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アイテム
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地面効果翼機の性能向上に関する研究
https://jaxa.repo.nii.ac.jp/records/6203
https://jaxa.repo.nii.ac.jp/records/620349a61b1e-1658-4370-905b-f436a47bf8ae
名前 / ファイル | ライセンス | アクション |
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49208021.pdf (1.1 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 | 地面効果翼機の性能向上に関する研究 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 地面効果機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 空力特性 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 改良 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | エアロトレイン | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | WIG翼型 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 設計最適化 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 後退翼 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 境界層剥離 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 剥離流 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | ground effect machine | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aerodynamic characteristic | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | improvement | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aerotrain | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | WIG aerofoil | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | design optimization | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | sweptback wing | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | boundary layer separation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | separated flow | |||||
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 performance improvement of Aero-Train | |||||
著者 |
Yoon, D. H.
× Yoon, D. H.× 鈴木, 和幸× 遠藤, 秀之× 小濱, 泰昭× Yoon, D. H.× Suzuki, Kazuyuki× Endo, Hideyuki× Kohama, Yasuaki |
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著者所属 | ||||||
東北大学流体科学研究所 | ||||||
著者所属 | ||||||
東北大学流体科学研究所 | ||||||
著者所属 | ||||||
東北大学流体科学研究所 | ||||||
著者所属 | ||||||
東北大学流体科学研究所 | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Fluid Science, Tohoku University | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Fluid Science, Tohoku University | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Fluid Science, Tohoku University | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Fluid Science, Tohoku University | ||||||
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: 境界層遷移の解明と制御研究会講演論文集 第35回・第36回 en : JAXA Special Publication: Proceedings of the 35th and 36th JAXA Workshops on Investigation and Control of Boundary-Layer Transition 巻 JAXA-SP-05-012, p. 67-68, 発行日 2006-02-01 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Aerodynamic performance improvement of the Aero-Train has been conducted both experimentally and numerically. Suction side of the WIG aerofoil tend to separate, because of the existence of the ground surface, and also wing-wing, wing-fuselage interactions appears. Those flow separations limit the lift to drag ratio performance. In order to improve overall Aero-Train performance, optimum wing configuration determination, blowing from the pressure side, and swept forward guide wing configuration are studied. | |||||
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: AA0049208021 | |||||
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-05-012 |