2017
DOI: 10.1080/10407782.2017.1330091
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Simulation of a temperature drop for the flow of rarefied gases in microchannels

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Cited by 15 publications
(12 citation statements)
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“…Close to the channel outlet (x/L > 0.9), the gas temperature drops, which is attributed to the rapid gas expansion in that region, which is known as the expansion cooling phenomenon [20,65]. A similar behaviour close to the channel outlet has been reported by others [28,37,[43][44][45] for Poiseuille micro-flows in microchannels with uniform cross-sections. The overall heat flow direction for the problem considered in the present work is determined by both the thermal and pressure gradients in the microchannel [66].…”
Section: Resultssupporting
confidence: 72%
See 1 more Smart Citation
“…Close to the channel outlet (x/L > 0.9), the gas temperature drops, which is attributed to the rapid gas expansion in that region, which is known as the expansion cooling phenomenon [20,65]. A similar behaviour close to the channel outlet has been reported by others [28,37,[43][44][45] for Poiseuille micro-flows in microchannels with uniform cross-sections. The overall heat flow direction for the problem considered in the present work is determined by both the thermal and pressure gradients in the microchannel [66].…”
Section: Resultssupporting
confidence: 72%
“…Despite the extensive interest in studying fluid flow at the micro-and nanoscales, numerical investigations of gas flow under nonequilibrium conditions are deficient in thermal analyses. Previous studies on thermal field analysis in microfluidics systems are mostly limited to the channels with uniform cross-sections (see, for instance, [37,[41][42][43][44][45][46][47][48]). Therefore, there is an indispensable need for detailed investigations on heat and fluid flow at the micro-and nanoscales under nonequilibrium conditions.…”
Section: Introductionmentioning
confidence: 99%
“…The centre-line pressure distribution is compared with the analytical solution of non-linear pressure distribution reported by Arkilic et al [20]. The present predictions are also compared with the DSMC data of compressible flow provided by Gavasane et al [25] on Argon gas for Kn = 0.124 at channel outlet, as illustrated in Fig. 2a.…”
Section: Validation Of Results With Analytical Solution and Dsmc Datamentioning
confidence: 76%
“…One of the middle Fig. 2 A comparison between variations of a centre-line pressure distribution along streamwise direction obtained in present simulation with analytical solution of Arkilic et al [20] and DSMC data of Gavasane et al [25], b centre-line velocities along streamwise direction, c centre-line static temperature distribution along streamwise direction, d slip velocity adjacent to the wall along streamwise direction, e cross-streamwise velocity profile obtained at half length of the channel, obtained in simulation, DSMC data [25], analytical solution of Karniadakis et al [26] for first and second-order slip boundary conditions ◂ Table 2 Validation of fRe for straight microchannel (α = 0.5) with analytical solution of Morini et al [27] The value in bold indicates the Kn value where minimum deviation is obtained with respect to the analytical solution Exit Kn (x/L = 1)…”
Section: Effect Of Reynolds Number On the Flow Characteristics Insidementioning
confidence: 74%
“…Translational kinetic temperature The translational kinetic temperature is the unknown parameter to define the main parameters related to the thruster performance. During a gas expansion into a very low pressure environment there is a gas temperature drop [19][20][21]. Using the conservation of energy and the equipartition principle we can analyse the energy throughout the microchannel.…”
Section: Exhaust Velocitymentioning
confidence: 99%