JAXA Repository / AIREX 未来へ続く、宙(そら)への英知

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titleキャビテーション噴流中の衝撃波発生頻度に関する研究 -境界条件及びノズル形状が及ぼす影響-
Other TitleStudy on Generation Frequency of Shock Wave in Cavitation Jet Flow -Influence of Boundary Condition and Nozzle Shape-
Author(jpn)西林, 昂大; 王, 静竹; 阿部, 晃久
Author(eng)Nishibayashi, Kota; Wang Jingzhu; Abe, Akihisa
Author Affiliation(jpn)神戸大学; 神戸大学; 神戸大学
Author Affiliation(eng)Graduate School of Maritime Sciences, Kobe University; Graduate School of Maritime Sciences, Kobe University; Graduate School of Maritime Sciences, Kobe University
Issue Date2017-03
Publisher宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)(ISAS)
Publication title平成28年度衝撃波シンポジウム 講演論文集
Proceedings of the Symposium on Shock Waves in Japan, FY2016
Publication date2017-03
Languagejpn
Description会議情報: 平成28年度衝撃波シンポジウム (2017年3月8日-10日. ヴェルクよこすか 横須賀市立勤労福祉会館)横須賀市, 神奈川県
Meeting Information: Symposium on Shock Waves in Japan, FY2016 (March 8-10, 2017. Werk Yokosuka), Kanagawa, Japan
KeywordsRebound Shock Wave; Cavitation Jet Flow; Orifice Plate; High Pressure Pump
Document TypeConference Paper
JAXA Categoryシンポジウム・研究会
SHI-NOSA6000084098
Report No3C1-2【若】
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/614440


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