@inproceedings{oai:jaxa.repo.nii.ac.jp:00013518,
 author = {賞雅, 寛而 and 波津久, 達也 and 福原, 豊 and 廣瀬, 由典 and 安部, 和也 and 日引, 俊 and Takamasa, Tomoji and Hazuku, Tatsuya and Fukuhara, Yutaka and Hirose, Yoshinori and Abe, Kazuya and Hibiki, Takashi},
 book = {宇宙利用シンポジウム　第23回　平成18年度, Space Utilization Research: Proceedings of the Twenty-third Space Utilization Symposium},
 month = {Mar},
 note = {It is essential to develop gas-liquid two-phase flow (gas-liquid concurrent flow) modeling not only for improved heat transfer efficiency in territorial energy plants but also for the design of fuel pipe flows and heat control lines in spacecraft. Many experimental and theoretical efforts have been devoted to achieving a two-fluid model, which is one of the most popular models for industrial use. Such a model consists of individual mass, momentum, and energy conservation equations for two-phase flow, using an accurate description of the interfacial area transport or interfacial area concentration and the drive force acting on the gas-liquid interface. In this research, a basic database was obtained by measuring interfacial area transport under micro- and normal-gravity environments, using the drop-shaft in the Micro-Gravity Laboratory of Japan (MGLAB). The database showed the proposed model accurately predicted the relative velocity between bubble and liquid flow in the channel even in micro-gravity condition, and the estimated weight caused by the frictional pressure loss should be taken into account in the interfacial area transport and drift velocity., 資料番号: AA0063349020},
 pages = {76--79},
 publisher = {宇宙航空研究開発機構宇宙科学研究本部, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA/ISAS)},
 title = {宇宙空間における気液2相流界面積濃度輸送機構解明に関する研究},
 year = {2007}
}