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 language | English |
|---|---|
| Pages (from-to) | 2189-2192 |
| Number of pages | 4 |
| Journal | Hangkong Dongli Xuebao/Journal of Aerospace Power |
| Volume | 24 |
| Issue number | 10 |
| State | Published - Oct 2009 |
| Externally published | Yes |
Keywords
- Boundary layer
- Micro-nozzle
- Monte-Carlo method
- Numerical simulation
- Scale effect
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