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横流れ不安定場の設計と制御
https://jaxa.repo.nii.ac.jp/records/36730
https://jaxa.repo.nii.ac.jp/records/36730735dcc77-158f-43fa-932d-0e3eab1b24f7
名前 / ファイル | ライセンス | アクション |
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nalsp0028001.pdf (369.3 kB)
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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 | 横流れ不安定場の設計と制御 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 3次元境界層遷移 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 遷移過程 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 流れ設計 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 能動制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 層流制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 遷移遅れ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 横流れ不安定場 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 境界流 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 偏揺れ平板 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 非定常攪乱 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 高周波攪乱 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 流れ場 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 風洞実験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 風速 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 境界層厚さ | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | three dimensional boundary layer transition | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | transition process | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flow design | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | active control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | laminar flow control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | transition delay | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | crossflow instability field | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | boundary layer flow | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | yawed flat plate | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | unsteady disturbance | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | high frequency disturbance | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flow field | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | wind tunnel test | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | wind velocity | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | boundary layer thickness | |||||
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 | Design and control of crossflow instability field | |||||
著者 |
小濱, 泰昭
× 小濱, 泰昭× 小野寺, 達也× Kohama, Yasuaki× Onodera, Tatsuya |
|||||
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 | ||||||
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 en : Special Publication of National Aerospace Laboratory 巻 28, p. 3-6, 発行日 1995-09 |
|||||
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 | 航空宇宙技術研究所 Sep. 1994 (15th). Mar. 1995 (16th) 東京 日本 | |||||
会議概要(会議名, 開催地, 会期, 主催者等)(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | National Aerospace Laboratory Sep. 1994 (15th). Mar. 1995 (16th) Tokyo Japan | |||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 横流れの支配的な境界層を制御するために、排除体を伴った偏揺れ平板より成る実験モデルを設計し、遷移過程を詳細に測定した。結果は、偏揺れ平板について測定した後退翼境界層流と極めて良く似た複雑な流れ構造を示した。静的横流れ渦、1次非定常横流れの不安定性、高周波2次モードなども測定した。これらの結果より、新しく設計した実験モデルは、後退翼とほぼ同様の横流れ不安定場を与えることができると言える。将来、偏揺れ平板境界層に分配吸入を適用する事で、横流れの不安定場の制御が達成できると思われる。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | In order to control crossflow dominant boundary layers, experimental model, which is composed from yawed flat plate with displacement body, is designed and transition process is measured in detail. Results showed that complicated flow structure which is quite similar to that of swept wing boundary layer flow is measured on the yawed flat plate. Stationary crossflow vortices, primary unsteady crossflow instability, high frequency secondary mode are also measured. From these results, it can be said that newly designed experimental model provides almost same crossflow instability field as a swept wing. Control of crossflow instability field will be performed in the future by applying distributed suction on a yawed flat plate boundary layer. | |||||
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: AA0000109001 | |||||
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-28 |