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ロケット実験機の空力データベース概要
https://jaxa.repo.nii.ac.jp/records/5444
https://jaxa.repo.nii.ac.jp/records/544457f657fc-1aee-41b1-b111-f17145d785b3
名前 / ファイル | ライセンス | アクション |
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64239008.pdf (10.3 MB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | ロケット実験機の空力データベース概要 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Database, Aerodynamics, Supersonic Transport | |||||
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 | Aerodynamic database of the supersonic experimental airplane (NEXST-1) in JAXA | |||||
著者 |
郭, 東潤
× 郭, 東潤× 黒田, 文武× 伊藤, 健× 徳川, 直子× 石川, 敬掲× 中畠, 浩二× 野口, 正芳× 上田, 良稲× 吉田, 憲司× Kwak, Dong-Youn× Kuroda, Fumitake× Ito, Takeshi× Tokugawa, Naoko× Ishikawa, Hirotaka× Nakahata, Koji× Noguchi, Masayoshi× Ueda, Yoshine× Yoshida, Kenji |
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著者所属 | ||||||
宇宙航空研究開発機構 | ||||||
著者所属 | ||||||
菱友システムズ | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 | ||||||
著者所属 | ||||||
三向ソフトウェア開発 | ||||||
著者所属 | ||||||
三向ソフトウェア開発 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 | ||||||
著者所属 | ||||||
東京ビジネスサービス | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Ryoyu Systems | ||||||
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 | ||||||
Sanko Soft | ||||||
著者所属(英) | ||||||
en | ||||||
Sanko Soft | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo Business Service | ||||||
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 | |||||
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: 小型超音速実験機(ロケット実験機)飛行実験データ解析完了報告 en : JAXA Special Publication 巻 JAXA-SP-08-008, 発行日 2009-02-27 |
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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 | 小型超音速実験機(ロケット実験機)飛行実験データ解析完了報告会(平成20年7月10日. 東京大学山上会館) | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | An aerodynamic database system named the NEXST-DB was constructed by JAXA to contribute on the aerospace research area in Japan. A number of aerodynamic data on the supersonic experimental airplane (NEXST-1) can be accumulated by the NEXST project. Three kinds of data of the pressure distribution, aerodynamic forces and boundary layer transitions were carried on the NEXST-DB. These aerodynamic data were obtained from the flight test, CFD analysis and wind tunnel tests. Furthermore, the geometry data of the NEXST-1 and the grid data for CFD analysis were also carried on the NEXST-DB. Those data can download on the website. | |||||
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 | |||||
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: AA0064239008 | |||||
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-08-008 |