Turbulent supersonic flow in the channel with a rearward-facing step

被引：0
|
作者：
Ponyavin, VI [1 ]
机构：
[1] Kazan State Technol Univ, Kazan, Russia
来源：
IZVESTIYA VYSSHIKH UCHEBNYKH ZAVEDENII AVIATSIONAYA TEKHNIKA | 2002年 / 04期
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D O I：
暂无
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
We present the results of the numerical calculation (by the finite-element method) of a turbulent supersonic flow in the channel with a rearward-facing step. The k - omega model with near-wall functions is used as a turbulence model. The calculation results are compared with the experimental data.
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页码：37 / 39
页数：3
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