Nonlinear aerolastic equations of motion of twisted, nonuniform, flexible horizontal-axis wind turbine blades /

Detalles Bibliográficos
Autor Principal: Kaza, Krishna Rao V.
Autores Corporativos: National Aeronautics and Space Administration, United States Department of Energy
Formato: Libro
Lengua:inglés
Datos de publicación: Cleveland : National Aeronautics and Space Administration, 1980
Washington : United States Department of Energy, 1980
Series:DOE/NASA
Temas:
Acceso en línea:https://ntrs.nasa.gov/citations/19800018275
Notas:Informe/número de patente NASA CR-159502
DOE/NASA/3139-1
Descripción Física:68 p. : figuras

MARC

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100 1 |a Kaza, Krishna Rao V.  |9 318653 
245 1 |a Nonlinear aerolastic equations of motion of twisted, nonuniform, flexible horizontal-axis wind turbine blades /   |c Krisha Rao V. Kaza 
260 |a Cleveland :   |b National Aeronautics and Space Administration,   |c 1980 
260 |a Washington :   |b United States Department of Energy,   |c 1980 
300 |a 68 p. :   |b figuras 
490 |a DOE/NASA 
500 |a Informe/número de patente NASA CR-159502 
500 |a DOE/NASA/3139-1 
505 |a 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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710 1 |a National Aeronautics and Space Administration  |9 318667 
710 1 |a United States Department of Energy  |9 268561 
856 |u https://ntrs.nasa.gov/citations/19800018275 
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