2008
DOI: 10.1002/fld.1868
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A computational study of gas flow in a De‐Laval micronozzle at different throat diameters

Abstract: SUMMARYA numerical study has been carried out to investigate the gas flows in a micronozzle using a continuum model under both slip and no-slip boundary conditions. The governing equations were solved with a finite volume method. The numerical model was validated with available experimental data. Numerical results of exit thrust showed good agreement with experimental data except at very low Reynolds numbers. For parametric studies on the effect of geometric scaling, the nozzle throat diameter was varied from … Show more

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Cited by 10 publications
(6 citation statements)
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“…Compared with thrusters of normal size, fluid flow in the micro-thruster chip shows different characteristics due to its large specific surface area and viscous effect at micro-scale. Although there have been many research papers available in the literature about micro-scale fluid flow in micro-channels [16,17] and micro-nozzles [18,19], few have related flow patterns with thrust performance. In this work, micro-thrust force and specific impulse of a VLM were measured, and the two-phase flow patterns were visualized by high speed camera bonded with a microscope.…”
Section: Introductionmentioning
confidence: 99%
“…Compared with thrusters of normal size, fluid flow in the micro-thruster chip shows different characteristics due to its large specific surface area and viscous effect at micro-scale. Although there have been many research papers available in the literature about micro-scale fluid flow in micro-channels [16,17] and micro-nozzles [18,19], few have related flow patterns with thrust performance. In this work, micro-thrust force and specific impulse of a VLM were measured, and the two-phase flow patterns were visualized by high speed camera bonded with a microscope.…”
Section: Introductionmentioning
confidence: 99%
“…Moreover, an optimized propulsion nozzle for high injection and ejection efficiency would result in superior performance. [17][18][19][20][21][22][23][24][25][26][27][28][29][30] The proposed micro-Ro-boat primarily requires wiring connections for power transmission. In this study, a thin gold wire (25 m diameter) is used for the power connection of the micro-Ro-boat, but it sometimes obstructed the movement because of the very light weight of the micro-Ro-boat and the large pulling force of the wire.…”
Section: Discussionmentioning
confidence: 99%
“…For throat diameters varying from 1.2 to 1.8 mm, a better velocity performance is presented under a throat diameter of 1.2 mm, and it gradually deteriorates as the throat diameter increases. It reported that a decrease in throat diameter helps to improve the gas velocity inside the Laval structure [29,36]. Thus, due to the decrease in the atomizing core acceleration performance of the NTN resulting from the increase in throat diameter, the injection power and atomization energy weaken, which results in a decrease in the droplet velocity.…”
Section: Influence Of the Throat Diametermentioning
confidence: 99%