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contributor authorX. Liang
contributor authorB. R. Ramaprian
date accessioned2017-05-08T23:35:48Z
date available2017-05-08T23:35:48Z
date copyrightSeptember, 1991
date issued1991
identifier issn0098-2202
identifier otherJFEGA4-27061#511_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/108725
description abstractThe evolution of the longitudinal vortex in the near field of a rectangular wing has been visualized using smoke and laser light sheet. The smoke photographs have been used to obtain qualitative and some quantitative information on the effect of small temporal and spatial pressure gradients on the evolution of the vortex in this region. The experiments indicate that even small temporal retardation of the flow can produce a significant increase in the vortex size. This effect becomes larger with increase in retardation, angle of incidence and distance downstream from the trailing edge. Also, vortex “breakdown” was found to occur in many temporal-deceleration experiments. The vortex evolution was, however, found to be relatively insensitive to the presence of small spatial adverse pressure gradients along the flow direction. The study is preliminary in nature and needs to be supported by more extensive quantitative measurements.
publisherThe American Society of Mechanical Engineers (ASME)
titleVisualization of the Wing-Tip Vortex in Temporal and Spatial Pressure Gradients
typeJournal Paper
journal volume113
journal issue3
journal titleJournal of Fluids Engineering
identifier doi10.1115/1.2909527
journal fristpage511
journal lastpage515
identifier eissn1528-901X
keywordsVisualization
keywordsVortices
keywordsPressure gradient
keywordsWings
keywordsFlow (Dynamics)
keywordsSmoke
keywordsLasers AND Measurement
treeJournal of Fluids Engineering:;1991:;volume( 113 ):;issue: 003
contenttypeFulltext


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