@inproceedings{oai:jaxa.repo.nii.ac.jp:00016731,
 author = {津田, 伸一 and 越, 光男 and 坪井, 伸幸 and 山西, 伸宏 and Tsuda, Shinichi and Koshi, Mitsuo and Tsuboi, Nobuyuki and Yamanishi, Nobuhiro},
 book = {宇宙輸送シンポジウム: 講演集録, Proceedings of Space Transportation Symposium},
 month = {},
 note = {平成20年度宇宙輸送シンポジウム(2009年1月19日-20日, 宇宙航空研究開発機構宇宙科学研究本部), In this study, we conducted a semi-empirical Molecular Dynamics (MD) simulation to estimate the interfacial tension between liquid oxygen and gas hydrogen around the inlet of LE-5B engine chamber. Although the calculation results in this paper were only obtained at a sub-critical region of oxygen, the present method can be extended to the region around its critical point or the supercritical region., 形態: カラー図版あり, 資料番号: AA0064292038},
 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)},
 title = {ロケットエンジン同軸型噴射器近傍の熱物性予測},
 volume = {平成20年度},
 year = {2009}
}