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ボルテックス・ジェネレーターによる翼前縁フラップ ヒンジラインの剥離制御に関する実験研究
https://jaxa.repo.nii.ac.jp/records/21690
https://jaxa.repo.nii.ac.jp/records/216907dfcb73f-05e2-479a-9f8e-e96193249e82
Item type | 学術雑誌論文 / Journal Article(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2016-03-28 | |||||
タイトル | ||||||
タイトル | ボルテックス・ジェネレーターによる翼前縁フラップ ヒンジラインの剥離制御に関する実験研究 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Vortex Generator | |||||
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 | Flow Control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | High-Lift Device | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Aerodynamic Performance | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_6501 | |||||
資源タイプ | journal article | |||||
アクセス権 | ||||||
アクセス権 | metadata only access | |||||
アクセス権URI | http://purl.org/coar/access_right/c_14cb | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Experimental Investigation of Vortex Generators for Flow Separation Control on the Hinge Line of Leading-Edge Flap | |||||
著者 |
雷, 忠
× 雷, 忠× 滝沢, 啓介× 郭, 東潤× 野口, 正芳× Lei, Zhong× Takizawa, Keisuke× Kwak, Dongyoun× Noguchi, Masayoshi |
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出版者 | ||||||
出版者 | Japan Society for Aeronautical and Space Sciences | |||||
出版者(英) | ||||||
出版者 | 日本航空宇宙学会 | |||||
書誌情報 |
日本航空宇宙学会論文集 en : Journal of the Japan Society for Aeronautical and Space Sciences 巻 64, 号 1, p. 35(35)-40(40), 発行日 2016-02-05 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Experiments were conducted to investigate effects of vortex generators on flow separation for a cranked-arrow wing at a low speed wind tunnel. A kind of delta-shaped vortex generator was applied to control the boundary layer separation flow near the hinge line of the deflected leading-edge flap. Effects on aerodynamic performance were estimated according to the force measurement data and flow patterns were observed by oilflow visualization technique. It was found that the drag coefficient was reduced and the lift-to-drag ratio was improved as the vortex generator was suitably equipped on the hinge line of the leading-edge flap. It was observed that swirling longitude vortices were generated from the leading-edge of the vortex generator, and thus suppressed the boundary layer flow separation. | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: 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 illustrations | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1344-6460 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11307372 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: DS1540529006 |