EXPERIMENTAL STAND AND MEASUREMENT METHODS TO BE USED IN TURBULENT BOUNDARY LAYER-NORMAL SHOCK WAVE INTERACTION ON A CURVED WALL.

被引：0
|
作者：
Doerffer, Piotr [1 ]
机构：
[1] Karlsruhe Univ, Karlsruhe, West Ger, Karlsruhe Univ, Karlsruhe, West Ger
来源：
Stroemungsmechanik und Stroemungsmaschinen | 1985年
关键词：
FLUID MECHANICS - Fluid Dynamics - WIND TUNNELS - Wall Interference;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
An experimental stand for the investigation of turbulent boundary layer-normal shock wave interaction is presented. It provides means for continuous and exact Mach number control in front of the interaction. A special method for boundary layer thickness change is presented which allows for Reynolds number control while Mach number is constant. Separation detection techniques are discussed. Oil-TiO//2 visualization combined with liquid crystals visualization should provide sufficient data for separation determination.
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页码：17 / 52
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