Please use this identifier to cite or link to this item: http://hdl.handle.net/10397/93018
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dc.contributorDepartment of Mechanical Engineeringen_US
dc.contributorDepartment of Aeronautical and Aviation Engineeringen_US
dc.creatorJiang, Yen_US
dc.creatorWen, CYen_US
dc.creatorZhang, Den_US
dc.date.accessioned2022-05-30T07:40:07Z-
dc.date.available2022-05-30T07:40:07Z-
dc.identifier.issn0001-1452en_US
dc.identifier.urihttp://hdl.handle.net/10397/93018-
dc.language.isoenen_US
dc.publisherAmerican Institute of Aeronautics and Astronauticsen_US
dc.rightsCopyright © 2020 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.en_US
dc.rightsThis is the peer reviewed version of the following article: Jiang, Y., Wen, C. Y., & Zhang, D. (2020). Space–Time Conservation Element and Solution Element Method and Its Applications. AIAA Journal, 58(12), 5408-5430, which has been published in final form at https://doi.org/10.2514/1.J058928.en_US
dc.titleSpace–time conservation element and solution element method and its applicationsen_US
dc.typeJournal/Magazine Articleen_US
dc.identifier.spage5408en_US
dc.identifier.epage5430en_US
dc.identifier.volume58en_US
dc.identifier.issue12en_US
dc.identifier.doi10.2514/1.J058928en_US
dcterms.abstractThis paper reviews the development of the space–time conservation element and solution element (CESE) method and summarizes its applications in various research areas. The CESE method is a special finite-volume-type method that provides an alternative approach to numerical solutions of fluid-dynamic equations and conservation laws in various physical systems. Based on a unified treatment of time and space, this method solves the integral form of the governing equations by discretization of the space–time domain. Recent progress in CESE schemes mainly includes the construction of a family of upwind CESE schemes, the extended definitions of conservation elements and solution elements for arbitrary meshes, and a new approach to developing high-order CESE schemes. Selected applications of the CESE method (including high-speed aerodynamics, multifluid flows, detonations, and aeroacoustics) are presented. Features of the CESE method are described.en_US
dcterms.accessRightsopen accessen_US
dcterms.bibliographicCitationAIAA journal, Dec. 2020, v. 58, no. 12, p. 5408-5430en_US
dcterms.isPartOfAIAA journalen_US
dcterms.issued2020-12-
dc.identifier.scopus2-s2.0-85097645467-
dc.identifier.eissn1533-385Xen_US
dc.description.validate202205 bchyen_US
dc.description.oaAccepted Manuscripten_US
dc.identifier.FolderNumberME-0195-
dc.description.fundingSourceRGCen_US
dc.description.fundingSourceOthersen_US
dc.description.fundingTextNational Natural Science Foundation of Chinaen_US
dc.description.pubStatusPublisheden_US
dc.identifier.OPUS43059292-
dc.description.oaCategoryGreen (AAM)en_US
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