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Cited 4 time in webofscience Cited 4 time in scopus
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Three-Dimensional Building-Cube Method for Inviscid Compressible Flow Computations

Authors
Kim, Lae-SungNakahashi, KazuhiroXu, Zhe-ZhuXiao, HongLyu, Sung-Ki
Issue Date
Dec-2015
Publisher
KOREAN SOC PRECISION ENG
Keywords
Building-Cube method; Three-dimensional inviscid compressible flows; Cartesian mesh; Parallel computation
Citation
INTERNATIONAL JOURNAL OF PRECISION ENGINEERING AND MANUFACTURING, v.16, no.13, pp 2673 - 2681
Pages
9
Indexed
SCIE
SCOPUS
KCI
Journal Title
INTERNATIONAL JOURNAL OF PRECISION ENGINEERING AND MANUFACTURING
Volume
16
Number
13
Start Page
2673
End Page
2681
URI
https://scholarworks.gnu.ac.kr/handle/sw.gnu/16886
DOI
10.1007/s12541-015-0342-4
ISSN
2234-7593
2005-4602
Abstract
In this study, the Building-Cube method (BCM) devised for calculating large-scale flows and getting rid of the grid dependencies of computational results is extended to perform 3D inviscid compressible fluid flow simulations. The proposed scheme divides a computational domain into a large number of cubes with different sizes, and each individual cube is a sub-flow field simulated with a Cartesian grid of uniform spacing and an equal number of cells and nodes. Through the proposed scheme, we determine the geometric size of individual cube by Adapting the flow characteristics and geometrical shapes using an adaptively refining Cartesian grid approaches. The uniform spacing and equal number of cells and nodes in the Cartesian grid of individual cubes ensure a good performance for parallel computations; large result data can be handled efficiently. Further, an algorithm to solve the inviscid flow equations on the Building-Cube mesh for three-dimensional (3D) geometries is presented. The validation and performance of the proposed 3D BCM are demonstrated through comparisons of the computed results with the experimental data for the ONERA M6 wing and ONERA M5 wing-fuselage configurations.
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