Cavitation in cryogenic fluids has a thermodynamic effect because of the thermal imbalance around the cavity. It improves cavitation performances in turbomachines due to the delay of cavity growth. The relationship between the thermodynamic effect and cavitation instabilities, however, is still unknown. To investigate the influence of the thermodynamic effect on rotating cavitation appeared in the turbopump inducer, we conducted experiments in which liquid nitrogen was set at different temperatures (74 K, 78 K, and 83 K) with a focus on the cavity length. At higher cavitation numbers, supersynchronous rotating cavitation occurred at the critical cavity length of with a weak thermodynamic effect in terms of the fluctuation of cavity length. In contrast, synchronous rotating cavitation occurred at the critical cavity length of at lower cavitation numbers. The critical cavitation number shifted to a lower level due to the suppression of cavity growth by the thermodynamic effect, which appeared significantly with rising liquid temperature. The unevenness of cavity length under synchronous rotating cavitation was decreased by the thermodynamic effect. Furthermore, we confirmed that the fluid force acting on the inducer notably increased under conditions of rotating cavitation, but that the amplitude of the shaft vibration depended on the degree of the unevenness of the cavity length through the thermodynamic effect.
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e-mail: yoshida.yoshiki@jaxa.jp
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September 2009
Research Papers
Thermodynamic Effect on Rotating Cavitation in an Inducer
Yoshiki Yoshida,
Yoshiki Yoshida
Kakuda Space Center,
e-mail: yoshida.yoshiki@jaxa.jp
Japan Aerospace Exploration Agency
, Koganezawa 1, Kimigaya, Kakuda, Miyagi 981-1525, Japan
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Yoshifumi Sasao,
Yoshifumi Sasao
Institute of Fluid Science,
Tohoku University
, Katahira 2-1-1, Aoba, Sendai, Miyagi 980-8577, Japan
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Mitsuo Watanabe,
Mitsuo Watanabe
Kakuda Space Center,
Japan Aerospace Exploration Agency
, Koganezawa 1, Kimigaya, Kakuda, Miyagi 981-1525, Japan
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Tomoyuki Hashimoto,
Tomoyuki Hashimoto
Kakuda Space Center,
Japan Aerospace Exploration Agency
, Koganezawa 1, Kimigaya, Kakuda, Miyagi 981-1525, 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
Kakuda Space Center,
Japan Aerospace Exploration Agency
, Koganezawa 1, Kimigaya, Kakuda, Miyagi 981-1525, Japane-mail: yoshida.yoshiki@jaxa.jp
Yoshifumi Sasao
Institute of Fluid Science,
Tohoku University
, Katahira 2-1-1, Aoba, Sendai, Miyagi 980-8577, Japan
Mitsuo Watanabe
Kakuda Space Center,
Japan Aerospace Exploration Agency
, Koganezawa 1, Kimigaya, Kakuda, Miyagi 981-1525, Japan
Tomoyuki Hashimoto
Kakuda Space Center,
Japan Aerospace Exploration Agency
, Koganezawa 1, Kimigaya, Kakuda, Miyagi 981-1525, 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, JapanJ. Fluids Eng. Sep 2009, 131(9): 091302 (7 pages)
Published Online: August 18, 2009
Article history
Received:
April 14, 2008
Revised:
June 21, 2009
Published:
August 18, 2009
Citation
Yoshida, Y., Sasao, Y., Watanabe, M., Hashimoto, T., Iga, Y., and Ikohagi, T. (August 18, 2009). "Thermodynamic Effect on Rotating Cavitation in an Inducer." ASME. J. Fluids Eng. September 2009; 131(9): 091302. https://doi.org/10.1115/1.3192135
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