日本航空宇宙学会論文集
Online ISSN : 2432-3691
Print ISSN : 1344-6460
ISSN-L : 1344-6460
論文
ロケットポンプインデューサの内部流れと非定常圧力変動 におよぼすケーシング形状の影響
島垣 満芳賀 宏行橋本 知之渡邉 光男長谷川 敏志村 隆上條 謙二郎
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2005 年 53 巻 617 号 p. 266-273

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The effects of the inlet casing configurations on unsteady cavitation were examined with a 3-bladed inducer. The inlet flow and cavitation pattern in two different casings were visualized using PIV (particle image velocimetry) and high-speed video. It was found that the rotating cavitation would be suppressed when the tip clearance at the inducer inlet was increased. The vortex cavitation in tip leakage flow and cavitation in back flow is considered to affect the appearance of the rotating cavitation by the inlet casing configuration.
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© 2005 The Japan Society for Aeronautical and Space Sciences
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