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Micronozzle flow based on simulation of molecule movement

  • Hai Wei Yang*
  • , Wei Bing Zhu
  • , Yang Zhao
  • *Corresponding author for this work
  • Harbin Engineering University
  • School of Astronautics, Harbin Institute of Technology

Research output: Contribution to journalArticlepeer-review

Abstract

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.

Original languageEnglish
Pages (from-to)2189-2192
Number of pages4
JournalHangkong Dongli Xuebao/Journal of Aerospace Power
Volume24
Issue number10
StatePublished - Oct 2009
Externally publishedYes

Keywords

  • Boundary layer
  • Micro-nozzle
  • Monte-Carlo method
  • Numerical simulation
  • Scale effect

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