Shock wave-boundary layer interaction on the non-adiabatic ramp surface

被引：6

作者：

Glushniova, A. V. ^{[1
]}

Saveliev, A. S. ^{[1
,2
]}

Son, E. E. ^{[1
,2
]}

Tereshonok, D. V. ^{[1
,2
]}

机构：

[1] State Univ, Moscow Inst Phys & Technol, Dolgoprudnyi, Moscow Oblast, Russia

[2] Russian Acad Sci, Joint Inst High Temp, Moscow, Russia

来源：

HIGH TEMPERATURE | 2014年 / 52卷 / 02期

关键词：

Particle Image Velocimetry; Proper Orthogonal Decomposition; Separation Bubble; Separation Region; Temperature Ratio;

D O I：

10.1134/S0018151X14020230

中图分类号：

O59 [应用物理学];

学科分类号：

摘要：

The boundary layer separation of the supersonic air flow over the heated compression ramp has been investigated. Particle Image Velocimetry and Shlieren non-invasive visualization methods were used to study the influence of surface heating on the structure of separation zone. The linear dependence of separation length on the temperature ratio was found. The influence of surface heating on separation region instability was studied. It was found experimentally that increase of wall temperature causes intensification of separation region fluctuations.

引用

页码：220 / 224

页数：5

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