Aeroelastic design and LPV modelling of an experimental wind turbine blade equipped with free-floating flaps

Conference Paper (2016)
Author(s)

Sachin Navalkar (TU Delft - Mechanical Engineering)

Lars Bernhammer (TU Delft - Aerospace Engineering)

Jurij Sodja (TU Delft - Aerospace Engineering)

Kees Slinkman (TU Delft - Mechanical Engineering)

Jan-Willem van Wingerden (TU Delft - Mechanical Engineering)

Gijs van Kuik (TU Delft - Aerospace Engineering)

Research Group
Team Raf Van de Plas
DOI related publication
https://doi.org/10.1088/1742-6596/753/4/042010 Final published version
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Publication Year
2016
Language
English
Research Group
Team Raf Van de Plas
Volume number
753
Article number
042010
Publisher
Institute of Physics Publishing
Event
(2016-10-05 - 2016-10-07), Technische Universität München (TUM), Campus Garching, Munich, Germany
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Abstract

Trailing edge aps located outboard on wind turbine blades have recently shown considerable potential in the alleviation of turbine lifetime dynamic loads. The concept of the free-oating ap is speci_cally interesting for wind turbines, on account of its modularity and enhanced control authority. Such a ap is free to rotate about its axis; camberline control of the free-oating ap allows for aeroelastic control of blade loads. This paper describes the design of a scaled wind turbine blade instrumented with free-oating aps, intended for use in wind tunnel experiments. The nature of the ap introduces a coupled form of utter due to the aeroelastic coupling of ap rigid-body and blade out-of-plane modes; for maximal control authority it is desired to operate close to the utter limit. Analytical and numerical methods are used to perform a utter analysis of the turbine blade. It is shown that the potential ow aeroelastic model can be recast as a continuous-time Linear-Parameter-Varying (LPV) state space model of a low order, for which formal controller design methodologies are readily available.