An experimental study of influence of slits in throat position on suppression of cavitation instabilities in liquid propellant rocket inducer

Moena Kanamaru, Yoshito Kamikura, Satoshi Kawasaki, Takashi Shimura, Iga Yuka

研究成果: Conference contribution

抄録

Experiments of an inducer with symmetric slits were conducted. The purpose of the study is to explore the suppression effect on cavitation instabilities by slits. The slits are located in a throat position in each blade and it means symmetric slits. The experiments are done through measuring pressure fluctuation in the flow field and shaft displacement and visualization using high speed camera. In this study, the head performance, the suction performance, the cavity length and the occurrence range and the strength of the cavitation instabilities are compared with the results of inducer without slit. As a result, the slit in throat position does not give bad effect on head performance, improves suction performance, and has a relation to suppression of oscillation of cavitation instabilities because of the suppression effect of cavity length, although the occurrence range of super-synchronous rotating cavitation unfortunately increases because the cavity develops slowly.

本文言語English
ホスト出版物のタイトルFluid Applications and Systems
出版社American Society of Mechanical Engineers (ASME)
ISBN(電子版)9780791859056
DOI
出版ステータスPublished - 2019
イベントASME-JSME-KSME 2019 8th Joint Fluids Engineering Conference, AJKFluids 2019 - San Francisco, United States
継続期間: 2019 7 282019 8 1

出版物シリーズ

名前ASME-JSME-KSME 2019 8th Joint Fluids Engineering Conference, AJKFluids 2019
3B-2019

Conference

ConferenceASME-JSME-KSME 2019 8th Joint Fluids Engineering Conference, AJKFluids 2019
国/地域United States
CitySan Francisco
Period19/7/2819/8/1

ASJC Scopus subject areas

  • 流体および伝熱

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