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Quasi-non intrusive measurement of the transonic flow field in an axi-symmetric critical nozzle based on recovery temperature measurement using a thin thermocouple

机译:基于使用薄热电偶进行恢复温度测量的轴对称临界喷嘴中跨音速流场的准非侵入式测量

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摘要

Flow velocities from several m/s to supersonic of a gas having a Prandtl number different from unity were measured based on the recovery temperatures measurement using a very thin thermocouple, which produced almost no disturbance in the field. Very high space resolution in the 10 μm order as well as very small disturbance from the supports of the thermocouple wire were achieved because the sensing point of a themocouple wire was concentrated exactly at the contact point, which allows to use a long thermocouple wire to locate its supports far away from the measuring point. A thermocouple wire of 50 μmφ accompanied with a traversing system was settled through an axi-symmetrical critical nozzle with a throat diameter of 13.4 mmφ to measure the velocity field in the nozzle. The results agreed quite well with the one-dimensional isentropic theory even qualitatively as well as they showed the fine structure predicted by the two-dimensional isentropic theory. Furthermore, the results revealed complicated flow structures, which were unpredictable by these simple theories, such as oblique shocks and normal shock whose amplitude and location changed depending on the back pressure ratio applied on the nozzle in a complicated manner.
机译:基于使用非常薄的热电偶进行的恢复温度测量,测量了从数m / s到普朗特数不同于单位的气体的超音速的流速,该热电偶在现场几乎不产生干扰。由于热电偶线的感测点正好集中在接触点上,因此实现了10μm量级的很高的空间分辨率以及来自热电偶线支架的很小的干扰,从而允许使用长的热电偶线进行定位它的支撑物远离测量点。将50μmφ的热电偶丝和一个横动系统通过一个轴对称的临界喷嘴(直径为13.4mmφ)安放,以测量喷嘴中的速度场。结果在质量上与一维等熵理论非常吻合,并且显示出二维等熵理论所预测的精细结构。此外,结果揭示了复杂的流动结构,而这些简单的理论无法预测这些流动结构,例如倾斜冲击和法向冲击,其振幅和位置取决于以复杂方式施加在喷嘴上的背压比而变化。

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