@inproceedings{oai:jaxa.repo.nii.ac.jp:00016480,
 author = {本江, 幹朗 and 嶋田, 徹 and Motoe, Mikiro and Shimada, Toru},
 book = {平成22年度宇宙輸送シンポジウム: 講演集録, Proceedings of Space Transportation Symposium: FY2010},
 month = {},
 note = {平成22年度宇宙輸送シンポジウム(2011年1月20-21日. 宇宙航空研究開発機構宇宙科学研究所), 相模原市, 神奈川県, Space Transportation FY2010 (January 20-21, 2011. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)(ISAS)), Sagamihara, Kanagawa Japan, For the hybrid engine, it has been proven by ground and flight experiments that the fuel regression characteristic can be improved by tangential injection of the oxidizer. The mechanism, however, of this enhancement has not yet been well-understood. The goal of this study is to establish most efficient way of this type of injection, as well as to better understand the physical mechanism of the effect, by means of Computational Fluid Dynamics., 形態: カラー図版あり, 形態: CD-ROM1枚, Physical characteristics: Original contains color illustrations, Note: One CD-ROM, 資料番号: AA0065073033},
 publisher = {宇宙航空研究開発機構宇宙科学研究所, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)},
 title = {酸化剤旋回流型ハイブリッドロケット燃焼室内における非燃焼流れ場の検証},
 year = {2011}
}