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基于分子运动模拟的微喷管流体流动
引用本文:杨海威,朱卫兵,赵阳.基于分子运动模拟的微喷管流体流动[J].航空动力学报,2009,24(10):2189-2192.
作者姓名:杨海威  朱卫兵  赵阳
作者单位:1.哈尔滨工程大学航天与建筑工程学院航天工程系, 哈尔滨 150001
基金项目:黑龙江省博士后启动基金 
摘    要:深入研究微喷管内流场性能有助于微推进系统的优化设计.在高克努森数条件下,运用直接模拟蒙特卡罗方法模拟微喷管流动过程,对不同入口温度下的拉伐尔喷管流场进行二维数值模拟,模拟结果表明随着入口流体温度的升高,由于黏性力的增强,微喷管的推力减小而比冲增大.对微喷管的三维数值模拟表明,推力效率随着喷管蚀刻深度的减少而降低,微喷管蚀刻深度的增加将使三维壁面边界的影响降低. 

关 键 词:微喷管    蒙特卡罗法    尺度效应    附面层    数值模拟
收稿时间:2008/4/26 0:00:00
修稿时间:2009/8/10 0:00:00

Micronozzle flow based on simulation of molecule movement
YANG Hai-wei,ZHU Wei-bing and ZHAO Yang.Micronozzle flow based on simulation of molecule movement[J].Journal of Aerospace Power,2009,24(10):2189-2192.
Authors:YANG Hai-wei  ZHU Wei-bing and ZHAO Yang
Institution:1.Department of Aerospace Engineering, College of Aerospace and Civil Engineering, Harbin Engineering University, Harbin 150001, China2.Department of Aerospace Engineering, School of Astronautics, Harbin Institute of Technology, Harbin 150001, China
Abstract:Study on micro-nozzle flow field performance contributes to the optimization design of micro-propulsion system. In high Knudsen number conditions, a Direct Simulation Monte Carlo method was employed in two-dimensional numerical simulation of the flow field within a Laval micro-nozzle under different inlet temperatures, results show that along with the increase of fluid temperature at the entrance, as the adhesive strength increase, micro-nozzle thrust would reduce and specific impulse would increase. Three-dimensional numerical simulation of micro-nozzle shows that thrust efficiency decrease along with the etching depth and as it etching deeper, influences of the 3-dimensional boundary wall will reduce.
Keywords:Micro Nozzle  Monte-Carlo method  Scale effect  Boundary layer  Numerical Simulation
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