2017
DOI: 10.5194/wes-2-343-2017
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Modal properties and stability of bend–twist coupled wind turbine blades

Abstract: Abstract.Coupling between bending and twist has a significant influence on the aeroelastic response of wind turbine blades. The coupling can arise from the blade geometry (e.g. sweep, prebending, or deflection under load) or from the anisotropic properties of the blade material. Bend-twist coupling can be utilized to reduce the fatigue loads of wind turbine blades. In this study the effects of material-based coupling on the aeroelastic modal properties and stability limits of the DTU 10 MW Reference Wind Turbi… Show more

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Cited by 26 publications
(26 citation statements)
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“…When the blades flex into and out of the wind, the rotor interacts with its own vorticity, calling the accuracy of the design assumptions into question. Additionally, structural dynamics of blades incorporating composite materials, built-in curvature and sweep, and large nonlinear deflection (including torsion and bend-twist coupling) further complicate models of the physics (69) and the assessment of crucial design aspects such as stability (70,71). In fact, although aeroelastic stability has typically not been a key design driver for rotor blades up to now, the situation may change for future highly flexible and large rotors.…”
Section: First Grand Challenge: Improved Understanding Of Atmosphericmentioning
confidence: 99%
“…When the blades flex into and out of the wind, the rotor interacts with its own vorticity, calling the accuracy of the design assumptions into question. Additionally, structural dynamics of blades incorporating composite materials, built-in curvature and sweep, and large nonlinear deflection (including torsion and bend-twist coupling) further complicate models of the physics (69) and the assessment of crucial design aspects such as stability (70,71). In fact, although aeroelastic stability has typically not been a key design driver for rotor blades up to now, the situation may change for future highly flexible and large rotors.…”
Section: First Grand Challenge: Improved Understanding Of Atmosphericmentioning
confidence: 99%
“…Steady operational points are defined by steady wind speed, pitch angle, and rotor angular speed. It performs modal analysis around a stationary deflected position of the blades with or without aerodynamic stiffness and damping terms . The normal (undamped) blade mode shapes were calculated in HAWCStab2 for different steady conditions, including the load effects such as centrifugal stiffening and without gravity, aerodynamic stiffness and aerodynamic damping effects.…”
Section: Methods and Implementationmentioning
confidence: 99%
“…The optimisation of blade twist and its resultant effects have been extensively studied for pitch-to-feather and fixed-pitch stall configurations using a number of methods [9][10][11]. In such instances, the design criteria commonly focuses on maximising the power coefficient and reducing blade vibrations and fatigue.…”
Section: Introductionmentioning
confidence: 99%
“…In such instances, the design criteria commonly focuses on maximising the power coefficient and reducing blade vibrations and fatigue. Stäblein et al [10] achieved increased platform damping, and hence, reductions in tower fore-aft moment from blade twist modifications. For fixed-stall blades, a back twist was employed (the blade twists back towards feather at the tip for a proportion of the blade's length) which resulted in the air flow remaining attached at the blade tip for higher wind speeds, thus increasing the power production capabilities of these sections of the blade [9].…”
Section: Introductionmentioning
confidence: 99%