Article ID Journal Published Year Pages File Type
10356389 Journal of Computational Physics 2005 43 Pages PDF
Abstract
Through numerous test cases from contact and shock discontinuities, vortex flow, shock wave/boundary-layer interaction to viscous shock tube problems, M-AUSMPW+ proves to be efficient and about twice more accurate than conventional upwind schemes. The three-dimensional implementation of M-AUSMPW+ is expected to provide accuracy and efficiency improvement furthermore.
Related Topics
Physical Sciences and Engineering Computer Science Computer Science Applications
Authors
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