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動的失速の最適制御
https://jaxa.repo.nii.ac.jp/records/37244
https://jaxa.repo.nii.ac.jp/records/37244da240871-1a98-4066-b6eb-df5284e8c17b
Item type | 会議発表論文 / Conference Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 動的失速の最適制御 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 動的失速制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 最適剥離制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 境界層剥離制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 翼剥離制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 翼ピッチング | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 壁面噴流吹出 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 吹出量低減 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | dynamic stall control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | optimal separation control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | boundary layer separation control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | airfoil separation control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | airfoil pitching | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | wall jet blowing | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | blowing amount reduction | |||||
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 | |||||
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 | Optimal control of dynamic stall | |||||
著者 |
望月, 修
× 望月, 修× Mochizuki, Osamu |
|||||
著者所属 | ||||||
北海道大学 工学部 | ||||||
著者所属(英) | ||||||
en | ||||||
Hokkaido University Faculty 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 en : Special Publication of National Aerospace Laboratory 巻 40, p. 81-82, 発行日 1999-01 |
|||||
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 | 30 Sep.-1 Oct. 1997 (21st). 26-27 Mar. 1998 (22nd) | |||||
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 | 30 Sep.-1 Oct. 1997 (21st). 26-27 Mar. 1998 (22nd) | |||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | ピッチングアップおよびピッチングダウン運動中のNACA0020翼の動的失速を翼前縁近傍の薄スリットから上面に沿った壁面噴流によって制御した。レイノルズ数は翼弦cと主流速度Uに基づき、8.6×10(exp 4)である。この翼は、低減ピッチ速度Ω=ωc/(2U)(ωはピッチ速度(rad/s))が0.012で、迎角が0から30度の間のピッチングアップおよびピッチングダウン運動に耐えた。1周期中の吹出し量は一定吹出しの場合の47%で、比例吹出しの場合の78%である。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Dynamic stall of a NACA0020 airfoil in pitching up and pitching down motion is controlled by a wall jet along the upper surface from a thin slit near the leading edge. The Reynolds number, based on the airfoil chord, c, and the free stream velocity, U, is 8.6 x 10(exp 4). The airfoil underwent pitching up and pitching down motion between angle of attack of 0 to 30 degrees at a reduced pitch rate, Omega (equals to omega x c/(2U), where omega is pitch rate (rad/s)) of 0.012. The amount of the injection during one period is 47 percent of that of the constant injection and 78 percent of that of the proportional injection. | |||||
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: AA0001655021 | |||||
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-40 |