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Volume 19, Issue 6
Computation of Nonequilibrium Hypersonic Flow over Concave Corners

Taehoon Park & You-Lan Zhu

J. Comp. Math., 19 (2001), pp. 617-628.

Published online: 2001-12

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  • 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.

  • Keywords

Shock fitting, Smooth transformation of domain, Finite difference method, Implicit method.

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COPYRIGHT: © Global Science Press

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@Article{JCM-19-617, author = {Park , Taehoon and Zhu , You-Lan}, title = {Computation of Nonequilibrium Hypersonic Flow over Concave Corners}, journal = {Journal of Computational Mathematics}, year = {2001}, volume = {19}, number = {6}, pages = {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.

}, issn = {1991-7139}, doi = {https://doi.org/}, url = {http://global-sci.org/intro/article_detail/jcm/9014.html} }
TY - JOUR T1 - Computation of Nonequilibrium Hypersonic Flow over Concave Corners AU - Park , Taehoon AU - Zhu , You-Lan JO - Journal of Computational Mathematics VL - 6 SP - 617 EP - 628 PY - 2001 DA - 2001/12 SN - 19 DO - http://doi.org/ UR - https://global-sci.org/intro/article_detail/jcm/9014.html KW - Shock fitting, Smooth transformation of domain, Finite difference method, Implicit method. AB -

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.

Park , Taehoon and Zhu , You-Lan. (2001). Computation of Nonequilibrium Hypersonic Flow over Concave Corners. Journal of Computational Mathematics. 19 (6). 617-628. doi:
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