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パルスデトネーションエンジンの推力性能推算に関する研究: 外部流の影響
https://jaxa.repo.nii.ac.jp/records/16608
https://jaxa.repo.nii.ac.jp/records/1660853c663fb-dc37-4c1e-af67-c6c19d8fb6cc
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 | パルスデトネーションエンジンの推力性能推算に関する研究: 外部流の影響 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Pulse Detonation Engine | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Numerical Simulation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Converging Diverging Nozzle | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Ambient Flow | |||||
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 | Numerical Study for Propulsive Performance on Pulse Detonation Engine | |||||
著者 |
江連, 諒介
× 江連, 諒介× 坪井, 伸幸× 林, 光一× 山田, 英助× Ezure, Ryosuke× Tsuboi, Nobuyuki× Hayashi, A. Koichi× Yamada, Eisuke× Tangirala, Venkat E. |
|||||
著者所属 | ||||||
青山学院大学理工学部機械創造学科 | ||||||
著者所属 | ||||||
九州工業大学大学院工学研究院 機械知能工学研究系機械工学部門 | ||||||
著者所属 | ||||||
青山学院大学理工学部機械創造学科 | ||||||
著者所属 | ||||||
青山学院大学理工学部機械創造学科 | ||||||
著者所属(英) | ||||||
en | ||||||
Department of Mechanical Engineering, College of Science and Engineering, Aoyama Gakuin University | ||||||
著者所属(英) | ||||||
en | ||||||
Department of Mechanical and Control Engineering, Faculty of Engineering, Kyushu Institute of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Department of Mechanical Engineering, Aoyama Gakuin University | ||||||
著者所属(英) | ||||||
en | ||||||
Department of Mechanical Engineering, College of Science and Engineering, Aoyama Gakuin University | ||||||
著者所属(英) | ||||||
en | ||||||
General Electric Company(GE) | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構宇宙科学研究本部 | |||||
出版者(英) | ||||||
出版者 | Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
宇宙輸送シンポジウム: 講演集録 en : Proceedings of Space Transportation Symposium 巻 平成21年度, 発行日 2010-01 |
|||||
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21年度宇宙輸送シンポジウム(2010年1月14日-15日, 宇宙航空研究開発機構宇宙科学研究本部) | |||||
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 Symposium (January 14-15, 2010. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)), Sagamihara, Kanagawa Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | This paper presents effect of ambient flow for propulsive performance and the valve operations on H2/Air Pulse Detonation Engine using the system-level modeling, multi-cycle and automatic valve timing with detail chemical reaction model. The present results show that effect of ambient flow appears on the propulsive performance when the jet becomes highly over-expanded. However the flow doesn't influence the cycle time and the valve operations. | |||||
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: AA0064741038 |