Volume 24 Issue 10
Oct.  2009
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YANG Hai-wei, ZHU Wei-bing, ZHAO Yang. Micronozzle flow based on simulation of molecule movement[J]. Journal of Aerospace Power, 2009, 24(10): 2189-2192.
Citation: YANG Hai-wei, ZHU Wei-bing, ZHAO Yang. Micronozzle flow based on simulation of molecule movement[J]. Journal of Aerospace Power, 2009, 24(10): 2189-2192.

Micronozzle flow based on simulation of molecule movement

  • Received Date: 2008-04-26
  • Rev Recd Date: 2009-08-10
  • Publish Date: 2009-10-28
  • 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.Three-dimensional numerical simulation of micro-nozzle shows that thrust efficiency would decrease with the declining etching depth,and as the etching depth becomes deeper,the influences of three-dimensional boundary wall would reduce.

     

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