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 a rotated split-film sensor
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A simple three component velocity measurement method using a rotated split-film sensor

机译:使用旋转裂膜传感器的简单三分量速度测量方法

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A rotated split-film anemometry method which can be used to obtain three-component average flow velocities is reviewed and evaluated. The related theory, apparatus, calibration procedure, and results of the new technique are discussed. The new technique utilizes a single split-film probe in combination with a mechanical rotating probe, holder. The basic procedure is to make a plane or two-component velocity measurement with the probe in one orientation and then to rotate the probe 90 degrees and make 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 an axisymmetric jet at various flow speeds and angles indicate that the method has, under most circumstances, errors of about 5%. Slightly greater errors were encountered at extreme test flow speeds and at large sensor yaw and pitch angles.
机译:回顾和评估了可用于获得三分量平均流速的旋转裂膜风速测定法。讨论了该新技术的相关理论,仪器,校准程序和结果。这项新技术将单个裂膜探针与机械旋转探针支架一起使用。基本步骤是在探头处于一个方向的情况下进行平面或两分量速度测量,然后将探头旋转90度并进行另一次测量。针对偏航流效应,将两对速度和流角数据进行关联,并解析以识别三个(恒流)速度和方向分量。在轴对称射流中以各种流速和角度进行的测量表明,在大多数情况下,该方法的误差约为5%。在极限测试流速和较大的传感器偏航角和俯仰角下,遇到的误差略大。

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