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Study of Rocket Engine Pump Cavitation Compliance

机译:火箭发动机泵空化顺应性研究

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摘要

This paper presents a brief overview of the pogo phenomenon in liquid propellant launch vehicles and reviews the dynamics of cavitating pumps. The importance of the cavitation compliance and mass flow gain factor in determining the dynamic characteristics and instabilities of rocket engine turbopumps is also discussed. A collection of the nondimensionalized pump inlet compliance data is plotted together on a single graph with the purpose of identifying trends and correlations between cavitation compliance and cavitation number. An initial assessment of the data demonstrated two trends, which separated the single term compliance data from the two term compliance data. The two term compliance data is suggested to be three to ten times smaller than the single term compliance data. However, by combining the nondimensionalized compliance together with the nondimensionalized mass flow gain factor to form a single compliance model, it is demonstrated that all of the data can be correlated together as a function of cavitation number. From this review, an initial estimate for pump cavitation compliance in new pump designs and pogo stability analyses can be obtained.
机译:本文简要概述了液体推进剂运载火箭中的pogo现象,并综述了空化泵的动力学特性。还讨论了气蚀顺应性和质量流量增加因子在确定火箭发动机涡轮泵的动力特性和不稳定性方面的重要性。将无量纲的泵入口顺应性数据的集合一起绘制在单个图形上,以识别空化顺应性和空化数之间的趋势和相关性。数据的初步评估显示出两种趋势,这将单项合规性数据与两个项合规性数据分开了。建议两个术语合规性数据比单个术语合规性数据小三到十倍。但是,通过将无量纲的顺应性与无量纲的质量流量增益因子结合在一起以形成一个单一的顺应性模型,证明了所有数据都可以作为空化数的函数相互关联。通过此审查,可以获得有关新泵设计中泵气穴合规性的初步估计以及pogo稳定性分析。

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