日本造船学会論文集
Online ISSN : 1884-2070
Print ISSN : 0514-8499
ISSN-L : 0514-8499
バブルキャビテーション時の翼型性能推定
豊田 真山口 一加藤 洋治
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ジャーナル フリー

1999 年 1999 巻 186 号 p. 59-64

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抄録
Existing theories for 2-dimensional foil sections can predict foil performance in noncavitating condition or sheet cavitation condition, but cannot predict foil performance in bubble/streak cavitation condition. In this study, the authors developed a new method to predict foil performance in bubble cavitation condition theoretically. Displacement thickness due to bubble cavity is calculated by solving Reyleigh-Plesset equation in an iterative method, and pressure distribution around the “displacement body” is computed.
Experiments are performed in a cavitation tunnel in order to verify the accuracy of new prediction theory. The calculated results by the new theory agreed well with the experimental results on foil performance. It is still difficult to predict foil performance when sheet cavitation turns into bubble cavitation.
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