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タイトルAn experimental study of dynamic stall on advanced airfoil section. Volume 2: Pressure and force data
本文(外部サイト)http://hdl.handle.net/2060/19830003778
著者(英)Pucci, S. L.; Mccroskey, W. J.; Mcalister, K. W.; Carr, L. W.
著者所属(英)NASA Ames Research Center|Army Aviation Research and Development Command
発行日1982-09-01
言語eng
内容記述Experimentally derived force and moment data are presented for eight airfoil sections that were tested at fixed and varying incidence in a subsonic two dimensional stream. Airfoil incidence was varied through sinusoidal oscillations in pitch over a wide range of amplitude and frequency. The surface pressure distribution, as well as the lift, drag, and pitching moment derived therefrom, are displayed in a uniform fashion to delineate the static and dynamic characteristics of each airfoil both in and out of stall.
NASA分類AERODYNAMICS
レポートNO83N12048
A-8925
NAS 1.15:84245-VOL-2
USAAVRADCOM-TR-82-A-8-VOL-2
NASA-TM-84245-VOL-2
権利No Copyright
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/164386


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