The relationship between the thermodynamic effect and subsynchronous rotating cavitation was investigated with a focus on cavity fluctuations. Experiments on a three-bladed inducer were conducted with liquid nitrogen at different temperatures (74, 78, and 83 K) to confirm the dependence of the thermodynamic effects. Subsynchronous rotating cavitation appeared at lower cavitation numbers in liquid nitrogen at 74 K, the same as in cold water. In contrast, in liquid nitrogen at 83 K the occurrence of subsynchronous rotating cavitation was suppressed because of the increase of the thermodynamic effect due to the rising temperature. Furthermore, unevenness of cavity length under synchronous rotating cavitation at 83 K was also decreased by the thermodynamic effect. However, surge mode oscillation occurred simultaneously under this weakened synchronous rotating cavitation. Cavity lengths on the blades oscillated with the same phase and maintained the uneven cavity pattern. It was inferred that the thermodynamic effect weakened peripheral cavitation instability, i.e., synchronous rotating cavitation, and thus axial cavitation instability, i.e., surge mode oscillation, was easily induced due to the synchronization of the cavity fluctuation with an acoustic resonance in the present experimental inlet-pipe system.
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June 2011
Research Papers
Thermodynamic Effect on Subsynchronous Rotating Cavitation and Surge Mode Oscillation in a Space Inducer
Hideaki Nanri,
Hideaki Nanri
Japan Aerospace Exploration Agency,
Kakuda Space Center
, Koganezawa 1, Kimigaya, Kakuda, Miyagi 981-1525, Japan
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Kengo Kikuta,
Kengo Kikuta
Japan Aerospace Exploration Agency,
Kakuda Space Center
, Koganezawa 1, Kimigaya, Kakuda, Miyagi 981-1525, Japan
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Yusuke Kazami,
Yusuke Kazami
Institute of Fluid Science
, Tohoku University, Katahira 2-1-1, Aoba, Sendai, Miyagi 980-8577, Japan
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Yuka Iga,
Yuka Iga
Institute of Fluid Science
, Tohoku University, Katahira 2-1-1, Aoba, Sendai, Miyagi 980-8577, Japan
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Toshiaki Ikohagi
Toshiaki Ikohagi
Institute of Fluid Science
, Tohoku University, Katahira 2-1-1, Aoba, Sendai, Miyagi 980-8577, Japan
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Yoshiki Yoshida
e-mail:
Hideaki Nanri
Japan Aerospace Exploration Agency,
Kakuda Space Center
, Koganezawa 1, Kimigaya, Kakuda, Miyagi 981-1525, Japan
Kengo Kikuta
Japan Aerospace Exploration Agency,
Kakuda Space Center
, Koganezawa 1, Kimigaya, Kakuda, Miyagi 981-1525, Japan
Yusuke Kazami
Institute of Fluid Science
, Tohoku University, Katahira 2-1-1, Aoba, Sendai, Miyagi 980-8577, Japan
Yuka Iga
Institute of Fluid Science
, Tohoku University, Katahira 2-1-1, Aoba, Sendai, Miyagi 980-8577, Japan
Toshiaki Ikohagi
Institute of Fluid Science
, Tohoku University, Katahira 2-1-1, Aoba, Sendai, Miyagi 980-8577, Japan
J. Fluids Eng. Jun 2011, 133(6): 061301 (7 pages)
Published Online: June 15, 2011
Article history
Received:
November 6, 2010
Revised:
April 13, 2011
Online:
June 15, 2011
Published:
June 15, 2011
Citation
Yoshida, Y., Nanri, H., Kikuta, K., Kazami, Y., Iga, Y., and Ikohagi, T. (June 15, 2011). "Thermodynamic Effect on Subsynchronous Rotating Cavitation and Surge Mode Oscillation in a Space Inducer." ASME. J. Fluids Eng. June 2011; 133(6): 061301. https://doi.org/10.1115/1.4004022
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