Year: 2001
Author: Taehoon Park, You-Lan Zhu
Journal of Computational Mathematics, Vol. 19 (2001), Iss. 6 : pp. 617–628
Abstract
This paper is devoted to computation of hypersonic flow of air with chemical reactions over concave corners. A technique combining smooth transformation of domain and implicit difference methods is used to overcome numerical difficulties associated with the lack of resolution behind the shock and near the body. The implicit treatment of right hand side terms is also an important part of our method.
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Journal Article Details
Publisher Name: Global Science Press
Language: English
DOI: https://doi.org/2001-JCM-9014
Journal of Computational Mathematics, Vol. 19 (2001), Iss. 6 : pp. 617–628
Published online: 2001-01
AMS Subject Headings:
Copyright: COPYRIGHT: © Global Science Press
Pages: 12
Keywords: Shock fitting Smooth transformation of domain Finite difference method Implicit method.