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ローテーティングデトネーションエンジンの数値解析: 厚み方向の影響とスケール効果
https://jaxa.repo.nii.ac.jp/records/4006
https://jaxa.repo.nii.ac.jp/records/4006c7a727f2-d688-4fd5-b788-84e5aff8ed31
名前 / ファイル | ライセンス | アクション |
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62268006.pdf (1.2 MB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | ローテーティングデトネーションエンジンの数値解析: 厚み方向の影響とスケール効果 | |||||
言語 | ||||||
言語 | jpn | |||||
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 | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Numerical Analysis of Rotating Detonation Engine: Effect of Thickness direction and Scale effect | |||||
著者 |
図斉, 健太
× 図斉, 健太× 桜澤, 歩× 朝原, 誠× 山田, 英助× 林, 光一× 坪井, 伸幸× Zusai, Kenta× Sakurazawa, Ayumu× Asahara, Makoto× Yamada, Eisuke× Hayashi, Koichi× Tsuboi, Nobuyuki |
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著者所属 | ||||||
青山学院大学大学院理工学研究科理工学専攻機械創造コース | ||||||
著者所属 | ||||||
青山学院大学大学院理工学研究科理工学専攻機械創造コース | ||||||
著者所属 | ||||||
青山学院大学大学院理工学研究科理工学専攻機械創造コース | ||||||
著者所属 | ||||||
青山学院大学大学院理工学研究科理工学専攻機械創造コース | ||||||
著者所属 | ||||||
青山学院大学大学院理工学研究科理工学専攻機械創造コース | ||||||
著者所属 | ||||||
九州工業大学大学院工学研究院 | ||||||
著者所属(英) | ||||||
en | ||||||
Mechanical Engineering Course, Graduate School of Science and Engineering, Aoyama Gakuin University | ||||||
著者所属(英) | ||||||
en | ||||||
Mechanical Engineering Course, Graduate School of Science and Engineering, Aoyama Gakuin University | ||||||
著者所属(英) | ||||||
en | ||||||
Mechanical Engineering Course, Graduate School of Science and Engineering, Aoyama Gakuin University | ||||||
著者所属(英) | ||||||
en | ||||||
Mechanical Engineering Course, Graduate School of Science and Engineering, Aoyama Gakuin University | ||||||
著者所属(英) | ||||||
en | ||||||
Mechanical Engineering Course, Graduate School of Science and Engineering, Aoyama Gakuin University | ||||||
著者所属(英) | ||||||
en | ||||||
Graduate School of Engineering, Kyushu Institute of Technology | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構(JAXA) | |||||
出版者(英) | ||||||
出版者 | Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
宇宙航空研究開発機構特別資料: 第45回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2013論文集 en : JAXA Special Publication 巻 JAXA-SP-13-011, p. 29-34, 発行日 2014-03-31 |
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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 | 第45回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2013 (2013年7月4日-5日. タワーホール船堀), 東京 | |||||
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 | 45th Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2013 (July 4-5, 2013. Tower Hall Funabori), Tokyo, Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The study about the detonation engine which is a high-performance pusher using a characteristic of the detonation is performed with many institutes. RDE is one of the detonation engines where detonation propagates to circumferential direction in annular combustion chamber. RDE can get a continuous thrust and can continue transmitting a detonation. However, there are many problems that should solve sustaining of the propagation. In this study, we consider detonation propagation mechanism of RDE, and the transverse wave dynamics and its radial direction mechanism are important to control detonation propagation. We focus on the transverse wave occurrence and propagation, and its detail of mechanism of radial direction by 3-D numerical analysis. We report the influence of a scale effect provided using a scale based on the actual machine size of the device of a past experiment. | |||||
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(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Physical characteristics: Original contains color illustrations | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1349-113X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11984031 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0062268006 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: JAXA-SP-13-011 |