@inproceedings{oai:jaxa.repo.nii.ac.jp:00016487,
 author = {高田, 智弘 and 平岡, 克己 and 北川, 幸樹 and 福永, 美保子 and 淺川, 弘也 and 松浦, 新 and 嶋田, 徹 and Takada, Tomohiro and Hiraoka, Katsumi and Kitagawa, Koki and Fukunaga, Mihoko and Asakawa, Hiroya and Matsuura, Shin 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, The purpose of this study is to understand the effects slurry properties or casting methods on flow and the investigation whether angles between isochronous surfaces by casting and burning direction is related to local burning rates by the propellant strand burn test. Three-dimensional casting processes were simulated with ANSYS FLUENT and the results were discussed. Newtonian and non-Newtonian fluids were assumed. Casting methods were continuous inflow and intermittent inflow. We obtained that intermittent inflow effects were appeared dominantly in case of a non-Newtonian fluid and intermittent inflow and that burning rates to increase as angles betweeen isochronous surfaces and burning direction increased., 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: AA0065073040},
 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 = {固体推進薬スラリ間欠流入解析における等時刻面と局所燃焼速度の相関について},
 year = {2011}
}