期刊文献+

氩工质连续激光加热推力器的数值仿真

Numerical simulation of a continuous wave laser powered thruster with argon propellant
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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 equations consistent)算法求解.对解算出的流场压力和黏性应力积分获得推力,其值与类似构型推力器的实验结果吻合较好.在不同流量条件下对推力器的流场进行了计算,通过分析其特征,提出了改进推力器性能的思路. 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.The thrust was computed by integrating the pressure and viscosity stress all over the wall,and the value was consistent with the experimental result of a similar configuration.Then the characteristics of the filed of a thruster under different mass flow rates were analyzed,and the methods for performance improvement were presented.
出处 《航空动力学报》 EI CAS CSCD 北大核心 2011年第1期217-222,共6页 Journal of Aerospace Power
基金 国家部委基金
关键词 激光推进 连续波 氩等离子体 推力器 数值仿真 laser propulsion continuous wave argon plasma thruster numerical simulation
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  • 1Black J W,Krier H,Zerkle D,et al. Characterization of la- ser sustained plasma behavior during 10 kW laser thruster tests[R]. AIAA 92-3022,1992.
  • 2Uehara S, Inoue T, Komurasaki K, et al. An experimental study on energy conversion process of an in-space CW la- ser thruster[C]//Proceedings of Third International Sym- posium on Beamed Energy Propulsion. Melville:American Institute of Physics, 2005 : 254-264.
  • 3Rachuk V S,Guterman V Y,Ivanov A V. Experimental in- vestigations of laser propulsion by using gas-dynamic laser [C] // Proceedings of Fourth International Symposium on Beamed Energy Propulsion. Melville: American Institute of Physics, 2006 : 48 -57.
  • 4Glumb R J, Krier H. Two-dimensinal model of laser-sus- tained plasmas in axisymmetric flowfileds[J]. AIAA Jour- nal,1986,24(8) :1331-1336.
  • 5Jeng S M,Keefer D R,Welle R,et al. Numerical study of laser-sustained argon plasmas in a forced convective flow [R]. AIAA 86-1078,1986.
  • 6Morales P M, Toyoda K, Komurasaki K, et al. CFD simu- lation of a 2 kW class laser thruster[R]. AIAA 2001-0650, 2001.
  • 7郑力铭,朱定强,徐旭,蔡国飙.激光推进火箭发动机吸收室的数值模拟[J].推进技术,2002,23(5):387-390. 被引量:4
  • 8王海兴,陈熙.激光推进的初步数值模拟研究[J].工程热物理学报,2004,25(S1):83-86. 被引量:4
  • 9Kruger C H. Nonequilibrium effects in thermal plasma chemistry[J]. Plasma Chemistry and Plasma Processing, 1989,9 (4) : 435-443.
  • 10Raizer Y P, Tybulewicz A. Laser induced discharge phe- nomena[ M]. New York:Plenum Publishing Corporation, 1977.

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