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スクラムジェットエンジンにおけるストラット後縁形状と流体滞在時間
https://jaxa.repo.nii.ac.jp/records/4264
https://jaxa.repo.nii.ac.jp/records/4264d6dad80e-b582-4d7f-84e1-73b20ff52485
名前 / ファイル | ライセンス | アクション |
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61958024.pdf (1.1 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 | スクラムジェットエンジンにおけるストラット後縁形状と流体滞在時間 | |||||
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 | Strut Tail Shape and Fluid Residence Time in a Scramjet Engine | |||||
著者 |
佐藤, 茂
× 佐藤, 茂× 渡邉, 孝宏× 福井, 正明× 宗像, 利彦× Sato, Shigeru× Watanabe, Takahiro× Fukui, Masaaki× Munakata, Toshihiko |
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著者所属 | ||||||
宇宙航空研究開発機構角田宇宙センター(JAXA) | ||||||
著者所属 | ||||||
日立東日本ソリューションズ | ||||||
著者所属 | ||||||
スペースサービス | ||||||
著者所属 | ||||||
日立東日本ソリューションズ | ||||||
著者所属(英) | ||||||
en | ||||||
Kakuda Space Center, Japan Aerospace Exploration Agency (JAXA)(KSPC) | ||||||
著者所属(英) | ||||||
en | ||||||
Hitachi East Japan Solutions | ||||||
著者所属(英) | ||||||
en | ||||||
Space Service | ||||||
著者所属(英) | ||||||
en | ||||||
Hitachi East Japan Solutions | ||||||
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 en : JAXA Special Publication: Proceedings of 44th Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2012 巻 JAXA-SP-12-010, p. 145-150, 発行日 2013-03-29 |
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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44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2012 (2012年7月5日-6日. 富山国際会議場大手町フォーラム), 富山市, 富山県 | |||||
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 | 44th Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2012 (July 5-6, 2012. Toyama International Conference Center), Toyama Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Japan Aerospace Exploration Agency (JAXA) has been investigating scramjet engines in Kakuda Space Center using Ram Jet Engine Test Facility (RJTF) et al. The engine tested at the flight condition of Mach 6 in RJTF showed very important characteristics depending on internal geometry. The authors found in the result of CFD research that a “hot triangle” is caused by 3-dimensional interaction of the cowl shock wave and the strut shock wave and that the hot triangle contributes to intensive combustion transition. Based on this hot triangle, an engine configuration with boat-tail strut is compared to that with 5/5 height strut that showed good thrust performance in the engine test. CFD is carried out to solve the inner air flow, and the residence time distribution behind the strut is made clear. It is found that the configuration with boat-tail strut can produce the outstanding residence time, improve the fuel distribution in the engine cross"" section and be worth being calculated in full-detail CFD. | |||||
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: AA0061958024 | |||||
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-12-010 |