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contributor authorAlessandro Corsini
contributor authorA. G. Sheard
contributor authorFranco Rispoli
date accessioned2017-05-09T00:41:31Z
date available2017-05-09T00:41:31Z
date copyrightJuly, 2010
date issued2010
identifier issn0889-504X
identifier otherJOTUEI-28764#031005_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/144985
description abstractThis paper reports on quantitative tests of passive techniques for rotor-tip noise control in low-speed axial flow fans, based on blade-tip modifications involving the addition of antivortex appendages as end-plates. The end-plate thickness chordwise distribution is determined to control the chordwise evolution of the leakage vortex rotation number. The results confirm that the new end-plate configurations provide a mechanism by which leakage vortex bursting can be avoided. As such, the modified rotors represent an effective means of passive control of vortex breakdown.
publisherThe American Society of Mechanical Engineers (ASME)
titleShaping of Tip End-Plate to Control Leakage Vortex Swirl in Axial Flow Fans
typeJournal Paper
journal volume132
journal issue3
journal titleJournal of Turbomachinery
identifier doi10.1115/1.3145017
journal fristpage31005
identifier eissn1528-8900
keywordsFans
keywordsRotors
keywordsVortices
keywordsFlow (Dynamics)
keywordsBlades
keywordsLeakage
keywordsLeakage flows
keywordsThickness
keywordsAxial flow AND Design
treeJournal of Turbomachinery:;2010:;volume( 132 ):;issue: 003
contenttypeFulltext


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