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Throttling a Laval Nozzle by a Vortex: an Analytical Theory

机译:通过漩涡节约拉瓦尔喷嘴:分析理论

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This paper presents an analytical theory for a vortex flow through a Laval nozzle. It will demonstrate that when a vortex is present the total velocity reaches sonic conditions upstream of the nozzle throat, that the axial velocity in the nozzle throat is equal to the local speed of sound and that the mass flow through the Laval nozzle depends on the vortex strength in such a way that the mass flow decreases with increasing vortex strength. The predictions of the analytical theory have been compared to the results of experiments and a numerical simulation, and it can be concluded that the analytical theory describes the characteristics of the flow very well.
机译:本文介绍了通过拉瓦尔喷嘴的涡流流动的分析理论。它将证明,当涡流存在时,总速度达到喷嘴喉上游的声音条件,即喷嘴喉部的轴向速度等于局部声速,并且通过拉瓦尔喷嘴的质量流动取决于涡流强度以使质量流量随着涡流强度的增加而降低。将分析理论的预测与实验结果和数值模拟进行了比较,并且可以得出结论,分析理论描述了流量的特性。

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