Investigation of the development of unsteady flow separation from a model swept wing

Autor:	I. V. Kolin, V. L. Sukhanov, D. V. Shukhovtsov, T. I. Trifonova, V. G. Markov
Rok vydání:	2009
Předmět:	Fluid Flow and Transfer Processes Unsteady flow Physics Boundary layer Flow separation Amplitude Angle of attack Mechanical Engineering Acoustics Separation (aeronautics) Swept wing General Physics and Astronomy Development (differential geometry)
Zdroj:	Fluid Dynamics. 44:680-686
ISSN:	1573-8507 0015-4628
DOI:	10.1134/s0015462809050068
Popis:	The results of an experimental wind-tunnel investigation of the flow patterns on the swept wing of a model aircraft realized for pitching oscillations with an amplitude Aα = 5° with respect to setup angles of attack α0 = 10 and 16° are presented.
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=doi_________::ec8e14ea99061f3688209fc223ecb92b https://doi.org/10.1134/s0015462809050068 Zobrazit plný text záznamu Plný text ve formátu PDF