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contributor authorW. A. Eckerle
contributor authorL. S. Langston
date accessioned2017-05-08T23:26:05Z
date available2017-05-08T23:26:05Z
date copyrightApril, 1987
date issued1987
identifier issn0889-504X
identifier otherJOTUEI-28583#278_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/103250
description abstractAn experimental investigation was conducted to characterize a symmetric horseshoe vortex system in front of and around a single large-diameter right cylinder centered between the sidewalls of a wind tunnel. Surface flow visualization and surface static pressure measurements as well as extensive mean velocity and pressure measurements in and around the vortex system were acquired. The results lend new insight into the formation and development of the vortex system. Contrary to what has been assumed previously, a strong vortex was not identified in the streamwise plane of symmetry, but started a significant angular distance away from it. Rather than the multiple vortex systems reported by others, only a single primary vortex and saddle point were found. The scale of the separation process at the saddle point was much smaller than the scale of the approaching boundary layer thickness. Results of the present study not only shed light on such phenomena as the asymmetric endwall flow in axial turbomachinery but can also be used as a test case for three-dimensional computational fluid mechanics computer codes.
publisherThe American Society of Mechanical Engineers (ASME)
titleHorseshoe Vortex Formation Around a Cylinder
typeJournal Paper
journal volume109
journal issue2
journal titleJournal of Turbomachinery
identifier doi10.1115/1.3262098
journal fristpage278
journal lastpage285
identifier eissn1528-8900
treeJournal of Turbomachinery:;1987:;volume( 109 ):;issue: 002
contenttypeFulltext


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