Numerical modeling of axisymmetric and three-dimensional flows in microelectromechanical systems nozzles

被引:63
作者
Alexeenko, AA [1 ]
Levin, DA
Gimelshein, SF
Collins, RJ
Reed, BD
机构
[1] Penn State Univ, Dept Aerosp Engn, University Pk, PA 16802 USA
[2] George Washington Univ, Dept Chem, Washington, DC 20052 USA
[3] Univ Minnesota, Dept Elect Engn, Minneapolis, MN 55455 USA
[4] NASA, John H Glenn Res Ctr, On Board Propuls Branch, Cleveland, OH 44125 USA
关键词
D O I
10.2514/2.1726
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A numerical study of three-dimensional effects on the performance of a micronozzle fabricated from flat silicon wafers is performed by use of both continuum and kinetic approaches: The nozzle operates in a low-Reynolds-number regime, and viscous effects dominate the gas expansion. Thrust losses occur because the shear on the wall is greater in a flat nozzle configuration than in an axisymmetric conical nozzle. Therefore, the prediction of the micronozzle performance based on axisymmetric or two-dimensional modeling can lead to significant design errors. Comparison of simulation with recent data shows good agreement in terms of thrust predictions for cold-gas thrusters at Reynolds numbers of approximately 2 x 10(2).
引用
收藏
页码:897 / 904
页数:8
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