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"publish_status": "0", "recid": "3851", "relation": {}, "relation_version_is_last": true, "title": ["スクラムジェットエンジン燃料最適化分布に向けた検討: 燃料偏在の補正法"], "weko_shared_id": -1}
  1. JAXA出版物(シリーズ別)
  2. 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
  3. 2014
  1. シンポジウム・研究会
  2. 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
  3. 2014
  1. コンテンツタイプ
  2. 会議発表論文/会議発表用資料 (Conference Paper/Presentation)
  1. JAXA出版物(種類別)
  2. 特別資料 Special Publication(略称:SP)
  3. 2014年度
  4. JAXA-SP-14-010 第46回流体力学講演会/第32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

スクラムジェットエンジン燃料最適化分布に向けた検討: 燃料偏在の補正法

https://jaxa.repo.nii.ac.jp/records/3851
https://jaxa.repo.nii.ac.jp/records/3851
53d37c30-d738-4bce-a95d-b502cab3912f
名前 / ファイル ライセンス アクション
AA1530023016.pdf AA1530023016.pdf (915.6 kB)
Item type 会議発表論文 / Conference Paper(1)
公開日 2015-04-28
タイトル
タイトル スクラムジェットエンジン燃料最適化分布に向けた検討: 燃料偏在の補正法
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 Consideration for Optimization of Fuel Distribution in a Scramjet Engine: Compensation for Steep Distribution
著者 佐藤, 茂

× 佐藤, 茂

WEKO 16238

佐藤, 茂

Search repository
福井, 正明

× 福井, 正明

WEKO 16239

福井, 正明

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渡邉, 孝宏

× 渡邉, 孝宏

WEKO 16240

渡邉, 孝宏

Search repository
宗像, 利彦

× 宗像, 利彦

WEKO 16241

宗像, 利彦

Search repository
Sato, Shigru

× Sato, Shigru

WEKO 16242

en Sato, Shigru

Search repository
Fukui, Masaaki

× Fukui, Masaaki

WEKO 16243

en Fukui, Masaaki

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Watanabe, Takahiro

× Watanabe, Takahiro

WEKO 16244

en Watanabe, Takahiro

Search repository
Munakata, Toshihiko

× Munakata, Toshihiko

WEKO 16245

en Munakata, Toshihiko

Search repository
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(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.
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46回流体力学講演会/第32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 46th Fluid Dynamics Conference / 32nd Aerospace Numerical Simulation Symposium

巻 JAXA-SP-14-010, p. 87-92, 発行日 2015-03-25
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46回流体力学講演会/第32回航空宇宙数値シミュレーション技術シンポジウム (2014年7月3日-4日. 弘前文化センター), 弘前市, 青森県
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 46th Fluid Dynamics Conference / 32nd Aerospace Numerical Simulation Symposium (July 3-4, 2014. Hirosaki Bunka Center), Hirosaki, Aomori, Japan
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 (RJTF) et al. 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 tap 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 shock wave on the fuel distribution. Being based on the aerodynamic effect of strut found by authors, the strut fuel injection is proposed to improve the fuel distribution. In the result of simulation by visualizing the steam lines in CFD, it is found that the strut fuel injection might be able to spread the fuel in the engine cross section much more than the side wall injection.
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: AA1530023016
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-14-010
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