期刊:50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition日期:2010-01-04被引量:23
标识
DOI:10.2514/6.2010-1301
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