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Comparison of SPIV Measurements for Different Test Room Air Inlet Nozzle Configurations

机译:不同测试室进气喷嘴配置的SPIV测量结果比较

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The effect of varying inlet air velocity due to a corresponding change in inlet nozzle slot size to achieve a constant slot Reynolds number was investigated in a benchmark room. The primary objective of the project was to evaluate the dependence of turbulence intensity levels in the room upon the air inlet nozzle slot geometry. A stereoscopic particle image velocimetry (SPIV) system was used to measure airflow characteristics for two different air inlet nozzle slot sizes in an irregularly shaped test room. The inlet Reynolds number of 2,226 based on inlet nozzle slot opening was the same for the two air inlet nozzle slot configurations. The SPIV measurements were taken at five measurement locations along the center plane of the test room for both configurations. For each measurement location and air inlet nozzle configuration, a series of SPIV data were collected and averaged to determine a grid of three-dimensional average velocities and normalized turbulence intensities over a 304.8 x 304.8 mm (12 x 12 in.) region. A comparison was made for the average velocities and normalized turbulence intensities at the five measurement locations for the two inlet configurations. It was found that there was a substantial shift in the center of rotation of overall airflow pattern due to a change in air inlet nozzle configuration. However, the turbulence levels in the room do not appear to be strongly dependent upon the inlet nozzle velocity because the inlet slot Reynolds number is not changed.
机译:在基准室中研究了由于进气喷嘴槽口尺寸的相应变化而导致进气风速变化以实现恒定的槽口雷诺数的影响。该项目的主要目的是评估房间中湍流强度水平对进气喷嘴槽几何形状的依赖性。在不规则形状的测试室中,使用立体粒子图像测速(SPIV)系统来测量两种不同进气喷嘴槽尺寸的气流特性。对于两种进气喷嘴插槽配置,基于进气喷嘴插槽开口的进气雷诺数为2,226,是相同的。对于这两种配置,在沿着测试室中心平面的五个测量位置进行了SPIV测量。对于每个测量位置和进气喷嘴配置,收集一系列SPIV数据并取平均值,以确定在304.8 x 304.8毫米(12 x 12英寸)范围内的三维平均速度和归一化湍流强度的网格。比较了两种进口配置的五个测量位置处的平均速度和归一化湍流强度。已经发现,由于进气喷嘴构造的改变,整个气流模式的旋转中心有很大的偏移。但是,由于进气口槽的雷诺数不变,因此室内的湍流程度似乎与进气喷嘴的速度没有很大关系。

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