Free-flow wind speed from a blade-mounted flow sensor
This paper presents a method for obtaining the free-inflow velocities from a 3-D flow sensor mounted on the blade of a wind turbine.</br></br>From its position on the rotating blade, e.g. one-third from the tip, a blade-mounted flow sensor (BMFS) is able to provide valuable informati...
Main Authors: | , , , |
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Format: | Article |
Language: | English |
Published: |
Copernicus Publications
2018-03-01
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Series: | Wind Energy Science |
Online Access: | https://www.wind-energ-sci.net/3/121/2018/wes-3-121-2018.pdf |
Summary: | This paper presents a method for obtaining
the free-inflow velocities
from a 3-D flow sensor mounted on the blade of a wind turbine.</br></br>From its position on the rotating blade, e.g. one-third from the tip,
a blade-mounted flow sensor (BMFS) is able to provide valuable
information about the turbulent sheared inflow in different regions of
the rotor. At the rotor, however, the inflow is affected by the wind
turbine, and in most cases the wind of interest is the inflow that the
wind turbine is exposed to, i.e. the free-inflow velocities.</br></br>The current method applies a combination of aerodynamic models and
procedures to estimate the induced velocities, i.e. the disturbance of
the flow field caused by the wind turbine. These velocities are
subtracted from the flow velocities measured by the BMFS to obtain the
free-inflow velocities. Aeroelastic codes, like HAWC2, typically use
a similar approach to calculate the induction, but they use it for the
reversed process, i.e. they add the induction to the free inflow to get
the flow velocities at the blades, which are required to calculate the
resulting aerodynamic forces.</br></br>The aerodynamic models included in the current method comprise models
based on blade element momentum (BEM) for axial and tangential
induction, a radial induction model and tip loss correction, and
models for skew and dynamic inflow.</br></br>It is shown that the method is able to calculate the free-inflow
velocities with high accuracy when applied to aeroelastic HAWC2
simulations with a stiff structural model while some deviations are seen
in simulations with a flexible structure.</br></br>Furthermore, the method is tested on simulations performed by a flexible
structural model coupled with a large-eddy simulation (LES) flow
solver. The results of this higher-fidelity verification confirm the
HAWC2-based conclusion. |
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ISSN: | 2366-7443 2366-7451 |