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タイトル: 一様流中に置かれた翼まわりの流れの周期的変動現象に関する実験的研究
その他のタイトル: Experimental Investigation of the Periodic Fluctuating Flow around NACA0008 and NACA0015 Blades in Uniform Inflow.
著者: 林, 秀千人 / 池田, 昌浩 / 児玉, 好雄
著者(別表記) : Hayashi, Hidechito / Ikeda, Masahiro / Kodama, Yoshio
発行日: 1990年 7月
出版者: 長崎大学工学部 / Faculty of Engineering, Nagasaki University
引用: 長崎大学工学部研究報告, 21(35), pp.1-8; 1990
抄録: The mechanism of the fluctuating phenomena in the wake was investigated to NACA0008 and NACA0015 blades with experimentally. It's found that when the attack angle a is small, the periodic fluctuating phenomenon emerges in the wake for both type blades. This phenomenon is the Karman vortex street which generates from the separation of a laminar boundary layer upstream of the trailing edge and from the formation of a dead air region. At NACA0008 blade the frequency of the Karman vortex formation falls with the attack angle increasing, because the separation of the laminar boundary layer occurs mainly on the suction surface and the dead air region becomes large as a attack angle increases. At NACA0015 blade, the frequency of the Karman vortex formation increases with the attack angle in'creasing, because the separation occurs mainly on the pressure surface and the dead air region becomes small as the attack angle increases. When the attack angle more increases, the Karman vortex street disappers for both blades because of the boundary layer on both surface of the blade attached before the trailing edge and no dead air region formed. When the attack angle is very large, the flow of suction side separates near the leading edge and the large dead air region forms so the Karman vortex street emerges and it's frequersy is very low.
URI: http://hdl.handle.net/10069/24316
ISSN: 02860902
資料タイプ: Departmental Bulletin Paper
原稿種類: publisher
出現コレクション:第21巻 第35号

引用URI : http://hdl.handle.net/10069/24316



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