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Atomistic simulation of micro‐scale adiabatic piston problem

cris.virtual.department#PLACEHOLDER_PARENT_METADATA_VALUE#
cris.virtual.department#PLACEHOLDER_PARENT_METADATA_VALUE#
cris.virtual.orcid#PLACEHOLDER_PARENT_METADATA_VALUE#
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cris.virtualsource.department3fade673-6db4-4e4b-a77c-0b1e7e3b5f6e
cris.virtualsource.department45885ceb-114e-412b-b4eb-b74225b17074
cris.virtualsource.orcid3fade673-6db4-4e4b-a77c-0b1e7e3b5f6e
cris.virtualsource.orcid45885ceb-114e-412b-b4eb-b74225b17074
dc.contributor.authorNevsan Sengil
dc.contributor.authorFirat Oguz Edis
dc.date.accessioned2024-07-09T07:57:50Z
dc.date.available2024-07-09T07:57:50Z
dc.date.issued2009-10-16
dc.description.abstract<jats:sec><jats:title content-type="abstract-heading">Purpose</jats:title><jats:p>The purpose of this paper is to demonstrate the utilization of the direct simulation Monte Carlo (DSMC) method for moving‐boundary/deforming‐domain micro‐scale gas flow problems. Furthermore, a hydrodynamic model, proposed in the literature, is used to compare its results with those obtained using the DSMC method.</jats:p></jats:sec><jats:sec><jats:title content-type="abstract-heading">Design/methodology/approach</jats:title><jats:p>A micro‐scale adiabatic piston problem is analyzed using a parallel DSMC implementation for deforming domains. Initially, pressures at both sides of the piston wall are different. Consequently, frictionless piston moves toward low‐pressure compartment, keeps oscillating from one side to the other. Eventually, the piston reaches the “Mechanical equilibrium” state. Although the temperatures are different, pressures are equal at this state. The unsteady problem is analyzed until it reaches this state. Three test cases, all with the same initial conditions but different piston masses are analyzed. The time variation of the piston position, conditions in the compartments separated by the piston, are presented and compared with the results obtained from a hydrodynamic model proposed in the literature.</jats:p></jats:sec><jats:sec><jats:title content-type="abstract-heading">Findings</jats:title><jats:p>The results show that the DSMC and hydrodynamic results agree for the case where the piston mass is much larger than the mass of the gas inside the cylinder. But for other two cases, where the piston mass is smaller, piston motion, and conditions in the compartments separated by the piston differ for the two methods. This is attributed to the linear velocity distribution assumption of the hydrodynamic model. The DSMC results demonstrate that this assumption is not valid for cases where the piston mass is equal or less than the mass of the gas inside the cylinder.</jats:p></jats:sec><jats:sec><jats:title content-type="abstract-heading">Originality/value</jats:title><jats:p>Implementation of the DSMC method for problems with deforming domain is presented and a limitation for applicability of hydrodynamic model for these problems is shown.</jats:p></jats:sec>
dc.identifier.doi10.1108/00022660910997793
dc.identifier.urihttps://acikarsiv.thk.edu.tr/handle/123456789/1497
dc.publisherEmerald
dc.relation.ispartofAircraft Engineering and Aerospace Technology
dc.relation.issn0002-2667
dc.titleAtomistic simulation of micro‐scale adiabatic piston problem
dc.typejournal-article
dspace.entity.typePublication
oaire.citation.issue6
oaire.citation.volume81

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