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Light-in-flight holographic particle image velocimetry for wind-tunnel applications

机译:风洞应用中的飞行中全息全息颗粒图像测速仪

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摘要

Holographic particle imaging techniques for air-flow investigations are mainly limited to small-scale laboratory experiments. The two main reasons are the limited light power available in conjunction with small tracer-particle sizes, which must be in the order of 1 μm to properly probe air flows, and the increased background noise from out-of-focus particles in deep volumes preventing investigations with higher particle densities. To ensure a good accuracy of the velocity measurements by faithful reconstruction geometry, the evaluation of particle images is often conducted in the original recording set-up. The time-consuming scanning process, however, blocks the flow facility during evaluation—a disadvantage for measurements in costly industrial wind tunnels. For an alternative, we have introduced off-site reconstruction and evaluation. In recent papers we have furthermore demonstrated principles to cope with little object light and to suppress background noise. Here we present a successful implementation of theses principles for wind-tunnel measurements.
机译:用于气流研究的全息粒子成像技术主要限于小型实验室实验。两个主要原因是,可用的光功率有限,且示踪剂颗粒尺寸较小(必须正确在1μm的数量级以正确探测空气流),以及深层中散焦颗粒的背景噪声增加,无法防止更高的颗粒密度的研究。为了确保通过忠实的重建几何形状获得良好的速度测量精度,通常在原始记录设置中对粒子图像进行评估。但是,耗时的扫描过程在评估过程中阻塞了流动设施,这对于在昂贵的工业风洞中进行测量是不利的。作为替代方案,我们引入了异地重建和评估。在最近的论文中,我们进一步展示了处理很少的物体光并抑制背景噪声的原理。在这里,我们介绍了风洞测量这些原理的成功实施。

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