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  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

超音速航空機の離陸性能最適化を含む概念設計に向けた研究

https://jaxa.repo.nii.ac.jp/records/3844
https://jaxa.repo.nii.ac.jp/records/3844
db699159-b9c1-4338-b4dd-b96bb64f898b
名前 / ファイル ライセンス アクション
AA1530023009.pdf AA1530023009.pdf (718.0 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 超音速航空機の離陸性能最適化を含む概念設計に向けた研究
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 Investigation on Supersonic Transport Conceptual Design towards Optimized Take-off Performance
著者 李家, 賢一

× 李家, 賢一

WEKO 16198

李家, 賢一

Search repository
豊田, 広祐

× 豊田, 広祐

WEKO 16199

豊田, 広祐

Search repository
郭, 東潤

× 郭, 東潤

WEKO 16200

郭, 東潤

Search repository
Rinoie, Kenichi

× Rinoie, Kenichi

WEKO 16201

en Rinoie, Kenichi

Search repository
Toyoda, Kosuke

× Toyoda, Kosuke

WEKO 16202

en Toyoda, Kosuke

Search repository
Kwak, Dongyoun

× Kwak, Dongyoun

WEKO 16203

en Kwak, Dongyoun

Search repository
著者所属
東京大学
著者所属
東京大学
著者所属
宇宙航空研究開発機構(JAXA)
著者所属(英)
en
The University of Tokyo
著者所属(英)
en
The University of Tokyo
著者所属(英)
en
Japan Aerospace Exploration Agency (JAXA)
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. 47-51, 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 One of the difficult design problems of supersonic transport is to improve both the low-speed and supersonic aerodynamic performance. This paper summarizes the authors' previous researches in this subject. First, a multi-point design method for preliminary design of supersonic transports to obtain a compromised solution at low speeds and at supersonic speeds is reviewed. Second, non-linear pitching moment characteristics which are observed at relatively high angle of attack at low speeds is discussed from design and aerodynamic points of view. The wind tunnel experimental results conducted by the authors are also described. Third, a simplified this non-linear pitching moment characteristics has been investigated and is summarized here. These methods are going to be integrated into a revised conceptual design method for supersonic transports.
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: AA1530023009
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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