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    Full-Scale Wind Turbine Near-Wake Measurements Using an Instrumented Uninhabited Aerial Vehicle

    Source: Journal of Solar Energy Engineering:;2011:;volume( 133 ):;issue: 004::page 41011
    Author:
    G. Kocer
    ,
    M. Müller
    ,
    M. Mansour
    ,
    N. Chokani
    ,
    R.S. Abhari
    DOI: 10.1115/1.4004707
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In this paper, the first-ever measurements of the wake of a full-scale wind turbine using an instrumented uninhabited aerial vehicle (UAV) are reported. The key enabler for this novel measurement approach is the integration of fast response aerodynamic probe technology with miniaturized hardware and software for UAVs that enable autonomous UAV operation. The measurements, made to support the development of advanced wind simulation tools, are made in the near-wake (0.5D–3D, where D is rotor diameter) region of a 2 MW wind turbine that is located in a topography of complex terrain and varied vegetation. Downwind of the wind turbine, profiles of the wind speed show that there is strong three-dimensional shear in the near-wake flow. Along the centerline of the wake, the deficit in wind speed is a consequence of wakes from the rotor, nacelle, and tower. By comparison with the profiles away from the centerline, the shadowing effects of nacelle and tower diminish downstream of 2.5D. Away from the centerline, the deficit in wind speed is approximately constant ≈ 25%. However, along the centerline, the deficit is ≈ 65% near to the rotor, 0.5D–1.75D, and only decreases to ≈ 25% downstream of 2.5D.
    keyword(s): Measurement , Wind velocity , Wakes , Wind , Wind turbines , Unmanned aerial vehicles , Aircraft , Flow (Dynamics) , Rotors , Probes AND Flight ,
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      Full-Scale Wind Turbine Near-Wake Measurements Using an Instrumented Uninhabited Aerial Vehicle

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    http://yetl.yabesh.ir/yetl1/handle/yetl/147538
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    contributor authorG. Kocer
    contributor authorM. Müller
    contributor authorM. Mansour
    contributor authorN. Chokani
    contributor authorR.S. Abhari
    date accessioned2017-05-09T00:46:45Z
    date available2017-05-09T00:46:45Z
    date copyrightNovember, 2011
    date issued2011
    identifier issn0199-6231
    identifier otherJSEEDO-28450#041011_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/147538
    description abstractIn this paper, the first-ever measurements of the wake of a full-scale wind turbine using an instrumented uninhabited aerial vehicle (UAV) are reported. The key enabler for this novel measurement approach is the integration of fast response aerodynamic probe technology with miniaturized hardware and software for UAVs that enable autonomous UAV operation. The measurements, made to support the development of advanced wind simulation tools, are made in the near-wake (0.5D–3D, where D is rotor diameter) region of a 2 MW wind turbine that is located in a topography of complex terrain and varied vegetation. Downwind of the wind turbine, profiles of the wind speed show that there is strong three-dimensional shear in the near-wake flow. Along the centerline of the wake, the deficit in wind speed is a consequence of wakes from the rotor, nacelle, and tower. By comparison with the profiles away from the centerline, the shadowing effects of nacelle and tower diminish downstream of 2.5D. Away from the centerline, the deficit in wind speed is approximately constant ≈ 25%. However, along the centerline, the deficit is ≈ 65% near to the rotor, 0.5D–1.75D, and only decreases to ≈ 25% downstream of 2.5D.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleFull-Scale Wind Turbine Near-Wake Measurements Using an Instrumented Uninhabited Aerial Vehicle
    typeJournal Paper
    journal volume133
    journal issue4
    journal titleJournal of Solar Energy Engineering
    identifier doi10.1115/1.4004707
    journal fristpage41011
    identifier eissn1528-8986
    keywordsMeasurement
    keywordsWind velocity
    keywordsWakes
    keywordsWind
    keywordsWind turbines
    keywordsUnmanned aerial vehicles
    keywordsAircraft
    keywordsFlow (Dynamics)
    keywordsRotors
    keywordsProbes AND Flight
    treeJournal of Solar Energy Engineering:;2011:;volume( 133 ):;issue: 004
    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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