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スクラムジェットエンジン性能向上に関する試み: 性能を左右する内部流剥離の範囲
https://jaxa.repo.nii.ac.jp/records/48390
https://jaxa.repo.nii.ac.jp/records/48390c07bfc5b-b00b-4e42-ba5d-6f23b4d5118f
名前 / ファイル | ライセンス | アクション |
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AA2130027017.pdf (2.1 MB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2022-02-14 | |||||
タイトル | ||||||
タイトル | スクラムジェットエンジン性能向上に関する試み: 性能を左右する内部流剥離の範囲 | |||||
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 | Trial for Performance Improvement of Scramjet Engine: Flow Separation Domain Affecting Engine Performance | |||||
著者 |
佐藤, 茂
× 佐藤, 茂× 福井, 正明× 宗像, 利彦× 渡邉, 孝宏× 髙橋, 正晴× SATO, Shigeru× FUKUI, Masaaki× MUNAKATA, Toshihiko× WATANABE, Takahiro× TAKAHASHI, Masaharu |
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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)(KSPC) | ||||||
著者所属 | ||||||
株式会社スペースサービス | ||||||
著者所属 | ||||||
株式会社日立ソリューションズ東日本 | ||||||
著者所属 | ||||||
株式会社日立ソリューションズ東日本 | ||||||
著者所属 | ||||||
株式会社日立ソリューションズ東日本 | ||||||
著者所属(英) | ||||||
en | ||||||
Kakuda Space Center, Japan Aerospace Exploration Agency (JAXA)(KSPC) | ||||||
著者所属(英) | ||||||
en | ||||||
Space Service Co., Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
Hitachi Solutions East Japan, Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
Hitachi Solutions East Japan, Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
Hitachi Solutions East Japan, Ltd. | ||||||
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53回流体力学講演会/第39回航空宇宙数値シミュレーション技術シンポジウム論文集 en : JAXA Special Publication: Proceedings of the 53rd Fluid Dynamics Conference / the 39th Aerospace Numerical Simulation Symposium 巻 JAXA-SP-21-008, p. 193-200, 発行日 2022-02-14 |
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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53回流体力学講演会/第39回航空宇宙数値シミュレーション技術シンポジウム (2021年6月30日-7月2日. 日本航空宇宙学会 : 宇宙航空研究開発機構(JAXA)オンライン会議) | |||||
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 | The 53rd Fluid Dynamics Conference / the 39th Aerospace Numerical Simulation Symposium (June 30 - July 2, 2021. The Japan Society for Aeronautical and Space Sciences : Japan Aerospace Exploration Agency (JAXA), Online meeting) | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Japan Aerospace Exploration Agency has been investigating scramjet engines in Kakuda Space Center using RamJet Engine Test Facility and others. The engine tested at the flight condition of Mach 6 showed very steep fuel distribution. The fuel injected from the vertical injector on the side wall stays near the side wall and the top wall along the engine. The steep fuel distribution is an obstacle for the engine performance completion. In order to solve the problem, the authors are focusing the influence of cowl and strut shock waves on the fuel distribution. In this paper the authors describe results of combustion calculation to compare with the test result. It is found that a flow separation occurs in the corner of internal flow, and that the separation causes inclined shock wave to promote the combustion. | |||||
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 | |||||
ISSNONLINE | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 2433-2232 | |||||
著者版フラグ | ||||||
出版タイプ | VoR | |||||
出版タイプResource | http://purl.org/coar/version/c_970fb48d4fbd8a85 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA2130027017 | |||||
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-21-008 |