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COMPUTATION OF NONEQUILIBRIUM HYPERSONIC FLOW OVER CONCAVE CORNERS
Taehoon Park and You-lan Zhu
Journal of Computational Mathematics
Vol. 19, No. 6 (NOVEMBER 2001), pp. 617-628
Stable URL: http://www.jstor.org/stable/43692971
Page Count: 12
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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.
Journal of Computational Mathematics © 2001 Institute of Computational Mathematics and Scientific/Engineering Computing