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Title: Space–time conservation element and solution element method and its applications
Authors: Jiang, Y 
Wen, CY 
Zhang, D
Issue Date: Dec-2020
Source: AIAA journal, Dec. 2020, v. 58, no. 12, p. 5408-5430
Abstract: This 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.
Publisher: American Institute of Aeronautics and Astronautics
Journal: AIAA journal 
ISSN: 0001-1452
EISSN: 1533-385X
DOI: 10.2514/1.J058928
Rights: Copyright © 2020 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.
This 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.
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