posted on 2017-03-27, 04:45authored byJasvipul Singh Chawla
This thesis seeks to
arrive at estimates of improvement in blade aerodynamic efficiency and
reduction in structural loads in small wind turbines through surface
suction-based active flow control at low Reynolds numbers (Re). Improved
aerodynamic efficiency and reduced fatigue loads help achieve lower
Cost-of-Energy.
Small wind turbines typically operate off-grid, providing power
at the point of consumption. Consequently, such turbines often operate in
locations with poor wind speed regimes. Low wind speeds coupled with small
chord length of the blades result in low operating Re that often lie between
104 and 105. It is well-known that such operating Re imposes significant
challenges in realising good aerodynamic efficiency due to the propensity for
flow separation to occur.
It has been established that flow separation can be avoided
or delayed using active flow control. However, much of such work on active flow
control has focused on high Re applications. This thesis focuses on the
application of surface suction, a popular active flow control methodology, in
low Re regimes seen in small wind turbines.
The approach adopted towards
arriving at the aforementioned estimates of improvement in blade aerodynamic
efficiency and reduction in structural loads in small wind turbines is as
follows:
1. Experimental characterisation of the improvement in the
aerodynamic characteristics of two aerofoil profiles, NACA0012 and S814,
commonly used in small wind turbine applications, in low Re regimes is
performed. Specifically, this characterisation captures both the steady-state
characteristics as well as identification of the temporal dynamics between
change in the coefficient of lift (ΔCL) and change in the coefficient of drag
(ΔCD) with the non-dimensional parameter, Cμ (defined as the ratio of the
momentum of air drawn through suction and the momentum of the air flowing over
the aerofoil, that is, ρAslitus2) / ( ρ AaerofoilU∞2), where ρ
is air density, Aslitarea of the slit, Aaerofoil area of the aerofoil, us
suction velocity and U∞ the free stream velocity):
ΔCL, ΔCD = f(Cμ)
ΔCL, ΔCD = f(Cμ,t)
2. Posing a similitude argument that as long as the
dimensionless parameters Cμ and Re remain comparable to the regimes for which
the aforesaid experimental characterisation was done, the steady-state and
temporal relationships between ΔCL, ΔCD and Cμ established could be directly
used in numerical simulations for predicting the behaviour of small wind
turbines.
3. Using the relation ΔCL, ΔCD = f(Cμ) and steady Blade
Element Momentum (BEM) theory to estimate increase in Coefficient of Power, CPof a small wind turbine employing surface suction on its blades working in the
same Cμ,Re regime.
4. Incorporating the dynamic map, ΔCL, ΔCD = f(Cμ,t) into
the dynamics of the aero-elastic simulator, FAST to formulate extended turbine
dynamics.
5. Utilising, appropriately, Cμ as an additional control
input towards reducing fore-aft oscillations of the tower top while
compensating for the said extended turbine dynamics.
6. Demonstrating, through rain-flow analysis, that the
reduced oscillations result in mitigation of fatigue loads on the turbine tower
structure.
The thesis documents that the approach indicated for
increasing CP , when applied to a small wind turbine in sub 1kW power output
range, with 2m radius, NACA0012-blades, operating in steady wind speed of
7.5m/s, increased the expected power output from 764W to 1511W by expending
106W of suction power.
Further, compensating for the extended dynamics of the
turbine in the aero-elastic simulator, tower-top oscillations reduced for a ~
10kW turbine of 2.9m radius, S814 blades, hub height 24m. Thus, for the turbine
operating over 20 years in turbulent IEC III-A wind conditions, the structural
damage equivalent reduced from ~ 10 to < 1.
History
Campus location
Australia
Principal supervisor
John Sheridan
Additional supervisor 1
Shashikanth Suryanarayanan
Year of Award
2017
Department, School or Centre
Mechanical and Aerospace Engineering
Additional Institution or Organisation
Indian Institute of Technology Bombay, India (IITB)