A Turbulent Boundary Layer on a Permeable Plate in a Supersonic Flow with a Positive Pressure Gradient under Foreign Gas Injection

IF 0.6 4区 物理与天体物理 Q4 MECHANICS
A. I. Leontiev, V. G. Lushchik, M. S. Makarova
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引用次数: 0

Abstract

A numerical simulation of a turbulent boundary layer on a permeable plate with helium injection into a supersonic xenon flow in the presence of a positive longitudinal pressure gradient has been carried out. The injection regimes in which the temperature of the injected gas is lower than the temperature of the adiabatic impermeable wall and the stagnation temperature of the oncoming flow are considered. The existence of a minimum temperature of the permeable wall is confirmed, at which the wall temperature is lower than the temperature of the injected gas, while there are two sections along the length of the permeable plate in which the adiabatic conditions are satisfied. The results of calculations of a supersonic flow with a longitudinal pressure gradient differ significantly from the results obtained for a gradientless flow around a plate, for both subcritical and critical injection.

Abstract Image

外来气体注入下具有正压梯度的超音速流中透气板上的湍流边界层
摘要 对存在正纵向压力梯度的超音速氙气流中注入氦气的透气板上的湍流边界层进行了数值模拟。考虑了注入气体温度低于绝热不透水壁温度和来流停滞温度的注入状态。结果证实,存在渗透壁的最低温度,在该温度下,渗透壁的温度低于注入气体的温度,而沿渗透板长度方向存在满足绝热条件的两个区段。在亚临界和临界注入情况下,具有纵向压力梯度的超音速流动的计算结果与板周围无梯度流动的计算结果有很大不同。
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来源期刊
Doklady Physics
Doklady Physics 物理-力学
CiteScore
1.40
自引率
12.50%
发文量
12
审稿时长
4-8 weeks
期刊介绍: Doklady Physics is a journal that publishes new research in physics of great significance. Initially the journal was a forum of the Russian Academy of Science and published only best contributions from Russia in the form of short articles. Now the journal welcomes submissions from any country in the English or Russian language. Every manuscript must be recommended by Russian or foreign members of the Russian Academy of Sciences.
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