辉光放电等离子体对边界层流动控制的机理研究  

Numerical study for the influence of high-pressure glow discharged-induced plasma on the flow of boundary region

作　　者：毛枚良[1] 邓小刚[1] 向大平[1] 陈坚强[1] 

机构地区：[1]中国空气动力研究与发展中心,四川绵阳621000

出　　处：《空气动力学学报》2006年第3期269-274,共6页Acta Aerodynamica Sinica

基　　金：中国自然科学基金创新研究群体科学基金资助项目(10321002);中国自然科学基金国家杰出青年科学基金(No.10225208)

摘　　要：本文求解电位势方程得到电场分布,假定电场强度大于击穿阈值的区域为等离子体区,给定电荷密度,得到了作用于流体上的电场力。通过求解带源项的NS方程,研究了一个大气压下的均匀辉光放电等离子体对边界层流动的影响,考察了电场力做功对流动的影响。本文研究结果同文献[6]一致,即电场力总体上使边界层流动加速。另外,电场力做功对流动参数的影响可以忽略。文献[6]给出的线化电场模型和本文得到的电场相比,具有较大的差别,该差别引起了流动参数显著差别。In this paper, the electric field distribution is obtained by solving the electric potential equation. The electric field forces acting on the fluid through one atmosphere uniform glow discharge plasma（OAUGDP） are obtained by such an assumption that the plasma region is where the electric field intensity is more than the breakdown threshhold, and the charge density is constant. The influences of OAUGDP on the boundary layer flow are studied and the effect of the work done by the electric field forces is investigated by solving the NS equation with source term. The results agree with those in literature [6] generally. The electric field forces can accelerate the fluid in the boundary. The influences of the work done by electric field forces on the flow parameter are trivial. The large computed electric fields given by simplified model in literature [6] are greatly different from those by solving the electric potential equation, which cause the great difference of the flow parameters, such as pressure and velocity.

关 键 词：等离子体 流动控制 电场 数值模拟 

分 类 号：V211.3[航空宇航科学与技术—航空宇航推进理论与工程]