1. Introduction
With a growing installation of high wind speed turbines globally, low and medium wind speed turbines are getting more attention [
1]. For low and medium wind speed conditions, specific wind turbines shall be designed to utilize the maximum possible wind potential of the site, to reduce loading and costs of energy [
2]. Fuglsang et al. showed the potential for a site-specific design that design loads and annual energy production depend on-site with considerably large maximum variations comparing two typical wind turbines at representative wind conditions. The study showed that site-specific turbines generated a smaller cost of energy than a fixed design turbine in every wind climate and appeared to offer great benefits for low-wind-speed sites. In addition to this, the study indicated that the redesign of only blades and towers results in significant reductions in the cost of energy and recommends designing particular wind turbines for low wind speed situations [
2]. Regardless of these, it is unmanageable to retain the standard rated-power of any wind turbine at its standard rated value at nonstandard air densities. Hence, to be used for nonstandard sites, it will require adapting to change the standard generator or using extenders with limitations [
3]. The cost of energy could also be minimized for onshore and offshore conditions, using a site-specific single wind turbine concept [
4].
On top of these, considering the cost of energy, site-specific wind turbine selection was also developed assuming the cost of energy model in terms of the radius of the rotor, hub height, and rated power as variables [
5]. For a fixed radius and hub height, the cost of energy increases with rated-power. On the other hand, a variation of lifetime cost could be estimated, in terms of changes in power rating with the assumption of an element of the cost fraction data that vary with changes of rated power [
6].
Numerical analysis methods for performance prediction shall be employed to design site-specific wind turbine blades. Computational fluid dynamics (CFD) and the blade element method (BEM) are commonly used numerical analysis tools for wind turbines. BEM is the most frequently used and computationally cheaper tool for designing and investigating the performance of wind turbine blades [
7,
8,
9]. CFD can be used to simulate the aerodynamic characteristics of wind turbine blades and examine the fluid-flows based on the Navier–Stokes equations [
9]. In solving the flow fields, Reynolds-averaged Navier–Stokes (RANS) equation is investigated mostly with two-equation turbulence models of the k-ε and k-ω series and four-equation transition k-ω SST (shear stress transport) turbulence model. The k-ε turbulence model is suitable for far-field flow simulations, while the k-ω turbulence model is appropriate in modeling the boundary layers. The transition k-ω SST turbulence model implements the k-ε model for far-field flows and k-ω model for boundary layers. It has mainly been used for the aerodynamic investigation of 3D wind turbine blades and confirmed with experimental results [
9,
10,
11].
Then, it is important to consider the performance measures to evaluate the aerodynamics of the blade. Among the different performance measures of wind turbines, power coefficient (CP), capacity factor (CF), and annual energy production (AEP) are the most common parameters. A review of the performance of small and large turbines shows that a power coefficient of approximately 25% and 45% respectively are depicted [
12]. Moreover, typical capacity factors are 20–40% with the values at the higher end of the range in mainly high wind sites [
13]. Capacity factors of 35–45% and 20–35% respectively of large and small wind turbines are also depicted [
14]. Several parameters affect the capacity factor of wind turbines, which include the generator size and inconsistency of the wind at the site. An inexpensive smaller generator would attain a higher capacity factor and produce a smaller amount of power in high wind speeds. On the contrary, a costly, big generator, which might stall out at low wind speed, would generate slight additional power [
15]. The simplified control mechanism and power characteristics of the turbine are also the main reasons for the low capacity factors of small wind turbines [
14].
On the other hand, as per the Danish wind industry association, having technically higher efficiency should not be an aim in itself for a wind turbine [
16]. With no need to save the free wind, what should matter is the cost of power production out of the winds during the lifetime of the turbine. Therefore, a turbine with the highest yearly energy production is not essentially an optimal one. Capturing a littlepower at higher wind speeds, a combination of a small generator with a large wind turbine could be harnessing power during several hours of the year. On the other hand, demanding a higher starting wind speed, higher efficiency at high wind speeds could be achieved [
16].
Therefore, attention should be given to the power density of the wind and wind speed distribution to fix the perfect arrangement of the size of the generator and turbine at various wind sites [
16]. Firstly, wind data of the sites should be reviewed in the design processes. Most of the potential methods of reviewing wind data of a particular site use direct or statistical techniques to assess the potential of the wind resource. Among these, the bins method, statistical analysis, development of velocity and power curves from data, and the direct use of averaged data are the most commonly used ones [
8].
On the other hand, controllers that can track maximum power are commonly used to ensure maximum energy yield and safety of the wind turbine. A review of the available maximum power point tracking algorithms shows that there are different options to consider depending on the parameters to control. These are tip speed ratio, optimal torque, power signal feedback, and perturbation and observation controls [
17]. Along with, for monitoring and maintenance purposes, the state of the wind turbine can be predicted using sensor measurements with repeat-accumulate coded communication methods remotely [
18]. A method of a particle filter, which is a nonlinear state estimator, can also be used to estimate the wind turbine parameters like rotor speed, tower top velocity, and tower top displacement [
19] to enhance the reliability of the wind turbines.
Even though a lot is done, on the aerodynamic design and analysis of small wind turbines, focusing on the power performance, site-specific conditions, the cost of energy, and related issues do not get due attention. Hence, considering these issues in the design and analysis process are expected to enhance the performance and reduce associated costs. Besides, for off-grid application with one or few installed turbines per site, designing and producing different wind turbine blades is costly for the reason that design and mold making costs are highly expensive when utilizing different blades than a single blade. On the other hand, for sites with various wind conditions, using a single blade at the design rated power might result in a higher cost of energy and low capacity factor than better possible ones.
Thus, the paper considers a single blade concept for use in all the sites in the catchment area. The bins and statistical methods are employed to the wind data of selected sites to characterize the wind condition.A proposed weighted average method is applied to create representative wind characteristics for designing the aerodynamics of the blade using a single blade concept. Catchment-based horizontal-axis wind turbine aerodynamics is analyzed implementing BEM using Matlab code validating it with CFD using Ansys-Fluent. The performance of the designed blade is evaluated based on the annual energy production, capacity factor, and power coefficient applying a maximum power point tracking mechanism. In the end, it examines the relationships between yearly energy production and rated power in terms of the site-specific wind conditions. It also assesses the performance of the blade at each site with the single blade concept and recommending rated-powers for a low cost of energy.
2. Materials and Methods
2.1. Study Area and Wind Data Sites
A study on wind energy resource potential shows that Ethiopia has total wind energy reserves of 3030 GW with exploitable potential of 1599 GW and installable potential of 1350 GW [
20,
21]. The sites considered in this paper are in the northern part of Ethiopia called Geba catchment located in the surrounding of the city of Mekelle, found at a latitude of 13.48° N, 39.49° E, and around 2208 m elevation. Wind data has been recorded at four wind measurement sites around Mekelle for at least two years. The summary of the selected study sites in the Geba catchment is as shown in
Table 1.
2.2. Wind Resource Characteristics
The bins method will be implemented based on the available records and best practice to summarize wind data. In addition to this, statistical methods are considered as per Manwell [
8] to define the wind energy potential of the sites and evaluated the expected turbine productivity of the designed wind turbine. Considering the wind data categorized into
Nb bins of width
, with midpoint wind speeds of
and frequency of occurrence
, in each bin, the total number of data
is defined as:
Then the average speed
and standard deviation
of the wind are defined as:
The average power density
is expressed as:
where
is the swept area of the rotor, and
is the density of air.
The average machine power
and the annual energy production by the rotor are then:
where
is the power produced defined by the power curve of the rotor, and
is the time of operation in a year.
In the statistical analysis, the probability distribution is used to describe the likelihood of the occurrence of certain wind speeds. The probability density function defines the probability of occurrence of wind speed between
and
. There are a few probability distributions in the literature to represent wind behavior. Among these, the Rayleigh and the Weibull are the most often used ones [
8]. The Weibull distribution, which needs information of two factors, a shape parameter
and shape factor
, better represents the wind behavior as it incorporates both the exponential and Rayleigh distributions [
8,
22].
The Weibull probability density function
and the cumulative distribution function
are defined as:
where the shape parameter
, for
, and the shape factor
, are defined as:
where
is gamma function defined:
.
Then, using the statistical methods, an equivalent value of the average machine power
Pw in Equation (5), is evaluated as:
which, in turn, is used to calculate capacity factor
that is a performance parameter of the wind turbine at a specific site, defined as the ratio of the average machine power to the rated power
over a given time. Thus:
2.3. Evaluating Representative Wind Parameters
Design and production of wind turbine blades are expensive for each different nearby sites with different wind resources or wind power production potentials within the same catchment area. Therefore, it is important to design a single blade based on a weighted average parameter of the wind potential of the sites. The weighted average parameter proposed in this paper wasthe wind power density per unit area of the selected sites within the catchment area. Therefore, the proposed weighting factor is:
where
is the weighting factor for site
, and
is the number of sites within the catchment area with available data.
Then, the representative parameters are the sum of the weighted parameters of each site. For instance, consider the midpoint wind speed of
, for the bins, the weighted average midpoint wind speeds
, is:
Based on these, weighted average values of the parameter wind bins, Weibull probability density function, and cumulative distributive function parameters will be available to design and analyze the representative small wind turbine blade.
2.4. Cost of Energy
The cost of energy (
CoE) is one of the key parameters required in the design and study of wind turbines, defined as the production cost of unit energy of the rotor [
8,
20]. Thus:
where
is the capital cost of the wind turbine,
is a fixed charge rate, and
is the operational cost.
In this paper, a variation of lifetime cost is estimated in terms of changes in power rating to evaluate relative-
CoE assuming elements of the cost fraction that vary with changes of rated power. Considering this assumption is reasonable for limited scopes related to cost effects. Hence, it is assumed that cost of power electronics varies proportional to the rated power. Blade cost also increases with power rating levels due to more cyclic loads around the rated-power and is likely to vary as to the square root of power [
6]. The gearbox is not considered in the scaling analysis as direct-drive small wind turbines are assumed. The costs applied are assuming the component level
CoE contribution reported by National Renewable Energy Laboratory (NREL) [
23]. Thus, relative-
CoE is defined evaluating Equation (13) accordingly as a ratio of nominal
CoE value of the respective sites. The rated power corresponding to a relative-
CoE of one offers the operation of the blade with minimum
CoE at the respective site.
2.5. Selection of Design Parameters
The paper aimed to design a 5 kW small wind turbine with appropriate parameters that suit the selected site conditions. Hence, the use of the best design parameters is very important to maximize the performance of the rotor. Among these, the tip-speed ratio and the number of blades are the most common ones that need careful selection. Hau and Barton et al. illustrates the variances in the efficiencies for rotors of different configurations qualitatively [
24,
25]. Accordingly, a three-bladed horizontal axis wind turbine at a tip-speed ratio of seven demonstrates maximum efficiency in comparison to the others. Therefore, a three-bladed wind turbine at a tip speed ratio of seven is the selected most efficient combination.
The design wind speed is another parameter that requires careful determination. There are different methods to select the design wind speed. For design considerations based on the wind classes, the International Electro-technical Commission (IEC) standard provides the average wind speeds for each wind class, and the design wind speed recommended is 40% more than the average wind speed [
26]. On the other hand, with available wind data for a specific site, the recommended practice is selecting the wind speed at around the highest power density. The practice based on the power density distribution allows us to design the blade at around wind speed corresponding to the highest wind power distribution. It will enable the wind turbine to harness the power at the wind speed with the highest power density at the optimized design. Usually, the mean wind speed of a specific site is slightly higher than the most repeated one. Thus, the design wind speed should be slightly higher than the one that corresponds to the densest wind power. This method of selecting design wind speed is a common practice in the wind-turbine design process [
27].
In addition to these density and the kinematic viscosity of air affects the design of wind turbines. For the selected catchment area, these values are taken based on the elevation, annual average temperature, and atmospheric pressure. Therefore, considering the data for environmental conditions of the Geba catchment, an average temperature of 23 °C and an atmospheric pressure of 760 hPa are considered. Accordingly, using the ideal gas law, an average air density of 0.92 kg/m3 and kinematic viscosity of 1.84 × 10−5 were found.
Airfoils are the major parts of the section requirements of the rotor blade design. These days it is easier to find and use existing airfoils for small wind turbine applications. National Renewable Energy Laboratory NREL (
wind.nrel.gov/airfoils) and other similar institutions have been developing some groups of airfoils for wind rotors. The airfoils with decent performance features for small rotors are listed in the literature [
15,
28,
29]. Hence, a set of airfoils of NREL, namely S823 and S822, developed for small wind turbines (2–20 kW) at various conditions, were found appropriate to the sites considered. A rectangular section is selected as the third airfoil to connect the rotor blades with the hub plate at the root part. Lift coefficient
Cl, and drag coefficient
Cd, at a specific angle of attack α that corresponds to around the maximum lift to drag ratio was taken for the NREL airfoils while the recommended force coefficient by the IEC 61400-2 2006 [
26] was considered for the rectangular section.
2.6. Blade Element Method and Iterative Process
The BEM is the most typically used method for the aerodynamic and aero-elastic study. Different modifications and improvements have been made, in the design of rotor blades, for better evaluation of forces and velocities. Madson and Dossing explained the BEM [
30,
31] that is also commonly available in the literature [
7,
8]. Therefore the modified BEM outlined by Madson and Dossing will be implemented [
30,
31], in combination with the tip loss factor modified by Shen [
32], which is a modification of the Glauert’s tip loss factor that gives an improvement in predicting the aerodynamic forces.
An iterative optimization process has been undertaken in two steps using Matlab code. The first step was the optimization process in the BEM. Here the tangential and axial induction factors have been the constraints required to converge to an ideal value within an acceptable tolerance level. The flow angle or the angle of attack, force coefficients, and element forces were variables to be determined and the tip speed ratio was considered as constant when designing for selected values. Taking the results of the first step as input, the second step considered the design power as the constraint. In the second step, the number of blades, wind velocity, density, and viscosity were the constants while the radius, angular velocity, and chord length were considered as variables.
2.7. CFD Modeling and Simulation
Ansys-Fluent, a widely used CFD modeling software, is used for the CFD simulation of the rotor. The CFD modeling considers one-third of a sector of the full cylindrical domain using one blade only with periodic boundary conditions to reduce computation time considerably.
Figure 1 shows the boundary conditions and computational-domain of the simulation. The cylindrical computational-domain at the upstream inlet waslocated in front of the blade at three times the blade radius (3R), and its diameter wasfive times the diameter of the blade (5D). On the downstream side, it waslocated at 10R behind the rotor blade with a computational domain cylinder diameter of 7D. These dimensions of the computational domain wereexpected to allow wake expansion and avoid unfavorable boundary dependency effects [
33,
34]. The rotational frame wasconsidered in the computational-domain to account for the rotor speed, with the blade taken as a non-slip wall boundary condition. Inflation layers of the prismatic type wereused forthe rotor face together with unstructured meshes for the computational-domain to get an improved resolution of the flow in boundary layers to get the wall distance y+ to be less than one [
34]. The wall distance y+ is a non-dimensional distance from the wall to the first mesh node used to describe the height of the first grid element next to a wall in a CFD simulation.
In CFD simulations of wind turbine blades, the fluid-flow was analyzed based on the Navier–Stokes equations. RANS equation is investigated usually with either two-equation turbulence models of the k-ε and k-ω series or four-equation shear stress transport k-ω SST turbulence model. The k-ε turbulence model could not depict flows at the boundary layers accurately. It is, therefore, suitable for far-field flow simulations. On the other hand, the k-ω turbulence model could not represent far field flows precisely. Hence, it is appropriate for modeling the boundary layers. The transition k-ω SST turbulence uses the k-ε model and k-ω model alternatively depending on the flow condition. It has the capability of flow separation forecasting on the rotor and reflects the effect of free-stream pressure gradients and turbulence [
33,
35,
36]. Therefore, a four-equation shear stress transport, k-ω SST turbulence model, was employed in the CFD analysis. As per the assessment and investigations of different researchers, the k-ω SST turbulence model was reliable for flow analysis with good agreement with experimental results. However, at large angles of attack, it was confirmed that the CFD simulation results tend to slightly underpredict the power and overpredict the thrust [
37,
38,
39,
40,
41]. An incompressible analysis was employed, as most of the wind turbine operation is in the subsonic region, with a constant local air density and viscosity. A coupled algorithm for pressure, which considerably increases the convergence rate, was considered in solving the incompressible Reynold-averaged Navier–Stokes (RANS) model [
33,
42].
Residuals and net mass imbalance were engaged to limit the running time of the solver and ensure convergence. Residuals of the specific dissipation
ω, the kinetic energy turbulence
k, velocities, and continuity were limited to less than 10
−4 during the solution process. In addition to these, the net imbalance was also checked to be below 0.1% [
33,
37,
43], and an integral static pressure surface monitor to remain constant for a considerable amount of iterations after convergence.
Furthermore, ASHES (simis.io) was employed as an off-design performance evaluation tool. It is a time-domain wind-turbine aerodynamics module, which uses AeroDyne of FAST with a rich user interface. Parameters like a chord, twist angle, pitch axis, airfoil type, and shapefiles of the airfoils at their corresponding radial positions from Matlabwere exported to ASHES as input in the table format. It internally implements xfoil to determine the lift and drag constants for the shapefiles to get the necessary parameters in the evaluation process.
4. Conclusions
Catchment based aerodynamically optimized small wind turbine was designed using representative wind conditions. The proposed weighting average was based on the wind power density of the wind sites within the catchment area. The blade design was applying the single blade concept and low cost of energy. In designing, BEM was implemented using Matlab code to optimize the local chords, twist angles, radius, and rotational speed of the turbine and exported to Ansys for CFD analysis. Ansys-Fluent was applied to validate the results of BEM, and good agreement found for the power coefficient for a different combination of wind speeds.
Accordingly, the maximum power coefficient achieved was around 51.8% at a design wind speed of 10 m/s. Considering the single blade concept for all the sites within the catchment area, the performance of the blade at a rated power of 5 kW resulted in capacity factors ranging from 18.8% to 50.2%. Therefore, analyzing the relationship between rated power against annual energy production, capacity factor, and relative cost of energy, a range of appropriate rated power that would give a low cost of energy at higher performances recommended for each site. It can be concluded that for Mekelle and Dera sites, which are low wind sites, rated-powers of 3.5 kW and 3 kW are appropriate at rated wind speeds of 8.8 m/s and 8.4 m/s, performing at capacity factors around 25.1% and 31.8% and corresponding annual energy production around 7.3 and 8.4 in MWh, respectively. While optimum rated-power of 5 kW would be proper for the Mayderhu site at 10 m/s rated wind speed, executing with a capacity factor around 38.6% and annual energy production around 16.9 MWh. On the other hand, as the Hagereselam site is a relatively high wind site, rated power of 6 kW would be proper at 10.5 m/s rated wind speed that would achieve a capacity factor of 45.9% and annual energy production of 24.1 MWh.
Even though the performance of the blade at the Mekelle site was low relative to other wind sites in the catchment, it was moderate to high compared to the most commonly reported wind turbines. On the other hand, the performance at the Hagereselam site was the highest in the catchment area considered and high compared to the existing wind rotors. As the Mayderhu wind condition is very close to the representative weighted average of all sites used for designing the blade, the performance was found very close to the results at design conditions.
In conclusion, it is possible to achieve high performance at a low cost of energy using a single blade concept at appropriate rated power, implementing proper design conditions and procedures for different sites with different wind conditions.