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    Dynamic Stall: The Case of the Vertical Axis Wind Turbine

    Source: Journal of Solar Energy Engineering:;1986:;volume( 108 ):;issue: 002::page 140
    Author:
    A. Laneville
    ,
    P. Vittecoq
    DOI: 10.1115/1.3268081
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This 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.
    keyword(s): Aerodynamics , Reynolds number , Turbines , Vortices , Blades , Vertical axis wind turbines AND Airfoils ,
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      Dynamic Stall: The Case of the Vertical Axis Wind Turbine

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/101654
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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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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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