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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
https://jaxa.repo.nii.ac.jp/records/16487
https://jaxa.repo.nii.ac.jp/records/164875902db1f-7489-4300-85a2-1f7d20c300de
Item type | 会議発表論文 / Conference Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 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 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Solid propellant | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Casting process | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Slurry flow | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Solid rocket | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_5794 | |||||
資源タイプ | conference paper | |||||
アクセス権 | ||||||
アクセス権 | metadata only access | |||||
アクセス権URI | http://purl.org/coar/access_right/c_14cb | |||||
その他のタイトル(英) | ||||||
その他のタイトル | About correlation between isochronous surface and local burning rate in the intermittent inflow analysis of solid propellant slurry | |||||
著者 |
高田, 智弘
× 高田, 智弘× 平岡, 克己× 北川, 幸樹× 福永, 美保子× 淺川, 弘也× 松浦, 新× 嶋田, 徹× Takada, Tomohiro× Hiraoka, Katsumi× Kitagawa, Koki× Fukunaga, Mihoko× Asakawa, Hiroya× Matsuura, Shin× Shimada, Toru |
|||||
著者所属 | ||||||
東海大学 | ||||||
著者所属 | ||||||
東海大学 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構宇宙科学研究所 (JAXA)(ISAS) | ||||||
著者所属 | ||||||
IHIエアロスペース | ||||||
著者所属 | ||||||
IHIエアロスペース | ||||||
著者所属 | ||||||
IHIエアロスペース | ||||||
著者所属 | ||||||
宇宙航空研究開発機構宇宙科学研究所 (JAXA)(ISAS) | ||||||
著者所属(英) | ||||||
en | ||||||
Tokai University | ||||||
著者所属(英) | ||||||
en | ||||||
Tokai University | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) | ||||||
著者所属(英) | ||||||
en | ||||||
IHI Aerospace | ||||||
著者所属(英) | ||||||
en | ||||||
IHI Aerospace (IA) | ||||||
著者所属(英) | ||||||
en | ||||||
IHI Aerospace (IA) | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構宇宙科学研究所 | |||||
出版者(英) | ||||||
出版者 | Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) | |||||
書誌情報 |
平成22年度宇宙輸送シンポジウム: 講演集録 en : Proceedings of Space Transportation Symposium: FY2010 発行日 2011 |
|||||
会議概要(会議名, 開催地, 会期, 主催者等) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 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 | |||||
会議概要(会議名, 開催地, 会期, 主催者等)(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Space Transportation FY2010 (January 20-21, 2011. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)(ISAS)), Sagamihara, Kanagawa Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 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. | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: カラー図版あり | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: CD-ROM1枚 | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Physical characteristics: Original contains color illustrations | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Note: One CD-ROM | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN10324301 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0065073040 |