Based on the length of the tip cavitation as an indication of cavitation, we focused on the effect of thermodynamics on cavitation performances and cavitation instabilities in an inducer. Comparison of the tip cavity length in liquid nitrogen ( and ) as working fluid with that in cold water allowed us to estimate the strength of the thermodynamic effect on the cavitations. The degree of thermodynamic effect was found to increase with an increase of the cavity length, particularly when the cavity length extended over the throat of the blade passage. In addition, cavitation instabilities occurred both in liquid nitrogen and in cold water when the cavity length increased. Subsynchronous rotating cavitation appeared both in liquid nitrogen and in cold water. In the experiment using liquid nitrogen, the temperature difference between and affected the range in which the subsynchronous rotating cavitation occurred. In contrast, deep cavitation surge appeared only in cold water at lower cavitation numbers. From these experimental results, it was concluded that when the cavity length extends over the throat, the thermodynamic effect also affects the cavitation instabilities as a “thermal damping” through the unsteady cavitation characteristics.
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e-mail: yoshida.yoshiki@jaxa.jp
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November 2008
Research Papers
Thermodynamic Effect on Cavitation Performances and Cavitation Instabilities in an Inducer
Kengo Kikuta,
Kengo Kikuta
Japan Aerospace Exploration Agency,
e-mail: kikuta.kengo@jaxa.jp
Kakuda Space Center
, Koganezawa 1, Kimigaya, Kakuda, Miyagi 981-1525, Japan
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Yoshiki Yoshida,
Yoshiki Yoshida
Japan Aerospace Exploration Agency,
e-mail: yoshida.yoshiki@jaxa.jp
Kakuda Space Center
, Koganezawa 1, Kimigaya, Kakuda, Miyagi 981-1525, Japan
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Mitsuo Watanabe,
Mitsuo Watanabe
Japan Aerospace Exploration Agency,
Kakuda Space Center
, Koganezawa 1, Kimigaya, Kakuda, Miyagi 981-1525, Japan
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Tomoyuki Hashimoto,
Tomoyuki Hashimoto
Japan Aerospace Exploration Agency,
Kakuda Space Center
, Koganezawa 1, Kimigaya, Kakuda, Miyagi 981-1525, Japan
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Katsuji Nagaura,
Katsuji Nagaura
Foundation for Promotion of Japanese Aerospace Technology
, Koganezawa 1, Kimigaya, Kakuda, Miyagi 981-1525, Japan
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Katsuhide Ohira
Katsuhide Ohira
Institute of Fluid Science,
Tohoku University
, Katahira 2-1-1, Aoba, Sendai, Miyagi 980-8577, Japan
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Kengo Kikuta
Japan Aerospace Exploration Agency,
Kakuda Space Center
, Koganezawa 1, Kimigaya, Kakuda, Miyagi 981-1525, Japane-mail: kikuta.kengo@jaxa.jp
Yoshiki Yoshida
Japan Aerospace Exploration Agency,
Kakuda Space Center
, Koganezawa 1, Kimigaya, Kakuda, Miyagi 981-1525, Japane-mail: yoshida.yoshiki@jaxa.jp
Mitsuo Watanabe
Japan Aerospace Exploration Agency,
Kakuda Space Center
, Koganezawa 1, Kimigaya, Kakuda, Miyagi 981-1525, Japan
Tomoyuki Hashimoto
Japan Aerospace Exploration Agency,
Kakuda Space Center
, Koganezawa 1, Kimigaya, Kakuda, Miyagi 981-1525, Japan
Katsuji Nagaura
Foundation for Promotion of Japanese Aerospace Technology
, Koganezawa 1, Kimigaya, Kakuda, Miyagi 981-1525, Japan
Katsuhide Ohira
Institute of Fluid Science,
Tohoku University
, Katahira 2-1-1, Aoba, Sendai, Miyagi 980-8577, JapanJ. Fluids Eng. Nov 2008, 130(11): 111302 (8 pages)
Published Online: September 22, 2008
Article history
Received:
May 25, 2007
Revised:
July 2, 2008
Published:
September 22, 2008
Citation
Kikuta, K., Yoshida, Y., Watanabe, M., Hashimoto, T., Nagaura, K., and Ohira, K. (September 22, 2008). "Thermodynamic Effect on Cavitation Performances and Cavitation Instabilities in an Inducer." ASME. J. Fluids Eng. November 2008; 130(11): 111302. https://doi.org/10.1115/1.2969426
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