Measurements of turbulent flow behind a wing-body junction

Wind tunnel measurements have been obtained for the turbulent shear flow behind a wing mounted on a flat plate at 30-deg angle-of-attack, giving attention to such physical aspects of the flow as the skin-friction coefficient and pattern, the static pressure coefficient, and two mean velocity compone...

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Veröffentlicht in:	AIAA journal 1988-04, Vol.26 (4), p.494-496
Hauptverfasser:	Ozcan, O, Olcmen, M. S
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamics Applied fluid mechanics Exact sciences and technology Fluid dynamics fluid mechanics Fundamental areas of phenomenology (including applications) Physics turbulent flow wings
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description	Wind tunnel measurements have been obtained for the turbulent shear flow behind a wing mounted on a flat plate at 30-deg angle-of-attack, giving attention to such physical aspects of the flow as the skin-friction coefficient and pattern, the static pressure coefficient, and two mean velocity components. No evidence is found of the presence of a second tornado vortex, perhaps due to the attached flow conditions on the windward side of the wing, where flow separation from the trailing edge did not lead to a sufficiently large reversed-flow region. (O.C.)
doi_str_mv	10.2514/3.9921
format	Article
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subjects	Aerodynamics Applied fluid mechanics Exact sciences and technology Fluid dynamics fluid mechanics Fundamental areas of phenomenology (including applications) Physics turbulent flow wings
title	Measurements of turbulent flow behind a wing-body junction
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