2017
DOI: 10.1016/j.jfluidstructs.2017.06.008
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Extension of the Non-Linear Harmonic method for the study of the dynamic aeroelasticity of horizontal axis wind turbines

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Cited by 12 publications
(7 citation statements)
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“…In the aeromechanical analysis of turbomachines, relatively small amplitudes are typically used. However, previous studies suggest that the deflection of the blade can be up to 9% of the blade span [30]. Therefore, a relatively large amplitude of 9% of the span is used in this study.…”
Section: Aeromechanical Analysis Of the Mexico-experiments Wind Turbinementioning
confidence: 99%
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“…In the aeromechanical analysis of turbomachines, relatively small amplitudes are typically used. However, previous studies suggest that the deflection of the blade can be up to 9% of the blade span [30]. Therefore, a relatively large amplitude of 9% of the span is used in this study.…”
Section: Aeromechanical Analysis Of the Mexico-experiments Wind Turbinementioning
confidence: 99%
“…It is found that a fully coupled multiple blade row model yields better accuracy in predicting flutter behaviour of the turbomachines than the simplified isolated one [28]. Although frequency domain methods are typically used for the aeromechanical analysis of turbomachinery applications, only a few studies recently applied these methods to wind turbine applications [29][30][31][32][33][34]. This has motivated the authors to seek an efficient numerical method employing a frequency domain method for the aerodynamic and aeroelasticity simulations of wind turbines at an affordable computational cost without compromising accuracy in predicting unsteady flows.…”
Section: Introductionmentioning
confidence: 99%
“…The flow inlet and outlet are located 2R upstream of the rotor and 4R downstream of the rotor, respectively, and the far-field boundary is placed 3R from the origin of coordinates, where R is the rotor radius. There are studies in the literature which used similar domain sizes and showed that they can accurately predict the blade loading and flow behaviour [12,26,38]. Therefore, it can be noted that the considered distances for far-field boundaries are sufficiently far away from the turbine.…”
Section: Computational Domain and Gridmentioning
confidence: 99%
“…11 It has been further improved to include unsteady uid loads in the structural deformation. 12,13 The structural ROM that has been retained for the present study is the Oofelie R Computational Structure Mechanics solver. It is a general purpose nite element software for structural and heat transfer analysis.…”
Section: Linear Beam Model With Rans-based Aerodynamicsmentioning
confidence: 99%