根据液体推进剂火箭发动机空化泵的理论传输矩阵确定其流体力学模型系数

S. Dolgopolov
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引用次数: 0

摘要

液体推进剂火箭发动机(LPRE)空化泵的特性分析是一个重要问题,因为需要提供液体推进剂运载火箭的波高稳定性和液体推进剂推进系统的空化振荡稳定性。建立 LPRE 汽蚀泵的可靠数学模型可以解决这一问题。这项工作的目标是根据分布参数模型获得的 LPRE 汽蚀泵理论传递矩阵,确定 LPRE 汽蚀泵集合参数流体动力学模型系数的汽蚀数和工作参数相关性。以下系数是运行参数的函数:空化弹性、空化阻力、空化引起的扰动传递延迟时间和空化阻力分布系数。后两个系数是气蚀泵流体力学模型中的新系数,是在使用实验和理论泵传递矩阵验证模型时引入的。通过分析气蚀阻力分布系数与运行参数的函数关系,可以发现该系数随着气蚀数的增加而明显减小。这证明块状空穴顺应性的位置从中间位置向泵入口移动。因此,无论气蚀数如何,块状腔顺应性都位于附着腔中部的假设是不成立的。作为空化数函数的分布系数在空化数为 0.25 附近与离散轴相交,这一事实可能表明了附着空腔存在的边界,从而也表明了理论模型的适用边界。扰动传递延迟时间与空化数的函数关系在空化数约为 0.05 时急剧增加。当空化数约为 0.25 时,延迟时间接近常数。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Determining the coefficients of a hydrodynamic model of cavitating pumps of liquid-propellant rocket engines from their theoretical transfer matrices
The characterization of cavitating pumps of liquid-propellant rocket engines (LPRE) is an important problem because of the need to provide the pogo stability of liquid-propellant launch vehicles and the stability of liquid-propellant propulsion systems for cavitation oscillations. The development of a reliable mathematical model of LPRE cavitating pumps allows this problem to be resolved. The goal of this work is to determine the cavitation number and operating parameter dependences of the coefficients of a lumped-parameter hydrodynamic model of LPRE cavitating pumps from their theoretical transfer matrices obtained by a distributed-parameter model. The following coefficients are found as a function of operating parameters: the cavitation elasticity, the cavitation resistance, the cavity-caused disturbance transfer delay time, and the cavitation resistance distribution coefficient. The last two coefficients are new in the hydrodynamic model of cavitating pumps, and they were introduced when verifying the model using experimental and theoretical pump transfer matrices. Analyzing the cavitation resistance distribution coefficient as a function of operating parameters shows that it markedly decreases with increasing cavitation number. This testifies to that the location of the lumped cavity compliance is shifted from the mid position towards the pump inlet. Therefore, the assumption that the lumped cavity compliance is located in the middle of the attached cavity regardless of the cavitation number is not justified. The fact that the distribution coefficient as a function of cavitation number intersects the abscissa axis near a cavitation number of 0.25 may indicate the boundary of existence of attached cavities and thus the applicability boundary of the theoretical model. The disturbance transfer delay time as a function of cavitation number sharply increases at cavitation numbers of about 0.05. At cavitation numbers of about 0.25, it is close to a constant.
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