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contributor authorA. Laneville
contributor authorP. Vittecoq
date accessioned2017-05-08T23:23:24Z
date available2017-05-08T23:23:24Z
date copyrightMay, 1986
date issued1986
identifier issn0199-6231
identifier otherJSEEDO-28189#140_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/101654
description abstractThis paper presents the results of an experimental investigation on a driven Darrieus turbine rotating at different tip speed ratios. For a Reynolds number of 3.8 × 104 , the results indicate the presence of dynamic stall at tip speed ratio less than 4, and that helicopter blade aerodynamics can be used in order to explain some aspects of the phenomenon. It was observed that in deep stall conditions, a vortex is formed at the leading edge; this vortex moves over the airfoil surface with 1/3 of the airfoil speed and then is shed at the trailing edge. After its shedding, the vortex can interact with the airfoil surface as the blade passes downstream.
publisherThe American Society of Mechanical Engineers (ASME)
titleDynamic Stall: The Case of the Vertical Axis Wind Turbine
typeJournal Paper
journal volume108
journal issue2
journal titleJournal of Solar Energy Engineering
identifier doi10.1115/1.3268081
journal fristpage140
journal lastpage145
identifier eissn1528-8986
keywordsAerodynamics
keywordsReynolds number
keywordsTurbines
keywordsVortices
keywordsBlades
keywordsVertical axis wind turbines AND Airfoils
treeJournal of Solar Energy Engineering:;1986:;volume( 108 ):;issue: 002
contenttypeFulltext


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