posted on 2022-09-23, 07:23authored byJeremiah Michael O'Brien
The simulation of the complex
flow in the wake of a Horizontal Axis
Wind Turbine and how it infuences the structural response of the
blades is a challenging problem. The difficulty of this problem is
further increased when the scale of modern turbine facilities is considered.
The substantial size of turbine blades has meant that design
tools have had to evolve from simple static calculations that assume
a constant wind loading to detailed dynamic calculations that take
into account the unsteady aerodynamic loads and aeroelastic response
of turbine blades. The Shear Stress Transport (SST) k-w,
Reynolds Stress Transport (RST) and Elliptical Blending-Reynolds
Stress Model (EB-RSM) turbulence models were used to model a
turbine wake in the current study, with the results verified against
experimental hot-wire data. The numerical data was compared to
experimental results for two Tip Speed Ratio (TSR) values of 2.54
and 3.87. The experimental investigation focused on the near field
wake with data taken from 0.66D (D is defined as the rotor diameter)
to 1.5D downstream. Initial comparisons show that the use of
high delity models is not required to predict the turbulent characteristics
of the
flow and that all models predicted rms velocities
and u'v' Reynolds Stresses to the correct order of magnitude. All
models proved capable to predict Reynolds stress values in the wake
with percentage errors ranging between -34% and 17% over the two
TSR values.
In addition to increasing the difficulty of aerodynamic modelling of
wind turbines, larger blades increase blade
flexibility and increase
the complexity of structural models also. Currently, due to the size
of blades, no data is available to the research community regarding
their structural properties and performance during operation.
Data such as this will be required to validate larger structural models
in the future. A novel methodology was adopted to benchmark
a Fluid-Structure Interaction (FSI) model of a representative 2.5
MW commercial wind turbine. The method involved comparing
blade deflection data from a field turbine, similar in size to the numerical
model. It was proposed that blade defection data (recorded
in the field) of a similar sized turbine to the numerical model could
be used to evaluate the performance of the numerical model. This
would also give opportunity to the research community to deviate
from the current process of validating structural models against previous
numerical works. Blade defection data was recorded from an
operating Nordex N90 wind turbine and used to benchmark a numerically
modelled 2.5 MW class turbine. The method involved
coupling both a structural model developed in the Finite Element
(FE) solver ABAQUS and an aerodynamic model developed in the
Finite Volume (FV) solver Star CCM+. The FSI model was carried
out with one-way coupling between both solvers. The FSI model
was shown to behave correctly with blade deflection values in front
of the tower structure falling within one standard deviation of the
mean recorded field deflection values.
The influence of the blade/tower interaction was also investigated.
The tower shadow was shown to effect a significant portion of each
blade's rotation cycle (roughly 40 left and right of the tower centre)
and caused a reduction in blade moment up of to 29%. The passing
of the blade in front of the tower structure effectively pushed the
tower stagnation point off centre and resulted in a periodic reduction
in the pressure loads applied to the tower.
Funding
Using the Cloud to Streamline the Development of Mobile Phone Apps