Measurements and applications of fast response pressure sensitive paint
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摘要: 近年来快速响应压敏涂料测试技术发展迅速。对该技术在国内外的发展及其应用进行详细调研的基础上展开了全面的综述。首先描述了快响应压敏漆测试技术的特点、工作原理及其动态响应机理。然后详述了目前普遍应用的3种多孔结构快响应压敏涂料包括TLC-PSP、AA-PSP和PC-PSP。详细介绍了不同的动态标定设备，包括激波管、电磁阀、驻波管、射流振荡器和脉冲射流装置。归纳了几种主要的测量方法，包括点测量方法，相位平均法，高速图像采集法，双分量运动捕获方法，单次激发寿命法和颗粒法等。引用国内外快速响应PSP技术的典型应用案例，展示了快速响应PSP技术对非定常流动测量的优势。Abstract: The fast response pressure sensitive paint measurement technique has been developed quickly in recent years. A general review of this technique based on detailed investigation is presented. The characteristic, principle and dynamic response mechanism are described. Three kinds of porous structure fast response pressure sensitive paint are introduced, including TLC-PSP, AA-PSP and PC-PSP. Several dynamic calibration devices are introduced, including the shock wave tube, fast response solenoid valve, loudspeaker, jet oscillator and pulse jet. Different measurement methods are introduced including the point measurement, phase averaging, high speed acquiring, motion-capture measurement, life time method, and PSP microspheres method. Different application cases around the world are introduced, which manifests the advantages of the fast response PSP technique on the unsteady flow measurement.
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Key words:
- fast response /
- pressure sensitive paint /
- porous structure /
- unsteady flow
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图 2 PC-PSP结构示意图及电镜扫描结果
Figure 2. Schematic illustrations and scanning electron micrographs of PC-PSP
图 3 PSP激波管响应时间测试示意图
Figure 3. Schematic illustrations of the shock tube for determining the PSP time response
图 11 圆柱绕流非定常压力变化过程前20ms图像，Ma=5，采集频率250 frames/s
Figure 11. The first 20ms image of unsteady pressure behavior around the cylinder, f=250 frames/s, Ma=5
图 19 压缩拐角压力分布云图，30°拐角
Figure 19. Pressure distribution on the compression corner model at the angle of 30°
图 20 前1.5ms中心线和对应的压力孔数据对比
Figure 20. PSP data compared to PSI data on center line in 1.5ms
图 22 尾舵数值模拟(a)和PSP(b)结果对比图(Ma=1.0，α=0°)
Figure 22. Comparison of numerical solution result and PSP result on the rudder, Ma=1.0, α=0°
图 23 舵前缘某测点压力数据随迎角变化对比，Ma=1.0，α=0°，-6°，-12°
Figure 23. Comparison of the pressure data at different angles of attack on the rudder, Ma=1.0, α=0°, -6°, -12°
图 24 弹身某测点PSP和Kulite无量纲功率谱对比，Ma=0.8，α=0°
Figure 24. Comparison of the PSP and the Kulite transducer spectrum on the missile body, Ma=0.8, α=0°
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