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氩工质连续激光加热推力器的数值仿真
引用本文:李小康,张育林,程谋森,鄢昌渝.氩工质连续激光加热推力器的数值仿真[J].航空动力学报,2011,26(1):217-222.
作者姓名:李小康  张育林  程谋森  鄢昌渝
作者单位:国防科学技术大学航天与材料工程学院,长沙,410073
摘    要:对氩气工质的连续激光推力器内加热与流动过程进行数值模拟,建立了包含激光吸收、化学反应、高温效应、黏性、扩散、热传导以及辐射效应等物理机制的模型.推力室内二维轴对称流场采用可压缩Navier-Stokes方程描述,用SIMPLEC(semi-implicit method for pressure-linked equa...

关 键 词:激光推进  连续波  氩等离子体  推力器  数值仿真
收稿时间:2009/11/20 0:00:00
修稿时间:2/5/2010 4:55:56 PM

Numerical simulation of a continuous wave laser powered thruster with argon propellant
LI Xiao-kang,ZHANG Yu-lin,CHENG Mou-sen and YAN Chang-yu.Numerical simulation of a continuous wave laser powered thruster with argon propellant[J].Journal of Aerospace Power,2011,26(1):217-222.
Authors:LI Xiao-kang  ZHANG Yu-lin  CHENG Mou-sen and YAN Chang-yu
Institution:LI Xiao-kang,ZHANG Yu-lin,CHENG Mou-sen,YAN Chang-yu(College of Aerospace and Materials Engineering,National University of Defense Technology,Changsha 410073,China)
Abstract:The heating and flow process in a continuous wave laser powered thruster using argon as propellant was modeled numerically.A model of physical mechanisms including laser absorption,chemical reaction,high-temperature thermodynamics properties,viscosity,diffusion,heat conduction and the effect of radiation was built up.The two-dimensional axisymmetric flow filed described by Navier-Stokes equations was solved by pressure-based SIMPLEC(semi-implicit method for pressure-linked equations consistent) algorithm.Th...
Keywords:laser propulsion  continuous wave  argon plasma  thruster  numerical simulation  
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