• DocumentCode
    3237433
  • Title

    Effect of laminate configuration and shell-thickness variation on the inducted twist distribution in wind turbine adaptive blades

  • Author

    Zhang, Hui ; Daadbin, Ali ; Maheri, Alireza ; Hackney, Phil

  • Author_Institution
    Northumbria Univ., Newcastle upon Tyne, UK
  • fYear
    2012
  • fDate
    25-27 June 2012
  • Firstpage
    406
  • Lastpage
    411
  • Abstract
    This paper presents an analytical model for predicting the dynamic characteristics of composite wind turbine blades. In this model, the governing equations of motion are derived using Hamiltion´s principle and are solved by using extended Galerkin´s method. This model is capable of predicting natural frequencies of composite beams with arbitrary single-cell cross sections. For various layup configurations, the results obtained by the developed analytical model are compared with the results of the finite element analysis. It is shown that the analytical model provides reasonable accuracy in predicting natural frequency of unbalanced layup configurations with ply angles of up to 40 degrees.
  • Keywords
    Galerkin method; beams (structures); blades; dynamic response; finite element analysis; frequency-domain analysis; wind turbines; Hamiltion principle; analytical model; arbitrary single-cell cross sections; composite beams; composite wind turbine adaptive blades; dynamic characteristics prediction; extended Galerkin method; finite element analysis; frequency analysis; governing equations of motion; natural frequency prediction; ply angles; unbalanced layup configurations; Adaptation models; Analytical models; Blades; Materials; Mirrors; Predictive models; Hamiltion´s principle; adaptive blades; extended Galerkin´s method; thin-walled composite beam; wind turbine blade;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Environment Friendly Energies and Applications (EFEA), 2012 2nd International Symposium on
  • Conference_Location
    Newcastle upon Tyne
  • Print_ISBN
    978-1-4673-2909-5
  • Electronic_ISBN
    978-1-4673-2910-1
  • Type

    conf

  • DOI
    10.1109/EFEA.2012.6294046
  • Filename
    6294046