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  • Other Sources  (1)
  • NASA Technical Reports  (1)
  • ENERGY PRODUCTION AND CONVERSION  (1)
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  • 2010-2014
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    In:  CASI
    Publication Date: 2016-06-07
    Description: The second degree nonlinear aeroelastic equations for a flexible, twisted, nonuniform wind turbine blade were developed using Hamilton's principle. The derivation of these equations has its basis in the geometric nonlinear theory of elasticity. These equations with periodic coefficients are suitable for determining the aeroelastic stability and response of large wind turbine blades. Methods for solving these equations are discussed.
    Keywords: ENERGY PRODUCTION AND CONVERSION
    Type: NASA. Lewis Res. Center Wind Turbine Structural Dyn.; p 61-69
    Format: application/pdf
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