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タイトルDevelopment of Boiling and Two-Phase Flow Experiments on Board ISS: Void Fraction Characteristics in the Observation Section just at the Downstream of the Heating Section
DOIinfo:doi/10.15011/ijmsa.33.330104
著者(日)五明, 泰作; 浅野, 等; 大田, 治彦; 新本, 康久; 河南, 治; 鈴木, 康一; 今井, 良二; 岡, 利春; 友部, 俊之; 宇宿, 功史郎; 島田, 雅喜; 高柳, 昌弘; 松本, 聡; 栗本, 卓; 高岡, 秀充; 坂本, 道人; 岡本, 篤; 澤田, 健一郎; 川崎, 春夫; 藤井, 清澄; 木暮, 和美
著者(英)Gomyo, Taisaku; Asano, Hitoshi; Ohta, Haruhiko; Shinmoto, Yasuhisa; Kawanami, Osamu; Suzuki, Koichi; Imai, Ryoji; Oka, Toshiharu; Tomobe, Toshiyuki; Usuku, Koshiro; Shimada, Masaki; Takayanagi, Masahiro; Matsumoto, Satoshi; Kurimoto, Takashi; Takaoka, Hidemitsu; Sakamoto, Michito; Okamoto, Atsushi; Sawada, Kenichiro; Kawasaki, Haruo; Fujii, Kiyosumi; Kogure, Kazumi
著者所属(日)神戸大学; 神戸大学; 九州大学; 九州大学; 兵庫県立大学; 山口東京理科大学; 室蘭工業大学; 株式会社IHIエアロスペース(IA); 株式会社IHIエアロスペース(IA); 株式会社IHIエアロスペース(IA); 株式会社IHIエアロスペース(IA); 宇宙航空研究開発機構(JAXA); 宇宙航空研究開発機構(JAXA); 宇宙航空研究開発機構(JAXA); 宇宙航空研究開発機構(JAXA); 宇宙航空研究開発機構(JAXA); 宇宙航空研究開発機構(JAXA); 宇宙航空研究開発機構(JAXA); 宇宙航空研究開発機構(JAXA); 奈良先端科学技術大学院大学; 日本宇宙フォーラム
著者所属(英)Kobe University; Kobe University; Kyushu University; Kyushu University; University of Hyogo; Tokyo University of Science, Yamaguchi; Muroran Institute of Technology; IHI AEROSPACE Co., Ltd. (IA); IHI AEROSPACE Co., Ltd. (IA); IHI AEROSPACE Co., Ltd. (IA); IHI AEROSPACE Co., Ltd. (IA); Japan Aerospace Exploration Agency (JAXA); Japan Aerospace Exploration Agency (JAXA); Japan Aerospace Exploration Agency (JAXA); Japan Aerospace Exploration Agency (JAXA); Japan Aerospace Exploration Agency (JAXA); Japan Aerospace Exploration Agency (JAXA); Japan Aerospace Exploration Agency (JAXA); Japan Aerospace Exploration Agency (JAXA); Nara Institute of Science and Technology; Japan Space Forum
発行日2016-01-31
発行機関などJapan Society of Microgravity Application (JASMA)
日本マイクログラビティ応用学会(JASMA)
刊行物名International Journal of Microgravity Science and Application (IJMSA)
33
1
開始ページ330104-1
終了ページ330104-10
刊行年月日2016-01-31
言語eng
抄録An observation section has been developed for the detail observation of gas-liquid interfacial structure in boiling and two-phase flow experiments onboard International Space Station. A stereoscopic photography method was applied for 3D measurement using one high frame-rate camera, and the accuracy in measurement of liquid film thickness was evaluated. It was confirmed in the preliminary experiment that liquid film thickness could be measured from images within plus or minus 5 % accuracy. Moreover, to evaluate the development of the flow structure from the exit of the heating section, flow observation and cross-sectional average void fraction measurement was performed at four locations at the downstream of the heating section. As the result, under the condition where slug flow was observed in the developed region, the fluctuation band of void fraction was small just at downstream of the exit of the heating section due to many small bubbles in liquid slugs. Under the conditions where annular flow was observed in the developed region, annular flow had been already formed at the exit, and then liquid film thickness became thicker.
内容記述Physical characteristics: Original contains color illustrations
形態: カラー図版あり
キーワードOne-component gas-liquid two-phase flow; ISS experiment; Flow pattern; Void fraction
資料種別Journal Article
NASA分類Space Processing
ISSN0915-3616
NCIDAN10537663
SHI-NOAA1540521000


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