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CFD模擬によるスクラムジェットエンジン内の諸燃焼形態について
https://jaxa.repo.nii.ac.jp/records/47331
https://jaxa.repo.nii.ac.jp/records/473311c453fd7-fdd2-4895-a22f-be340b9eda92
名前 / ファイル | ライセンス | アクション |
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AA2030013010.pdf (2.8 MB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2021-02-08 | |||||
タイトル | ||||||
タイトル | CFD模擬によるスクラムジェットエンジン内の諸燃焼形態について | |||||
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 | Various Combustion Modes in a Scramjet Engine Simulated by CFD | |||||
著者 |
小寺, 正敏
× 小寺, 正敏× 富岡, 定毅× 宗像, 利彦× 三谷, 徹× KODERA, Masatoshi× TOMIOKA, Sadatake× MUNAKATA, Tohsihiko× MITANI, Toru |
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著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
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 | ||||||
- | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Hitachi Solutions East Japan, Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
- | ||||||
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: 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2020オンライン論文集 en : JAXA Special Publication: Proceedings of Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2020 Online 巻 JAXA-SP-20-008, p. 69-78, 発行日 2021-02-08 |
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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 | 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2020オンライン (2020年9月28日-30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 | Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2020 Online (September 28-30, 2020. 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 | In this study, three-dimensional CFD analysis was carried out for a hydrogen fueled scramjet engine tested at the Ramjet Engine Test Facility (RJTF) under Mach 6 flight conditions. As a result, for a fuel equivalence ratio of 0.3, various combustion modes were observed depending on the combustor wall temperature, operation of igniter, presence of water vapor in air conditions as well as initial solutions. Those combustion modes were classified into 4 groups: Partially-anchored, Fully-anchored, Partially-blow-off and Blow-off modes, from the point of view of flame anchor point, and were investigated in detail. In addition, it was demonstrated that several combustion phenomena occurred in the RJTF tests corresponded to one of them. | |||||
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: AA2030013010 | |||||
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-20-008 |