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dc.contributor.authorTseng, K. C.en_US
dc.contributor.authorCave, H. M.en_US
dc.contributor.authorKuo, T. C.en_US
dc.contributor.authorJermy, M. C.en_US
dc.contributor.authorKrumdieck, S. P.en_US
dc.contributor.authorWu, J. S.en_US
dc.date.accessioned2017-04-21T06:49:35Z-
dc.date.available2017-04-21T06:49:35Z-
dc.date.issued2009en_US
dc.identifier.isbn978-0-7354-0615-5en_US
dc.identifier.issn0094-243Xen_US
dc.identifier.urihttp://hdl.handle.net/11536/135015-
dc.description.abstractA method of transient adaptive sub-cells (TAS) suitable for unstructured grids in Direct Simulation Monte Carlo (DSMC) simulations is introduced. The TAS algorithm is implemented within the frame work of a parallelized DSMC code (PDSC). Benchmarking tests are conducted for driven cavity (low, hypersonic flow over a two-dimensional cylinder and the unsteady vortex shedding behind a two-dimensional cylinder. The use of TAS enabled a reduction in the computational expense of the simulation since larger sampling cells and less simulation particles could be employed. Furthermore, the collision quality of the simulation was maintained or improved and the preservation of property gradients and vorticity at the scale of the sub-cells enabled correct unsteady vortex shedding frequencies to be predicted. The use of TAS in a parallel DSMC code allows simulations of unsteady processes at a near continuum level to be carried out efficiently, accurately and with acceptable computational times.en_US
dc.language.isoen_USen_US
dc.subjectDSMCen_US
dc.subjectunsteadyen_US
dc.subjectvortex sheddingen_US
dc.subjectdriven cavity flowen_US
dc.subjecthypersonicen_US
dc.titleImplementation of the Transient Adaptive Sub-Cell Module for the Parallel DSMC Codeen_US
dc.typeProceedings Paperen_US
dc.identifier.journalRAREFIED GAS DYNAMICSen_US
dc.citation.volume1084en_US
dc.citation.spage287en_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:000265564800046en_US
dc.citation.woscount0en_US
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