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常气压辉光放电等离子体对边界层流动的影响
引用本文:毛枚良,邓小刚,陈亮中,陈坚强.常气压辉光放电等离子体对边界层流动的影响[J].计算物理,2009,26(1).
作者姓名:毛枚良  邓小刚  陈亮中  陈坚强
作者单位:中国空气动力研究与发展中心,四川,绵阳,621000
基金项目:国家创新研究群体科学基金,国家自然科学基金 
摘    要:基于Shyy提出的常气压下均匀辉光放电等离子体与空气干扰的物理模型,通过求解电位势方程得到电场分布及作用于流体上的电场力.以NACA0015翼型低速绕流为对象,通过数值求解考虑等离子体作用的流体运动控制方程,研究等离子体位置和个数控制对翼型绕流分离的影响.位于分离点上游的等离子体能够有效地抑制流动分离,而在分离区的等离子体对流动影响很弱,这一结论同实验观察一致,并给出等离子体对翼型壁面压力和气动力影响的规律.

关 键 词:NACA0015翼型  低速流动控制  等离子体  数值模拟

Boundary Layer Flows with One Atmosphere Uniform Glow Discharge Plasma
MAO Meiliang,DENG Xiaogang,CHEN Liangzhong,CHEN Jianqiang.Boundary Layer Flows with One Atmosphere Uniform Glow Discharge Plasma[J].Chinese Journal of Computational Physics,2009,26(1).
Authors:MAO Meiliang  DENG Xiaogang  CHEN Liangzhong  CHEN Jianqiang
Institution:China Aerodynamic Research and Development Center;Mianyang 621000;China
Abstract:In a model for interaction between one atmosphere uniform glow discharge plasma(OAUGDP)and air proposed by Shyy,electric field and electric forces acting on air as body force are obtained.The electric field is calculated with electric potential equation. The influence of OAUGDP on flows around a NACA0015 airfoil at low speed is investigated by solving N-S equation with a body force term.Plasma located upstream of the separation point damps the flow separation around the airfoil efficiently,while plasma loca...
Keywords:NACA0015 airfoil  low speed flow control  plasma  numerical simulation  
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