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contributor authorY. Senoo
contributor authorM. Nishi
date accessioned2017-05-09T01:38:24Z
date available2017-05-09T01:38:24Z
date copyrightMarch, 1974
date issued1974
identifier issn0098-2202
identifier otherJFEGA4-26853#4_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/164919
description abstractVortex generators, which consist of small blades, are applied to conical diffusers the divergence angles of which are 8, 12, 16, 20, and 30 deg, respectively. The area ratio of each diffuser is four. The experiment covers the influence of various parameters, such as the arrangement of blades, inlet boundary layer thickness, and location of vortex generators relative to the conical diffuser, on the pressure-recovery coefficient. The experiment shows that the vortex generators prevent the flow in a conical diffuser from separating up to a divergence angle of 16 deg, and that the pressure-recovery coefficient is approximately equal to that of conventional best conical diffusers.
publisherThe American Society of Mechanical Engineers (ASME)
titleImprovement of the Performance of Conical Diffusers by Vortex Generators
typeJournal Paper
journal volume96
journal issue1
journal titleJournal of Fluids Engineering
identifier doi10.1115/1.3447097
journal fristpage4
journal lastpage10
identifier eissn1528-901X
keywordsDiffusers
keywordsVortices
keywordsGenerators
keywordsBlades
keywordsPressure
keywordsFlow (Dynamics)
keywordsBoundary layers AND Thickness
treeJournal of Fluids Engineering:;1974:;volume( 096 ):;issue: 001
contenttypeFulltext


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