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Investigation of Nano Nozzle Flows using Direct Simulation Monte Carlo

نویسنده:
سید علی سعادتی
,
احسان روحی گل خطمی
,
Seyed Ali Saadati
,
Ehsan Roohi
سال
: 2015
چکیده: The aim of the current work is to simulate nanonozzle flows using Simplified Bernoulli-Trials collision algorithm in the dsmcfoamstrath solver of OpenFoam. In this test, the inlet Knudsen number, pressure ratio and wall temperature are about 7.781×10-6, 10 and 300 K, respectively. The phenomenon which we observed in nanonozzles is the prevention of formation of supersonic flows in these scales while this behavior does not happen in micronozzles. The reason can be the boundary layer growth due to scale reduction, so that flow is unable to choke. It leads to produce a lower thrust compared to the larger scales. In addition, temperature gradients are smaller than what we observed in micro nozzles.
یو آر آی: https://libsearch.um.ac.ir:443/fum/handle/fum/3390520
کلیدواژه(گان): DSMC,rarefied flow,nano nozzle
کالکشن :
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    Investigation of Nano Nozzle Flows using Direct Simulation Monte Carlo

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contributor authorسید علی سعادتیen
contributor authorاحسان روحی گل خطمیen
contributor authorSeyed Ali Saadatifa
contributor authorEhsan Roohifa
date accessioned2020-06-06T14:17:42Z
date available2020-06-06T14:17:42Z
date copyright3/8/2015
date issued2015
identifier urihttps://libsearch.um.ac.ir:443/fum/handle/fum/3390520?locale-attribute=fa
description abstractThe aim of the current work is to simulate nanonozzle flows using Simplified Bernoulli-Trials collision algorithm in the dsmcfoamstrath solver of OpenFoam. In this test, the inlet Knudsen number, pressure ratio and wall temperature are about 7.781×10-6, 10 and 300 K, respectively. The phenomenon which we observed in nanonozzles is the prevention of formation of supersonic flows in these scales while this behavior does not happen in micronozzles. The reason can be the boundary layer growth due to scale reduction, so that flow is unable to choke. It leads to produce a lower thrust compared to the larger scales. In addition, temperature gradients are smaller than what we observed in micro nozzles.en
languageEnglish
titleInvestigation of Nano Nozzle Flows using Direct Simulation Monte Carloen
typeConference Paper
contenttypeExternal Fulltext
subject keywordsDSMCen
subject keywordsrarefied flowen
subject keywordsnano nozzleen
identifier linkhttps://profdoc.um.ac.ir/paper-abstract-1046975.html
conference titleAsian Nanoforum conferenceen
conference locationجزیره کیشfa
identifier articleid1046975
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