Journal cover Journal topic
Wind Energy Science The interactive open-access journal of the European Academy of Wind Energy
https://doi.org/10.5194/wes-2016-39
© Author(s) 2016. This work is distributed under
the Creative Commons Attribution 3.0 License.
Research articles
06 Dec 2016
Review status
A revision of this discussion paper was accepted for the journal Wind Energy Science (WES) and is expected to appear here in due course.
Modal Properties and Stability of Bend-Twist Coupled Wind Turbine Blades
Alexander R. Stäblein, Morten H. Hansen, and David R. Verelst Technical University of Denmark, Department of Wind Energy, Frederiksborgvej 399, 4000 Roskilde, Denmark
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 utilised to reduce the fatigue loads of wind turbine blades. In this study the effect of material based coupling on the aeroelastic modal properties and stability limits of the DTU 10 MW Reference Wind Turbine are investigated. The modal properties are determined by means of eigenvalue analysis around a steady-state equilibrium using the aero-servo-elastic tool HAWCStab2 which has been extended by a beam element that allows for fully coupled cross-sectional properties. Bend-twist coupling is introduced in the cross-sectional stiffness matrix by means of coupling coefficients that introduce twist for flapwise (flap-twist coupling) or edgewise (edge-twist coupling) bending. Edge-twist coupling can increase or decrease the damping of the edgewise mode relative to the reference blade, depending on the operational condition of the turbine. Edge-twist to feather coupling for edgewise deflection towards the leading edge reduces the inflow speed at which the blade becomes unstable. Flap-twist to feather coupling for flapwise deflections towards the suction side increase the frequency and reduce damping of the flapwise mode. Flap-twist to stall reduces frequency and increases damping. The reduction of blade root flapwise and tower bottom fore-aft moments due to variations in mean wind speed of a flap-twist to feather blade are confirmed by frequency response functions.

Citation: Stäblein, A. R., Hansen, M. H., and Verelst, D. R.: Modal Properties and Stability of Bend-Twist Coupled Wind Turbine Blades, Wind Energ. Sci. Discuss., https://doi.org/10.5194/wes-2016-39, in review, 2016.
Alexander R. Stäblein et al.
Interactive discussionStatus: closed
AC: Author comment | RC: Referee comment | SC: Short comment | EC: Editor comment
Printer-friendly Version - Printer-friendly version      Supplement - Supplement
 
RC1: 'Review comments for WES-2016-38', Anonymous Referee #1, 07 Jan 2017 Printer-friendly Version 
AC1: 'Reviewer #1 Author Comments', Alexander Stäblein, 12 Apr 2017 Printer-friendly Version 
 
RC2: 'Referee Comments', Anonymous Referee #2, 15 Mar 2017 Printer-friendly Version 
AC2: 'Reviewer #2 Author Comments', Alexander Stäblein, 12 Apr 2017 Printer-friendly Version 
Alexander R. Stäblein et al.
Alexander R. Stäblein et al.

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Short summary
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 or from the anisotropic properties of the blade material. Bend-twist coupling can be utilised to reduce the fatigue loads of wind turbine blades. In this study the effect of material based coupling on the aeroelastic modal properties and stability limits of the DTU 10 MW Reference Wind Turbine are investigated.
Coupling between bending and twist has a significant influence on the aeroelastic response of...
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