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.
In-depth study on micro-nozzle flow field performance contributes to optimization design of micro-propulsion system.Under high Knudsen number conditions,a direct simulation Monte-Carlo method was employed for two-dimensional numerical simulation of the flow field within a Laval micro-nozzle at different inlet temperatures.The results show that along with the increase of fluid temperature at the entrance,micro-nozzle thrust would reduce and specific impulse would increase as the adhesive strength increase.Th...
出处
《航空动力学报》
EI
CAS
CSCD
北大核心
2009年第10期2189-2192,共4页
Journal of Aerospace Power
基金
黑龙江省博士后基金(LBH-Z08249)
关键词
微喷管
蒙特卡罗法
尺度效应
附面层
数值模拟
micro-nozzle
Monte-Carlo method
scale effect
boundary layer
numerical simulation