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

被引：0
|
作者：
A. V. Glushniova
A. S. Saveliev
E. E. Son
D. V. Tereshonok
机构：
[1] State University,Moscow Institute of Physics and Technology
[2] Russian Academy of Sciences,Joint Institute for High Temperatures
来源：
High Temperature | 2014年 / 52卷
关键词：
Particle Image Velocimetry; Proper Orthogonal Decomposition; Separation Bubble; Separation Region; Temperature Ratio;
D O I：
暂无
中图分类号：
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.
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页码：220 / 224
页数：4
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