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["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: 質量流率との対比"], "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. 2013
  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. 2013
  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. 2013年度
  4. JAXA-SP-13-011 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

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: 質量流率との対比

https://jaxa.repo.nii.ac.jp/records/4027
https://jaxa.repo.nii.ac.jp/records/4027
075386ce-296c-4f83-bc26-b012170d0d28
名前 / ファイル ライセンス アクション
62268027.pdf 62268027.pdf (809.3 kB)
Item type 会議発表論文 / Conference Paper(1)
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燃料最適化分布に向けた検討: 質量流率との対比
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 Study on Optimization of Fuel Injection Distribution in a Scramjet Engine: Comparison to Mass Flux
著者 佐藤, 茂

× 佐藤, 茂

WEKO 17310

佐藤, 茂

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渡邉, 孝宏

× 渡邉, 孝宏

WEKO 17311

渡邉, 孝宏

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福井, 正明

× 福井, 正明

WEKO 17312

福井, 正明

Search repository
宗像, 利彦

× 宗像, 利彦

WEKO 17313

宗像, 利彦

Search repository
Sato, Shigeru

× Sato, Shigeru

WEKO 17314

en Sato, Shigeru

Search repository
Watanabe, Takahiro

× Watanabe, Takahiro

WEKO 17315

en Watanabe, Takahiro

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Fukui, Masaaki

× Fukui, Masaaki

WEKO 17316

en Fukui, Masaaki

Search repository
Munakata, Toshihiko

× Munakata, Toshihiko

WEKO 17317

en Munakata, Toshihiko

Search repository
著者所属
宇宙航空研究開発機構宇宙輸送ミッション本部宇宙輸送系推進技術研究開発センター(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
Space Transportation Propulsion Research and Development Center, Space Transportation Mission Directorate, Japan Aerospace Exploration Agency (JAXA)
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: 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. 151-156, 発行日 2014-03-31
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 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. CFD has been carried out to solve the inner air flow, and some concepts for the design method have been found by the authors. This time, mass flux (density times velocity) distributions in the engine inner flow is calculated for two engine configurations. One is an engine configuration with rectangular-tailed strut which showed the good performance in the engine test at RJTF, and the other one is a virtual engine configuration with boat-tail strut which will be an improved configuration of the former. CFD results showed that the mass flux distribution is better than that of configuration with rectangular-tailed strut. Discussion on the better fuel distribution is described based on the result of mass flux distributions in the two engine configurations in this paper.
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: AA0062268027
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
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