.588-589.1372",
language = "英语",
isbn = "9783037855287",
series = "Advanced Materials Research",
pages = "1372--1375",
booktitle = "Advances in Mechanics Engineering",
note = "2012 International Conference on Advances in Mechanics Engineering, ICAME 2012 ; Conference date: 03-08-2012 Through 05-08-2012",
}