Turbomachinery
Online ISSN : 1880-2338
Print ISSN : 0385-8839
ISSN-L : 0385-8839
Technical papers
Observation of Unsteady Behavior of Cavitation in a Liquid Rocket Inducer Using a Multi-Point Pressure Measurement Technique
Yuka IGAYuto NAKURASota HARADASatoshi KAWASAKI
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2025 Volume 53 Issue 4 Pages 218-228

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Abstract

A multi-point pressure measurement method has been developed that visualizes cavity volume fluctuations in a steel casing over a long period of time with a time resolution of 1/ 3 of a rotation of the inducer by arranging three rows of pressure sensors on the casing and scanning the pressure distribution around a rotating inducer. In this study, the multi-point pressure measurement method is used to observe the unsteady behavior of cavitation that occurs in three-blade inducer during depressurization operation. The time variation of pressure distribution around the inducer obtained by the multi-point pressure measurement method are used to estimate the waveform of fluctuation of cavity length and the frequency, thereby determining the occurrence of cavitation instability.

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© 2025 by Turbomachinery Society of Japan
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