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Effect of the Pitot Tube on Measurements in Supersonic Axisymmetric Underexpanded Microjets

机译:皮托管对超声轴对称悬垂性微目亡射精测量的影响

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摘要

This paper describes the results of methodical investigations of the effect of the Pitot tube on measurements of gas-dynamic parameters of supersonic axisymmetric underexpanded real and model microjets. Particular attention is paid to distortions of Pitot pressure variations on the jet axis associated with the wave structure of the jet and to distortions of the supersonic core length. In experiments with model jets escaping from nozzles with diameters ranging from 0.52 to 1.06 mm into the low-pressure chamber, the measurements are performed by the Pitot tubes 0.05 to 2 mm in diameter. The results are analyzed together with the earlier obtained data for real microjets escaping from nozzles with diameters ranging from 10 to 340 µm where the parameters of real microjets were determined by the Pitot microtube 12 µm in diameter. Interaction of the Pitot tube with an unsteady jet in the laminar-turbulent transition region is investigated; the influence of this interaction on Pitot pressure measurements is determined, and a physical interpretation of this phenomenon is provided.
机译:本文介绍了皮托管对超声轴对称悬垂性实体和模型微进程的气体动力学参数测量的有条件研究的结果。与射流的波浪结构相关联的喷射轴和超音速芯长度的扭曲的射流轴上的皮特压力变化的扭曲特别注意。在实验中,使用直径为0.52至1.06mm的喷嘴逸出的模型喷射到低压室中,测量由0.05至2mm的直径执行。结果与先前获得的真实微射精的数据一起分析,用于从10至340μm的直径从10至340μm逸出,其中真实微射精的参数由直径的皮托米特管12μm确定。研究了皮托管与非稳定射流在层状湍流过渡区域中的相互作用;确定该相互作用对皮特压力测量的影响,提供了这种现象的物理解释。

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