首页> 外文会议>Instrumentation in Aerospace Simulation Facilities, 1991. ICIASF '91 Record., International Congress on >A simple three component velocity measurement method using arotated split-film sensor
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A simple three component velocity measurement method using arotated split-film sensor

机译:一种简单的三分量速度测量方法旋转分膜传感器

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A rotated split-film anemometry method which can be used to obtainthree-component average flow velocities is reviewed and evaluated. Therelated theory, apparatus, calibration procedure, and results of the newtechnique are discussed. The new technique utilizes a single split-filmprobe in combination with a mechanical rotating probe, holder. The basicprocedure is to make a plane or two-component velocity measurement withthe probe in one orientation and then to rotate the probe 90° andmake another measurement. The two pairs of velocity and flow angle data,are correlated, for yawed flow effects, and resolved to identify three(steady-flow) speed and direction components. Measurements in anaxisymmetric jet at various flow speeds and angles indicate that themethod has, under most circumstances, errors of about 5%. Slightlygreater errors were encountered at extreme test flow speeds and at largesensor yaw and pitch angles
机译:旋转裂膜风速测定法可用于获得 审查和评估三组分平均流速。这 相关理论,仪器,校准程序和新结果 技术进行了讨论。这项新技术利用了单个裂膜 探头与机械旋转探头,支架结合使用。基础的 程序是用 将探针朝一个方向旋转,然后将探针旋转90°,然后 再做一个测量。两对速度和流角数据, 相互关联,以解决偏航流的影响,并确定了三个 (恒流)速度和方向分量。测量中 在各种流速和角度下的轴对称射流表明, 在大多数情况下,该方法的误差约为5%。轻微地 在极端的测试流速和较大的速度下会遇到更大的错误 传感器偏航角和俯仰角

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