@techreport{oai:jaxa.repo.nii.ac.jp:00002601,
 author = {吉田, 義樹 and 渡邉, 光男 and 長谷川, 敏 and 橋本, 知之 and 島垣, 満 and 木村, 俊哉 and 永浦, 克司 and 菊田, 研吾 and 笹尾, 好史 and 風見, 佑介 and Yoshida, Yoshiki and Watanabe, Mitsuo and Hasegawa, Satoshi and Hashimoto, Tomoyuki and Shimagaki, Mitsuru and Kimura, Toshiya and Nagaura, Katsuji and Kikuta, Kengo and Sasao, Yoshifumi and Kazami, Yusuke},
 month = {Dec},
 note = {Turbopump inducer, which is actually a high-precision, high-speed, sophisticated rotating impeller, is one of the key components of a liquid propellant rocket engine. On the other hand, the thermodynamic effect on cavitation is a favorable phenomenon in cryogenic fluids. It suppresses the growth of cavity since thermal imbalance appears around the cavity due to heat transfer for evaporation. Therefore, cavitation performance in cryogenic fluids is improved. In this article, some highlights about the thermodynamic effects on cavitating inducer carried out during the years 2004-2006 through the Cryogenic Inducer Test Facility in JAXA are presented., 形態: カラー図版あり, 著者人数: 14人, 資料番号: AA0064231000, レポート番号: JAXA-RM-08-005},
 title = {JAXA極低音インデューサ試験結果の概要},
 year = {2008}
}