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Simultaneous measurement of velocity and fluctuating pressure in a turbulent wing-tip vortex using triple hot-film sensor and miniature total pressure probe

机译:使用三重热膜传感器和微型总压探头同时测量湍流的翼尖涡流中的速度和脉动压力

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摘要

We have developed a probe-system for simultaneous measurement of three velocity components and pressure in turbulent flows. A miniature total pressure probe is placed adjacent to the sensors of a triple hot-film probe in order to achieve the spatial resolution which is equivalent to that of the triple hot-film probe itself. The instantaneous static pressure is calculated from measured velocity and total pressure by means of a newly developed processing method based on the Bernoulli equation for unsteady flows. The measurements were undertaken in a turbulent wing-tip vortex flow. The look-up table method is employed for the calibration of the hot-film probe so accurate velocity data could be obtained over a wide range of the flow-attack angles. It is also demonstrated that the present probe-system is capable of measuring fluctuations in both velocity and pressure in the 20-650 Hz frequency range. The distribution of the fluctuating pressure obtained by this indirect method is in good agreement with the results from direct measurements of static pressure, demonstrating the promising performance of the present method. Furthermore, an improvement in the ability to make measurements of the velocity-pressure correlation across the wing-tip vortex is achieved. This improvement is possible because the effects of lateral velocity components are properly taken into account in the present formulation. The investigation regarding the transport equation budget for turbulent kinetic energy shows an anomalous structure of turbulence in this flow, mainly due to the meandering of the vortex, and the measurement of pressure diffusion is found to play an important role in the characterization of this kind of flow.
机译:我们开发了一种探针系统,用于同时测量湍流中的三个速度分量和压力。将微型总压力探头放置在三重热膜探头的传感器附近,以实现与三重热膜探头本身相同的空间分辨率。瞬时静压力是根据对不稳定流量的伯努利方程式,通过新开发的处理方法,根据测得的速度和总压力计算得出的。测量是在湍流的翼尖涡流中进行的。查找表方法用于热膜探头的校准,因此可以在很大的流动攻角范围内获得准确的速度数据。还证明了本探针系统能够测量20-650Hz频率范围内的速度和压力的波动。通过这种间接方法获得的脉动压力的分布与静压直接测量的结果非常吻合,证明了本方法的前景广阔。此外,实现了跨翼尖涡旋测量速度-压力相关性的能力的提高。这种改进是可能的,因为在本配方中适当考虑了横向速度分量的影响。关于湍动能的输运方程预算的研究表明,这种流动中湍流的结构是异常的,这主要是由于涡流的曲折所致,并且发现压力扩散的测量在表征此类湍流中起着重要的作用。流。

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