高超声速绕流模型中激波与层流边界层相互作用的数值模拟

S. Surzhikov
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引用次数: 1

摘要

利用Calspan-UB研究中心(CUBRC)获得的一系列实验数据,以及测试计算机代码工作组参与者进行的相关数值计算,对作者的计算机代码PERAT-2D进行验证。研究了分子氮在带弯折的尖锥和钝锥上的高超声速流动问题,以及在带尖边和膨胀裙边的空心圆筒上的高超声速流动问题。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Numerical modeling of shock-wave interaction with a laminar boundary layer during hypersonic flow around models with a kink
A series of experimental data obtained at the Calspan-UB Research Center (CUBRC), and related numerical calculations performed by participants of the working group of testing computer codes, were used to validate the author's computer code PERAT-2D. The problems of flowing by hypersonic flows of molecular nitrogen of a sharp and blunt cone with a kink are considered, as well as the problem of flowing around a hollow cylinder with a sharp edge and an expanding skirt.
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