NASA Technical Reports Server (NTRS) 19780011679: Aeroelastic stability of wind turbine blades Wind Turbine Structural Dynamics

Book details

Title
NASA Technical Reports Server (NTRS) 19780011679: Aeroelastic stability of wind turbine blades Wind Turbine Structural Dynamics
Publication year listed
1928
Format
Public domain eBook
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View on Archive.org

About this book

NASA Technical Reports Server (NTRS) 19780011679: Aeroelastic stability of wind turbine blades Wind Turbine Structural Dynamics

Author: NASA Technical Reports Server (NTRS)

Year: 1928

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.

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