Advances in Wind Turbine Blade Design and Materials 2013
DOI: 10.1533/9780857097286.2.175
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Fatigue as a design driver for composite wind turbine blades

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Cited by 29 publications
(23 citation statements)
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“…Regarding common literature characterisations [45,46] for the fatigue life behaviour of typical unidirectional composites, for example, those used in rotor blade applications, the results obtained with the new test specimens are well comparable. In particular, the slopes of the best-fit SN-curves, as well as the composites strength, stiffness, and ply structure, are of the same magnitude.…”
Section: Details Of Fatigue Testing After Hygrothermal Wet Ageingsupporting
confidence: 53%
“…Regarding common literature characterisations [45,46] for the fatigue life behaviour of typical unidirectional composites, for example, those used in rotor blade applications, the results obtained with the new test specimens are well comparable. In particular, the slopes of the best-fit SN-curves, as well as the composites strength, stiffness, and ply structure, are of the same magnitude.…”
Section: Details Of Fatigue Testing After Hygrothermal Wet Ageingsupporting
confidence: 53%
“…During a wind turbine's life-time of around 20-30 years, it experiences a high number of load cycles (in the range of 10 8 − 10 9 cycles) [2]. The blade is subjected to repeated flapwise bending from the wind and repeated edge-wise bending from the blade weight combined with the rotation [3]. The main load carrying parts of a wind turbine blade consist of uni-directional (UD) glass fibre composite materials made from non-crimp fabrics (NCF).…”
Section: Introductionmentioning
confidence: 99%
“…The fatigue damage mechanisms in glass fibre-reinforced composite materials used for wind turbine rotor blades are closely related to the material architecture and the material systems (Nijssen & Brøndsted, 2011). The damage progression in fibre-reinforced composites can be monitored experimentally and quantified in the measurement of the experimentally observed stiffness degradation (Brøndsted et al, 1996).…”
Section: Fatigue Damagementioning
confidence: 99%
“…This is in order to give an optimised wind flow around the blade, taking the optimal energy out from the wing, to obtain optimal structural performance and aeroelasticity, combining interaction between dynamic loads and structural elasticity and damping, and to ensure material strength and stiffness in the critical load-carrying parts. These topics are described in detail in various chapters elsewhere (Nijssen & Brøndsted, 2011, 2013. The flap-wise longitudinal loads are carried by two longitudinal spars, referred to as the main laminates (beams), separated by one or more webs taking up the shear and edge-wise loads.…”
Section: Blade Design Conceptsmentioning
confidence: 99%