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飛行実験における力及び圧力特性解析
https://jaxa.repo.nii.ac.jp/records/5441
https://jaxa.repo.nii.ac.jp/records/54414ca9c990-fdc3-4a98-bd4c-2c02200c4df6
名前 / ファイル | ライセンス | アクション |
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64239005.pdf (4.6 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 | 飛行実験における力及び圧力特性解析 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Aerodynamic Force, Pressure distribution, Flight test, 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 forces and pressure distributions of the supersonic experimental airplane (NEXST-1) on the flight test | |||||
著者 |
郭, 東潤
× 郭, 東潤× 中畠, 浩二× 石川, 敬掲× 野口, 正芳× 吉田, 憲司× Kwak, Dong-Youn× Nakahata, Koji× Ishikawa, Hirotaka× Noguchi, Masayoshi× Yoshida, Kenji |
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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 | ||||||
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 | ||||||
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 | ||||||
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 | A supersonic flight test was conducted by JAXA to validate the aerodynamic design technology of the supersonic transport. Surface static pressure distributions and aerodynamic forces of the supersonic experimental airplane (NEXST-1) were obtained by the flight test. Flight test data were analyzed with high accuracy, and were evaluated by comparing with the CFD analysis. Relatively good agreements were observed with the flight test results and the CFD results. The validity of the drag reduction design concepts and design tools were confirmed from the flight test. | |||||
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: AA0064239005 | |||||
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 |