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dc.contributor.authorLian, Y-Y.en_US
dc.contributor.authorTseng, K-C.en_US
dc.contributor.authorChen, Y. -S.en_US
dc.contributor.authorWu, M. -Z.en_US
dc.contributor.authorWu, J. -S.en_US
dc.contributor.authorCheng, Garyen_US
dc.date.accessioned2017-04-21T06:49:36Z-
dc.date.available2017-04-21T06:49:36Z-
dc.date.issued2009en_US
dc.identifier.isbn978-0-7354-0615-5en_US
dc.identifier.issn0094-243Xen_US
dc.identifier.urihttp://hdl.handle.net/11536/135017-
dc.description.abstractAn improved parallelized hybrid DSMC-NS algorithm presented and verified. In previous work [11, it showed the slow convergence of coupling between two numerical solvers if the normal velocities across the breakdown interfaces are very low. By detailed kinetic velocity sampling study from the pure DSMC simulation of a two-dimensional supersonic nitrogen flow (M-infinity=4) past a 25 finite wedge, we have found most of boundary layer region is in nearly thermal equilibrium, even with very high continuum breakdown Kn(max)[10]. Thus, a new continuum breakdown parameter based on pressure gradient, pressure and local mean free path, which can be used to effectively "exclude" the "false" breakdown region like the boundary layer, is proposed in this paper. Results show that the improved algorithm can greatly reduce the computational cost while maintaining essentially the same accuracy.en_US
dc.language.isoen_USen_US
dc.subjectcontinuum breakdown parameteren_US
dc.subjectdirect simulation Monte Carlo (DSMC)en_US
dc.subjecthybrid DSMC-NS algorithmen_US
dc.titleAn Improved Parallelized Hybrid DSMC-NS Algorithmen_US
dc.typeProceedings Paperen_US
dc.identifier.journalRAREFIED GAS DYNAMICSen_US
dc.citation.volume1084en_US
dc.citation.spage341en_US
dc.citation.epage+en_US
dc.contributor.department機械工程學系zh_TW
dc.contributor.departmentDepartment of Mechanical Engineeringen_US
dc.identifier.wosnumberWOS:000265564800055en_US
dc.citation.woscount0en_US
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