Numerical Simulation of Shock-Wave Interaction with a Laminar Boundary Layer in a Hypersonic Flow around Models with a Kink in the Generatrix

被引:0
|
作者
Surzhikov, S. T. [1 ,2 ]
机构
[1] Russian Acad Sci, Ishlinsky Inst Problems Mech, Moscow 119526, Russia
[2] All Russian Res Inst Automat, Moscow 127030, Russia
关键词
hypersonic flow; interaction of a shock wave with a boundary layer; validation of author's computer code; VALIDATION;
D O I
10.1134/S001546282260122X
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
A series of experimental data obtained at the Calspan-University at Buffalo Research Center (CUBRC) and accompanying numerical calculations performed by members of the computer code testing working group were used to validate the author's PERAT-2D computer code. The problems of a hypersonic flow of molecular nitrogen around a sharp and blunt cone with a kink in the generatrix, as well as around a hollow cylinder with a sharp edge and an expanding skirt, are considered.
引用
收藏
页码:S97 / S116
页数:20
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