Abstract
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 × 102.
Original language | English (US) |
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Pages (from-to) | 897-904 |
Number of pages | 8 |
Journal | AIAA journal |
Volume | 40 |
Issue number | 5 |
DOIs | |
State | Published - May 2002 |
Externally published | Yes |
ASJC Scopus subject areas
- Aerospace Engineering