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    Assessing the Importance of Geometric Nonlinear Effects in the Prediction of Wind Turbine Blade Loads

    Source: Journal of Computational and Nonlinear Dynamics:;2015:;volume( 010 ):;issue: 004::page 41008
    Author:
    Manolas, D. I.
    ,
    Riziotis, V. A.
    ,
    Voutsinas, S. G.
    DOI: 10.1115/1.4027684
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: As the size of commercial wind turbines increases, new blade designs become more flexible in order to comply with the requirement for reduced weights. In normal operation conditions, flexible blades undergo large bending deflections, which exceed 10% of their radius, while significant torsion angles toward the tip of the blade are obtained, which potentially affect performance and stability. In the present paper, the effects on the loads of a wind turbine from structural nonlinearities induced by large deflections of the blades are assessed, based on simulations carried out for the NREL 5 MW wind turbine. Two nonlinear beam models, a second order (2nd order) model and a multibody model that both account for geometric nonlinear structural effects, are compared to a first order beam (1st order) model. Deflections and loads produced by finite element method based aeroelastic simulations using these three models show that the bending–torsion coupling is the main nonlinear effect that drives differences on loads. The main effect on fatigue loads is the over 100% increase of the torsion moment, having obvious implications on the design of the pitch bearings. In addition, nonlinearity leads to a clear shift in the frequencies of the second edgewise modes.
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      Assessing the Importance of Geometric Nonlinear Effects in the Prediction of Wind Turbine Blade Loads

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    https://yetl.yabesh.ir/yetl1/handle/yetl/157304
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    • Journal of Computational and Nonlinear Dynamics

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    contributor authorManolas, D. I.
    contributor authorRiziotis, V. A.
    contributor authorVoutsinas, S. G.
    date accessioned2017-05-09T01:15:45Z
    date available2017-05-09T01:15:45Z
    date issued2015
    identifier issn1555-1415
    identifier othercnd_010_04_041008.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/157304
    description abstractAs the size of commercial wind turbines increases, new blade designs become more flexible in order to comply with the requirement for reduced weights. In normal operation conditions, flexible blades undergo large bending deflections, which exceed 10% of their radius, while significant torsion angles toward the tip of the blade are obtained, which potentially affect performance and stability. In the present paper, the effects on the loads of a wind turbine from structural nonlinearities induced by large deflections of the blades are assessed, based on simulations carried out for the NREL 5 MW wind turbine. Two nonlinear beam models, a second order (2nd order) model and a multibody model that both account for geometric nonlinear structural effects, are compared to a first order beam (1st order) model. Deflections and loads produced by finite element method based aeroelastic simulations using these three models show that the bending–torsion coupling is the main nonlinear effect that drives differences on loads. The main effect on fatigue loads is the over 100% increase of the torsion moment, having obvious implications on the design of the pitch bearings. In addition, nonlinearity leads to a clear shift in the frequencies of the second edgewise modes.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleAssessing the Importance of Geometric Nonlinear Effects in the Prediction of Wind Turbine Blade Loads
    typeJournal Paper
    journal volume10
    journal issue4
    journal titleJournal of Computational and Nonlinear Dynamics
    identifier doi10.1115/1.4027684
    journal fristpage41008
    journal lastpage41008
    identifier eissn1555-1423
    treeJournal of Computational and Nonlinear Dynamics:;2015:;volume( 010 ):;issue: 004
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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