Design of Flexible Wind Tunnel Model of Yawed Wind Turbine Rotor with Teetering Hub

Conference Paper (2023)
Author(s)

P. Georgopoulos (TU Delft - Group De Breuker)

J Sodja (TU Delft - Aerospace Structures & Computational Mechanics)

R Breuker (TU Delft - Aerospace Structures & Computational Mechanics)

Research Group
Aerospace Structures & Computational Mechanics
Copyright
© 2023 P. Georgopoulos, J. Sodja, R. De Breuker
DOI related publication
https://doi.org/10.2514/6.2023-2091
More Info
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Publication Year
2023
Language
English
Copyright
© 2023 P. Georgopoulos, J. Sodja, R. De Breuker
Research Group
Aerospace Structures & Computational Mechanics
ISBN (electronic)
978-1-62410-699-6
Reuse Rights

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Abstract

The present study regards a novel wind turbine design featuring a two-bladed rotor on ate etering hub and a yawed tower. A reduced order modelling methodology is proposed for the equation of motion, using a lumped parameter approximation to derive expressions for the structural, rotor dynamic and geometric stiffness terms. The analytical expressions are validated numerically. In addition, a methodology is developed for aero elastic scaling of the rotor for use in wind tunnel tests. This results in two blade design templates, a "stiff" and a "flexible" design focusing on the vibration behaviour and deflected shapes respectively. The templates are designed to be 3D-printable as a single part. Design optimisation was performed in MSCN as tran, yielding two rotor designs, each aiming to match the non-dimensional parameters of interest. The stiff rotor matches the flap wise and torsional natural frequencies within 2.7%error, but has a mismatch in the edgewise mode, as well as the mode shapes and anti-symmetric modes. The flexible rotor is capable of capturing the target normalised displacement profile, at reduced structural mass, partially alleviating the mismatch in Lock number.

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