Keywords

1 Introduction

Humanity has known for ages how useful wind power can be in daily life, from sailboats to windmills. Developing and designing vertical axis wind turbines have been the subject of several research projects. Among the few investigations, two were emphasized here and categorized as computational studies and experimental studies. Due to population increase and the expansion of economies, the world's energy demand is anticipated to more than quadruple by 2060. Lift-based Darrieus VAWT design is more frequently utilized since it has larger power coefficients [1]. Darrieus VAWTs typically fall into one of two categories based on blade configuration: both straight and curved blades. Straight line blades, in particularly the H-rotor types, have gained popularity because of how easily they can be produced. On employing VAWT, maximum power coefficient can be achieved, but on the other hand, construction, operation, and cost of manufacturing are crucial considerations when choosing VAWTs as in [2] for power production. Power generation expenses will be decreased by raising the power coefficient of VAWTs and HAWTs.

2 Problem Statement

The present analysis incorporates the formation of vorticity in the wind turbines and the intensity of vortices in the tip and the root of the blades. Unlike the aircrafts, the vortex in the wind turbine blade is of different structures and it is an important aspect of study the vortex structure in the blades. The airfoils chosen are S833, S834, and S835 of the NREL series. Also, vorticity formation due to the upstream flow or the wind speed is analyzed and an insight on ways to reduce the vortices is given. The turbulence analysis is included in the paper and the corresponding results are provided.

3 Methodology

The paper is expected to exhibit the study of vortex formation in the wind turbines. Initially, the blade is designed with S833, S834, and S835 airfoils separately and the simulation is done with four different wind speeds, and the vortices’ formations are obtained. The turbulence models are taken and analyzed [3]. These airfoils are made with the intention of having a constrained maximum lift and a minimal sensitivity to leading-edge roughness [4]. In the past, an analysis for this type of wind turbine was performed where the analysis was performed for HAWT with a NACA airfoil. However, in this study, the HAWT blade type is chosen and S833, S834, and S835 airfoils are picked, and they are then given an aerodynamic analysis [5]. The vortex formations in the wind turbine is a function of wind speed which is why the analysis involves choosing different wind speeds in order to provide the best airfoil for wind turbines.

4 Code QBlade

The turbulence analysis and vorticity formation were simulated in QBlade. It is a wind turbine design and simulation software. QBlade is a software that helps to design wind turbine and maximizes all the key relations between blade twist, chord, section airfoil performance, turbine control, power, and load curves in a clear and understandable manner.

5 Theory

For quantitatively predicting liquid and gas flows in many industrial applications, Computational Fluid Dynamics (CFD) is a potent tool. Air flows around wind turbines to produce renewable energy by turning the turbine blades, which is an obvious application of CFD in wind energy.

5.1 Vorticity

The vortex flow is that type of flow in which the fluid particles take a rotational motion during its flow separation from the fluid–solid interaction. Free vortex flow and forced vortex flow are the two types of vortex flows, whereas in forced vortex flow, the fluid particles rotate in its own axis by means of the external torque applied to the fluid flow. Tangential velocity acting on the fluid,

$$v=\omega r.$$
(1)

The analysis is based on the formation of vortices in the wind turbine which replicates the number of vortex filaments that has formed during the flow separation in the wind turbine blades. The vortices are developed is formed in the downstream of the blades which induces a velocity at some points by Biot–Savart law.

$${\text{d}}\vec{v} = \frac{\Gamma }{4\pi }\frac{{\overrightarrow {{d_{l} }} X\vec{r}}}{{r^{3} }}$$
(2)

By integrating the above expression, the velocity relation is obtained

$$v = \frac{\Gamma }{4\pi }\mathop \smallint \limits_{ - \infty }^{\infty } \frac{\sin \vartheta }{{r^{2} }}{\text{d}}l$$
(3)

The Lifting Line Free Vortex Wake technique may be used in QBlade to mimic the aerodynamic forces operating on a rotor (LLFVW). The FVW approach used in this study solves for the turbine wake. The FVW model is derived from Lagrangian method (Fig. 1).

Fig. 1
An illustration of the L L F V W model. It depicts a plane with a grid. The left side is labeled bound vorticity, the top is labeled trailing vorticity and the bottom is labeled shed vorticity.

LLFVW model

6 Results and Discussions

In this analysis, geometric models of the airfoils have been created and vortex formations in the wind turbines are simulated for three different turbine blade geometries. According to the author’s knowledge, it is found theoretically that the number of vortex filaments formed across the wake of the blade is inversely proportional to the wind speed.

6.1 Geometric Model

The below given figure shows the blade design of the airfoils S833, S834, and S835:

  1. 1.

    S833 (Fig. 2).

    Fig. 2
    An illustration of a S 833 blade. It depicts a rectangular base with two slanting edges that lead to a narrow tip.

    S833 blade

  1. 2.

    S834 (Fig. 3).

    Fig. 3
    An illustration of a S 834 blade. It depicts a narrow rectangular base with two slanting edges that lead to a narrow tip.

    S834 blade

  1. 3.

    S835 (Fig. 4).

    Fig. 4
    An illustration of a S 835 blade. It depicts a narrow rectangular base with a broad slanting upper edge that leads to a narrow tip.

    S835 blade

6.2 Vortex Simulations

The vortex simulations for four different wind speeds are shown:

  1. (1)

    Airfoil: S833 speed of wind in m/s

    1. 1.

      Speed of wind: 10 (Fig. 5).

      Fig. 5
      A computer model of the vortex formation of S 833 open parenthesis 10 close parenthesis. The vortex is depicted as a circular net behind the blades of the windmill.

      Vortex formation of S833 (10)

    2. 2.

      Speed of wind: 12 (Fig. 6).

      Fig. 6
      A computer model of the vortex formation of S 833 open parenthesis 12 close parenthesis. The vortex is depicted as a circular net with spaces between the net behind the blades of the windmill.

      Vortex formation of S833 (12)

    3. 3.

      Speed of wind: 14 (Fig. 7).

      Fig. 7
      A computer model of the vortex formation of S 833 open parenthesis 14 close parenthesis. The vortex is depicted as a circular net with spaces between the net that are less prominent behind the blades of the windmill.

      Vortex formation of S833 (14)

    4. 4.

      Speed of wind: 16 (Fig. 8).

      Fig. 8
      A computer model of the vortex formation of S 833 open parenthesis 16 close parenthesis. The vortex is depicted as an extended circular net with spaces between the net behind the blades of the windmill.

      Vortex formation of S833 (16)

6.3 Turbulence Graphs

The graphs of blade length versus circulation, time versus induced velocity, and time versus vortex filaments for S833 are given below (Figs. 9, 10 and 11):

Fig. 9
A multiple-line graph of circulation versus blade length for four legends. All depict an increase in circulation. The maximum circulation is observed for 16 m per s, approximately above 6.00 E plus 00.

Plot of blade length versus circulation

Fig. 10
A multiple-line graph of induced velocity versus time for four legends. All depict a decreasing trend after a peak and the maximum decrease in induced velocity is observed for 10 m per s.

Plot of time versus induced velocity

Fig. 11
A multiple-line graph of vortex filaments versus time for four legends. All depict an increasing trend with the maximum vortex filament for 10 m per s.

Plot of time versus vortex filaments

  1. (2)

    Airfoil: S834

    1. 1.

      Speed of wind: 10 (Fig. 12).

      Fig. 12
      A computer model of the vortex formation of S 834 open parenthesis 10 close parenthesis. The vortex is depicted as a circular net with spaces between the net that are less prominent behind the blades of the windmill.

      Vortex formation of S834 (10)

    2. 2.

      Speed of wind: 12 (Fig. 13).

      Fig. 13
      A computer model of the vortex formation of S 834 open parenthesis 12 close parenthesis. The vortex is depicted as a circular net with spaces between the net that are more prominent behind the blades of the windmill.

      Vortex formation of S834 (12)

    3. 3.

      Speed of wind: 14 (Fig. 14).

      Fig. 14
      A computer model of the vortex formation of S 834 open parenthesis 14 close parenthesis. The vortex is depicted as an extended circular net with spaces between the net that are more prominent behind the blades of the windmill.

      Vortex formation of S834 (14)

    4. 4.

      Speed of wind: 16 (Fig. 15).

      Fig. 15
      A computer model of the vortex formation of S 834 open parenthesis 16 close parenthesis. The vortex is depicted as an extended circular net with spaces between the net that are more prominent behind the blades of the windmill.

      Vortex formation of S834 (16)

6.4 Turbulence Graphs

The graphs of blade length versus circulation, time versus induced velocity and time versus vortex filaments for S834 are given below (Figs. 16, 17 and 18):

Fig. 16
A multiple-line graph of circulation versus blade length for four legends. All depict an increasing trend. The legend 16 m per s depicts the maximum increase.

Plot of blade length versus circulation

Fig. 17
A multiple-line graph of induced velocity versus time for four legends. All the four legends peak up to 1.60E plus 00 initially and then decrease.

Plot of time versus induced velocity

Fig. 18
A multiple-line graph of vortex filaments versus time for four legends. All depict an increasing trend.

Plot of time versus vortex filaments

  1. (3)

    Airfoil: S835

    1. 1.

      Speed of wind: 10 (Fig. 19).

      Fig. 19
      A computer model of the vortex formation of S 835 open parenthesis 10 close parenthesis. The vortex is depicted as a circular net with fewer spaces between the net behind the windmill's blades.

      Vortex formation of S835 (10)

    2. 2.

      Speed of wind: 12 (Fig. 20).

      Fig. 20
      A computer model of the vortex formation of S 835 open parenthesis 12 close parenthesis. The vortex is depicted as a circular net with fewer spaces between the net behind the windmill's blades.

      Vortex formation of S835 (12)

    3. 3.

      Speed of wind: 14 (Fig. 21).

      Fig. 21
      A computer model of the vortex formation of S 835 open parenthesis 14 close parenthesis. The vortex is depicted as an extended circular net with fewer spaces between the net behind the windmill's blades.

      Vortex formation of S835 (14)

    4. 4.

      Speed of wind: 16 (Fig. 22).

      Fig. 22
      A computer model of the vortex formation of S 835 open parenthesis 16 close parenthesis. The vortex is depicted as an extended circular net with spaces between the net behind the windmill's blades.

      Vortex formation of S835 (16)

6.5 Turbulence Graphs

The graphs of blade length versus circulation, time versus induced velocity, and time versus vortex filaments for S835 are given below (Figs. 23, 24 and 25):

Fig. 23
A multiple-line graph of circulation versus blade length for four legends. All depict an increasing trend.

Plot of blade length versus circulation

Fig. 24
A multiple-line graph of velocity induced from blade 1 versus time for four legends. All the legends peak initially up to 2.00E plus 00 and then decrease.

Plot of time versus induced velocity

Fig. 25
A multiple-line graph of the number of vortex filaments versus time for four legends. All the legends depict an increasing trend.

Plot of time versus vortex filaments

7 Conclusion

The vorticity formation for the three airfoils has been obtained along with the graphs to study turbulence. The vortices formed during the working of a wind turbine affect the performance of it. Hence, it is essential to analyze and study ways to reduce them. From this analysis, it is found that distance between the wind turbine and the formation of vortex filaments is lesser at low wind speeds and formation of vortex filaments which is at high wind speeds is farther from the wind turbine. During the blade rotation, there is formation of vortices’ downstream of wind turbine. By comparing the airfoils S833, S834, S835 based on the formation of vortex filaments, it is found that for S834 airfoil, the distance between the formation vortex filaments and wind turbine is more at low wind speeds, whereas for S833 and S835 airfoils, the distance is less at low wind speeds.