雷诺数
风洞
海洋工程
环境科学
低温学
航空航天工程
机械
计算机科学
物理
工程类
湍流
热力学
作者
Uwe Fey,Yasuhiro Egami,Robert Konrath,Tania Kirmse,Thomas Ahlefeldt,J. Kompenhans
出处
期刊:50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
日期:2010-01-04
被引量:23
摘要
The present paper addresses the development, qualification trials and application of some non-intrusive measurement techniques suitable for operation in industry-scale,
pressurised cryogenic wind tunnels. The application of cryogenic Temperature-Sensitive Paint (cryoTSP) as a tool for transition detection is described as well as the implementation
of the Image Pattern Correlation Technique (IPCT) and the Backward Oriented Schlieren method (BOS) in the European Transonic Windtunnel (ETW). Progress on the development
of cryogenic Pressure-Sensitive Paint (cryoPSP) is shown, and considerations for the
establishment of a Particle Image Velocimetry system suited for low temperatures (cryoPIV)
are presented. Furthermore, the state of adaptation of the microphone array technique
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