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Cavitation flow instability of subcooled liquid nitrogen in converging–diverging nozzles

机译:会聚-扩张喷嘴中过冷液氮的空化流不稳定性

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摘要

The cavitation flow instability of subcooled liquid nitrogen in two types of converging–diverging (C–D)circular nozzles with throat diameters of 1.5 and 2.0 mm was experimentally investigated. Flow observations were also performed to clarify the instability phenomenon and the differences in cavitation behavior between the two nozzles. The cavitation mode changed from continuous mode to intermittent mode as the temperature of the subcooled liquid nitrogen decreased. This change occurred in both C–D nozzles when the temperature of the liquid reached approximately 76 K. Occurrence of the intermittent mode accompanying very large pressure-oscillations was considered to be caused by a drastic reduction of the speed of sound in the single-component, vapor–liquid flow because the speed of sound restricted the throat velocity in the C–D nozzle during cavitation. Oscillation pressure values in intermittent mode were much larger than those in continuous mode, peaking between 74 and 76 K. The magnitude of the oscillation pressure in intermittent mode could be evaluated from the difference between the throat static-pressure immediately prior to the occurrence of cavitation and that during cavitation.
机译:实验研究了两种直径为1.5和2.0 mm的会聚(发散)圆形喷嘴中过冷液氮的空化流动不稳定性。还进行了流量观察以澄清两个喷嘴之间的不稳定性现象和气蚀行为的差异。随着过冷液氮的温度降低,空化模式从连续模式改变为间歇模式。当液体的温度达到约76 K时,两个C-D喷嘴都发生了这种变化。出现间歇模式并伴有很大的压力振荡被认为是由于单组分声速的急剧降低引起的。气液流动,因为声速限制了气蚀过程中C–D喷嘴的喉咙速度。间歇模式下的振荡压力值要比连续模式下大得多,峰值介于74和76 K之间。可以根据刚发生气蚀之前的喉部静压之差来评估间歇模式下的振荡压力幅度。以及在气蚀过程中。

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