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Nonlinear aerolastic equations of motion of twisted, nonuniform, flexible horizontal-axis wind turbine blades / Krisha Rao V. Kaza

Por: Colaborador(es): Tipo de material: TextoTextoIdioma: Inglés Series DOE/NASADetalles de publicación: Cleveland : National Aeronautics and Space Administration, 1980; Washington : United States Department of Energy, 1980Descripción: 68 p. : figurasTema(s): Recursos en línea:
Contenidos:
The second-degree nonlinear equations of motion for a flexible, twisted, nonuniform, horizontal axis wind turbine blade were developed using Hamilton's principle. A mathematical ordering scheme which was consistent with the assumption of a slender beam was used to discard some higher-order elastic and inertial terms in the second-degree nonlinear equations. The blade aerodynamic loading which was employed accounted for both wind shear and tower shadow and was obtained from strip theory based on a quasi-steady approximation of two-dimensional, incompressible, unsteady, airfoil theory. The resulting equations had periodic coefficients and were suitable for determining the aeroelastic stability and response of large horizontal-axis wind turbine blades.
Tipo de ítem: Libro
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Informe/número de patente NASA CR-159502

DOE/NASA/3139-1

The second-degree nonlinear equations of motion for a flexible, twisted, nonuniform, horizontal axis wind turbine blade were developed using Hamilton's principle. A mathematical ordering scheme which was consistent with the assumption of a slender beam was used to discard some higher-order elastic and inertial terms in the second-degree nonlinear equations. The blade aerodynamic loading which was employed accounted for both wind shear and tower shadow and was obtained from strip theory based on a quasi-steady approximation of two-dimensional, incompressible, unsteady, airfoil theory. The resulting equations had periodic coefficients and were suitable for determining the aeroelastic stability and response of large horizontal-axis wind turbine blades.

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