@inproceedings{oai:jaxa.repo.nii.ac.jp:00016186,
 author = {井川, 祥平 and 津田, 伸一 and Ikawa, Shohei and Tsuda, Shinichi},
 book = {平成24年度宇宙輸送シンポジウム: 講演集録, Proceedings of Space Transportation Symposium: FY2012},
 month = {Jan},
 note = {平成24年度宇宙輸送シンポジウム (2013年1月17日-1月18日. 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)), 相模原市, 神奈川県, Space Transportation FY2012 (January 17-18, 2013. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan, Understanding of atomization properties of oxygen in coaxial jet flow around the inlet of rocket engine combustion chamber is important for CFD simulation with high fidelity. However, there is no experimental data of interfacial tension that influences the atomization properties. In this study, we conducted a Molecular Dynamics (MD) simulation for reproduction of oxygen-hydrogen interface in rocket engine combustion chamber, and then we studied the interfacial tension between liquid oxygen and gas hydrogen focusing microscopic structure of the interface., 形態: カラー図版あり, 形態: PDF, Physical characteristics: Original contains color illustrations, Physical characteristics: PDF, 資料番号: AA0061856050, レポート番号: STCP-2012-050},
 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)},
 title = {ロケットエンジン燃焼室の入口近傍を想定した酸水素界面の微視的研究},
 year = {2013}
}