Analysis of Acoustic Cavitation Surge in a Rocket Engine Turbopump

In a liquid rocket engine, cavitation in an inducer of a turbopump sometimes causes instability phenomena when the inducer is operated at low inlet pressure. Cavitation surge (auto-oscillation), one such instability phenomenon, has been discussed mainly based on an inertia model assuming incompressi...

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Main Authors: Hideaki Nanri, Hiroki Kannan, Naoki Tani, Yoshiki Yoshida
Format: Article
Language:English
Published: Wiley 2010-01-01
Series:International Journal of Rotating Machinery
Online Access:http://dx.doi.org/10.1155/2010/717013
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author Hideaki Nanri
Hiroki Kannan
Naoki Tani
Yoshiki Yoshida
author_facet Hideaki Nanri
Hiroki Kannan
Naoki Tani
Yoshiki Yoshida
author_sort Hideaki Nanri
collection DOAJ
description In a liquid rocket engine, cavitation in an inducer of a turbopump sometimes causes instability phenomena when the inducer is operated at low inlet pressure. Cavitation surge (auto-oscillation), one such instability phenomenon, has been discussed mainly based on an inertia model assuming incompressible flow. When this model is used, the frequency of the cavitation surge decreases continuously as the inlet pressure of the turbopump decreases. However, we obtained an interesting experimental result in which the frequency of cavitation surge varied discontinuously. Therefore, we employed one-dimensional analysis based on an acoustic model in which the fluid is assumed to be compressible. The analytical result qualitatively corresponded with the experimental result.
format Article
id doaj-art-9e2b50796d7e49f39dfa8d5c531ff54e
institution Kabale University
issn 1023-621X
1542-3034
language English
publishDate 2010-01-01
publisher Wiley
record_format Article
series International Journal of Rotating Machinery
spelling doaj-art-9e2b50796d7e49f39dfa8d5c531ff54e2025-02-03T01:24:18ZengWileyInternational Journal of Rotating Machinery1023-621X1542-30342010-01-01201010.1155/2010/717013717013Analysis of Acoustic Cavitation Surge in a Rocket Engine TurbopumpHideaki Nanri0Hiroki Kannan1Naoki Tani2Yoshiki Yoshida3Space Transportation Propulsion Research and Development Center, Japan Aerospace Exploration Agency (JAXA), 1 Takakuzo, Jinjiro, Kakuda, Miyagi 981-1526, JapanSpace Transportation Propulsion Research and Development Center, Japan Aerospace Exploration Agency (JAXA), 1 Takakuzo, Jinjiro, Kakuda, Miyagi 981-1526, JapanJAXA's Engineering Digital Innovation Center, JAXA 2-1-1, Sengen, Tsukuba, Ibaraki 305-8505, JapanSpace Transportation Propulsion Research and Development Center, Japan Aerospace Exploration Agency (JAXA), 1 Takakuzo, Jinjiro, Kakuda, Miyagi 981-1526, JapanIn a liquid rocket engine, cavitation in an inducer of a turbopump sometimes causes instability phenomena when the inducer is operated at low inlet pressure. Cavitation surge (auto-oscillation), one such instability phenomenon, has been discussed mainly based on an inertia model assuming incompressible flow. When this model is used, the frequency of the cavitation surge decreases continuously as the inlet pressure of the turbopump decreases. However, we obtained an interesting experimental result in which the frequency of cavitation surge varied discontinuously. Therefore, we employed one-dimensional analysis based on an acoustic model in which the fluid is assumed to be compressible. The analytical result qualitatively corresponded with the experimental result.http://dx.doi.org/10.1155/2010/717013
spellingShingle Hideaki Nanri
Hiroki Kannan
Naoki Tani
Yoshiki Yoshida
Analysis of Acoustic Cavitation Surge in a Rocket Engine Turbopump
International Journal of Rotating Machinery
title Analysis of Acoustic Cavitation Surge in a Rocket Engine Turbopump
title_full Analysis of Acoustic Cavitation Surge in a Rocket Engine Turbopump
title_fullStr Analysis of Acoustic Cavitation Surge in a Rocket Engine Turbopump
title_full_unstemmed Analysis of Acoustic Cavitation Surge in a Rocket Engine Turbopump
title_short Analysis of Acoustic Cavitation Surge in a Rocket Engine Turbopump
title_sort analysis of acoustic cavitation surge in a rocket engine turbopump
url http://dx.doi.org/10.1155/2010/717013
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AT naokitani analysisofacousticcavitationsurgeinarocketengineturbopump
AT yoshikiyoshida analysisofacousticcavitationsurgeinarocketengineturbopump