COMPUTATION OF NONEQUILIBRIUM HYPERSONIC FLOW OVER CONCAVE CORNERS  

作　　者：Taehoon Park You-lan Zhu 

出　　处：《Journal of Computational Mathematics》2001年第6期617-628,共12页计算数学（英文）

基　　金：This work was partially supported by the North Carolina Supercomputing Center.

摘　　要：Discusses a technique for the computation of hypersonic flow of air with chemical reactions over concave corners. Details of smooth transformation of domain; Use of finite difference method; Numerical results.Discusses a technique for the computation of hypersonic flow of air with chemical reactions over concave corners. Details of smooth transformation of domain; Use of finite difference method; Numerical results.

关 键 词：Shock fitting Smooth transformation of domain Finite difference method Implicit method. 

分 类 号：O351[理学—流体力学]