2019
DOI: 10.1063/1.5083807
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Numerical study of species separation in rarefied gas mixture flow through micronozzles using DSMC

Abstract: This work investigates the species separation in the rarefied flow of the argon-helium mixture through convergent-divergent micronozzles. Imposing a molecular mass ratio in the order of 10, the flow of this mixture can lead to the formation of serious nonhomogeneous phenomena such as the species separation. This study is performed in the ranges of 2.0–4.0 for the geometrical expansion ratio, 200–400 K for the wall temperature, and 0.003–1.454 for the inlet Knudsen number. The effects of these parameters are ex… Show more

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Cited by 33 publications
(12 citation statements)
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“…It should be noticed that the nozzle flow behavior in the considered conditions deviates from the classical one, as described by inviscid theory. Although the inlet pressure is high enough to avoid rarefaction effects, viscous forces are very pronounced (the nozzle throat Reynold's number is about 300) and delay the supersonic transition within the divergent section whose effective area is strongly reduced by a thick boundary layer [17]. So far, the best nozzle configuration consists of a simple double cone geometry with an inlet diameter of 220 μm, a 60 μm throat diameter and a 90 μm exit diameter, whose size is the largest as possible which preserves the guiding characteristics of the hollow waveguide.…”
Section: Resultsmentioning
confidence: 99%
“…It should be noticed that the nozzle flow behavior in the considered conditions deviates from the classical one, as described by inviscid theory. Although the inlet pressure is high enough to avoid rarefaction effects, viscous forces are very pronounced (the nozzle throat Reynold's number is about 300) and delay the supersonic transition within the divergent section whose effective area is strongly reduced by a thick boundary layer [17]. So far, the best nozzle configuration consists of a simple double cone geometry with an inlet diameter of 220 μm, a 60 μm throat diameter and a 90 μm exit diameter, whose size is the largest as possible which preserves the guiding characteristics of the hollow waveguide.…”
Section: Resultsmentioning
confidence: 99%
“…It should be noticed that the nozzle flow behavior in the considered conditions deviates from the classical one, as described by the inviscid theory. Although the inlet pressure is high enough to avoid rarefaction effects, viscous forces are very pronounced (the nozzle throat Reynold's number is about 300) and delay the supersonic transition within the divergent section whose effective area is strongly reduced by a thick boundary layer [18]. So far, the best nozzle configuration consists of a simple double cone geometry with an inlet diameter of 220 µm, a 60 µm throat diameter, and a 90 µm exit diameter, whose size is the largest as possible which preserves the guiding characteristics of the hollow waveguide.…”
Section: Discussionmentioning
confidence: 99%
“…The multi-scale mechanism from the continuum flow to the rarefied flow (or from the macroscopic flow to the microscopic flow) is crucial for the force and heat loaded on nearspace and reentry vehicles, the control of spacecraft by thrusters 1,2 , the propelling and cooling of Micro-Electro-Mechanical System (MEMS) 3,4 , etc. Since the continuum flow and rarefied flow often exist simultaneously in a singe multi-scale flow field, the modeling and prediction become complicated: The continuum flow is governed by the Navier-Stokes (N-S) equation, and the rarefied flow is governed by the Boltzmann equation, while there is no multi-scale governing equation for the transitional flow between continuum and rarefied ones.…”
Section: Introductionmentioning
confidence: 99%