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はく離抑制の最適化
https://jaxa.repo.nii.ac.jp/records/38109
https://jaxa.repo.nii.ac.jp/records/381090750dcfb-60eb-47e9-9b99-6b6a4bb9e164
名前 / ファイル | ライセンス | アクション |
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nalsp0054017.pdf (2.1 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 | はく離抑制の最適化 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 剥離流 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 2次元モデル | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 速度分布 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 流れの可視化 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 境界層吸引 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 仰角 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 最適化 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | separated flow | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | two dimensional model | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | velocity distribution | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flow visualization | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | boundary layer suction | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | angle of attack | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | optimization | |||||
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 | Adequate control for suppression of separation | |||||
著者 |
石川, 仁
× 石川, 仁× 望月, 修× Ishikawa, Hitoshi× Mochizuki, Osamu |
|||||
著者所属 | ||||||
北海道大学 大学院工学研究科 | ||||||
著者所属 | ||||||
北海道大学 大学院工学研究科 | ||||||
著者所属(英) | ||||||
en | ||||||
Hokkaido University Graduate School of Engineering | ||||||
著者所属(英) | ||||||
en | ||||||
Hokkaido University Graduate School of Engineering | ||||||
出版者 | ||||||
出版者 | 航空宇宙技術研究所 | |||||
出版者(英) | ||||||
出版者 | National Aerospace Laboratory (NAL) | |||||
書誌情報 |
航空宇宙技術研究所特別資料: 第28回境界層遷移の解明と制御研究会講演論文集 en : Special Publication of National Aerospace Laboratory: Proceedings of the 28th NAL Workshops on Investigation and Control of Boundary-Layer Transition 巻 54, p. 65-68, 発行日 2002-01 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | An optimum condition for suppression of separation was investigated experimentally. A two-dimensional airfoil of NACA0015 with a large angle of attack was used to generate a separation. The flow near the surface was sucked in by four suction-cells independently. The cells were arranged in line at the center of the span. Several combinations of active cells and their suction volumes were tested to obtain the minimum power consumption of suction required for the suppression of separation. The extent of suppression was judged by the velocity profile obtained by flow visualization near the trailing edge. Each cell showed an optimum value of the suction volume for a specific angle of attack with separation. It was found that the suction performance of a cell was greatest if the cell was placed just in front of the separation point. A large saving in suction power was achieved when the cells were placed just in front of and the separation point. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0289-260X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN10097345 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0032827017 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: NAL SP-54 |