Numerical Study of the Three-dimensional Flow in a Flat Plate Solar Collector with Baffles

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Numerical Study of the Three-dimensional Flow in a Flat Plate Solar Collector with Baffles M.A. AMRAOUI a, K. ALIANE b a. Department of Mechanical Engineering, Faculty of Technology, University of Tlemcen, Algeria. amraoui_mohammedamine@yahoo.fr b. Department of Mechanical Engineering, Faculty of Technology, University of Tlemcen, Algeria. kh_aliane@yahoo.fr Abstract: This paper presents the study of fluid flow and heat transfer in solar flat plate collector by using Computational Fluid Dynamics (CFD) which reduces time and cost. In the present paper the computational fluid dynamics (CFD) tool has been used to simulate the solar collector for better understanding the heat transfer capability. 3D model of the collector involving air inlet, the collector is modeled by ANSYS Workbench and the grid was created in ANSYS ICEM. The results were obtained by using ANSYS FLUENT and ANSYS CFX. The objective of this work is to compare theoretically and experimentally work done with the work done by using computational fluid dynamics (CFD) tool with respect to flow and temperature distribution inside the solar collector. The outlet temperature of air is compared with experimental results and there is a good agreement in between them. Key Words: Flat plate solar collector, Fluid flow, k_ε turbulent model, CFD 1 Introduction Flat-plate collectors are the most common solar collector for solar water-heating systems in homes and solar space heating. A typical flat-plate collector is an insulated metal box with a glass or plastic cover (called the glazing) and a dark-colored absorber plate. These collectors heat liquid or air at temperatures less than 80 C. The use of artificial roughness on a surface is an effective technique to enhance the rate of heat transfer to fluid flowing in a duct (Nikuradse, 1950[6]; Nunner, 1958[1]; Dipprey and Sabersky, 1963[2]; Webb and Eckert, 1972[3]; Han, 1984[4]; Hosni and al., 1991[5]). Roughness elements have been used to improve the convective heat transfer by creating turbulence in the flow. However, it would result in an increase in friction losses and hence, greater power requirement by fan or blower. In order to keep the friction losses at a minimum level, the turbulence must be created only in the region very close to the surface i.e. in laminar sub-layer. The surface roughness can be produced by several methods, such as sand blasting, machining, casting, forming, welding ribs and wires along the surface. Different types of wire, rib or wire mesh with different shapes, orientations and configurations on the surface are used to create required roughness. S.V. Karmare and al [6]presents a study of fluid flow

and heat transfer in a solar air heater by using Computational Fluid Dynamics (CFD) which reduces time and cost. In this analysis collector plate is made rough with metal ribs of circular, square and triangular cross-section, having 600 Inclination to the air flow. The grit rib elements are fixed on the surface in staggered manner to form defined grid. To validate CFD results, experimental investigations were carried out in the laboratory. The experimental results of the roughened solar air heater are compared with CFD analysis results. The square cross-section ribs with 580 angle of attack give maximum heat transfer. The percentage enhancement in the heat transfer for square plate over smooth surface is 30%. The unglazed transpired solar air collector is now a well-recognized solar air heater for heating outside air directly, Chongjie Wang and al [7] introduced numerical simulation tools into the solar air collector research area, analyzed the performance characteristics of the unglazed transpired solar air collector and compared them with several kinds of traditional solar air collectors. The results showed that the unglazed transpired solar air collector has unparalleled advantages in the ventilation preheating area and also proves that CFD tools have their own advantages in the solar air collector research area. The success of the solar energy applications is closely related to the performance of the collectors which convert it. For the collectors whose caloporting fluid is water; thermal transfer is made suitably because water is a good conductor of heat. However, for solar air collectors, heat transfer is low. In this paper, we show the design of air collector on which it is possible to act to improve the heat transfer between the absorber and the caloporting air and thus to favor the energetic efficiency while assuring a maximum increase of temperature. we will introduce of baffles by simulation We observe the formation of a meandering flow. In this case, it is clear that the length of the trajectory is more than double that of the collector, thus increasing the air speed and the heat transfer. On the other hand,the size of the dead zones is considerable. 2 Problematic 2.1 Geometry The model of the solar collector has been studied experimentally by [8]. The air flow moves between the insulation and the absorber, with two types of baffles. Baffles arranged transversely to the insulation 80% of each occupant collectors width (Fig. 1), a rectangular shape, and which have the same height as the passage, they are five in number arranged in a labyrinth. Baffles small size 50x25 mm, of rectangular shape, placed in the space between those of larger sizes, in other words in the compartments of the labyrinth. 2.1.1 The collector - length (L)=900 mm. - width (l)=500 mm. - height of the flow path=25 mm. 2.1.2 The baffles - the space between the baffles forming the labyrinth=150 mm - the space between the baffles small=30 mm. - height baffles=25 mm.

Figure 1. Sketch for the solar collector. 2.2 The boundary conditions As the flow is turbulent, k ε model is selected as turbulent model for further analysis of the problem. No slip condition is applied to all the walls. According to the models selected earlier the equations which were going to be solved by continuity equation or energy equation or momentum equation or equation for turbulence. To solve these equations, under-relaxation factors are used: -The velocity of the air at the inlet: u 0 = 0.02216 m / s corresponding for rate flow 79.79 m 3 /hm 2 -The air temperature at the inlet Te = 300 K -The turbulent kinetic energy at inlet -The energy dissipation at inlet -The temperature of the absorber: Tabs = 380 K (corresponding to a solar flux value equal to 800w/m2). -The temperature of the insulation and the lower baffle: Tiso = 340 K -The outlet pressure: Ps = Patm 2.3 Mesh Meshing of the domain was done using ANSYS, with non-uniform quad grid of 1 mm grid size. This size was suitable to resolve the laminar sub-layer. A general practice is to use fine mesh size in the area where greater details are desired such as fins and coarse mesh in areas of small changes in domain geometry. Non uniform high density mesh in inter fin region and on edges and corners were employed while low density mesh was adapted in the smooth wall regions. The mesh density for the CFD analyses was kept at 51 x 34 x 2. This helped in economizing the number of cells needed for acceptable computational time and computer memory, Figures 2and 3 show the grid pattern for the flow domain.

Figure 2.3D mesh of Solar Flat Plate Collector Figure 3.Flow domain with Baffles arranged transversely and Baffles small 3 Discussions and interpretations The results obtained from the CFD analysis of solar flat plate collector are presented in this section. The simulation is carried out for different flow. Then the results obtained by this simulation compared with the experimental results as shown in Table I. It seems that the difference between experimental and simulated outlet temperature for different flow is almost 4 C. Flow m 3 /hm 2 Table 1. comparıson of experımental and cfd results Collector temperature obtained by CFD( C) Collector Temperature [17] ( C) Q1=79.79 53 50 Q2=58.97 62 58 Q3=23.71 69 68 3.1 Temperatures Field The temperature distribution is obtained by CFD simulation. The contour plots obtained for temperature distribution is given by Fig 4. As air passes above absorber the heat exchange takes place from the surface to air. The air very close to surface gets heated due to convection. This primary hot layer mixes with the secondary cold air due to baffles, and heat transfer takes place due to conduction and convection. As a result the temperature of air close to surface is higher, and goes on decreasing away from the surface up to one third height of the duct. Fig. 5 shows the distribution of the temperature field for a cross section in the plane X, Z At the entrance, the air has a temperature of 300K, it begins to apply heat across half the distance between the inlet and the first transverse baffle it reaches a temperature of 335K, bypassing the latter, it reaches a temperature of about 350K. bypassing the latter, it reaches a temperature of about 350K. bypassing the

latter, it reaches a temperature of about 350K. In conclusion follows that the flow of air keeps the same temperature (350 k), they cross the rows of baffles until exit. Intel flow Figure 4.Temperatures Field for the collector Figure 5. Temperatures Field (plane X, Z). 3.2 The velocity vector V In this case (Fig.6 ), it is clear that the length of the trajectory is more than double that of the collector thanks baffles, thus increasing the air speed. On the other hand, the size of the dead zones is considerable. To cure the problem of the large dead zones, let us introduce longitudinal baffles which will extend the flow and will reduce the extent of the dead zones to a minimum. The efficiency is very much increased. Figures 7 shows the shape of the current lines of different turn baffles and small transverse baffles Figure 7 shows that the current lines are going to turn will trais small baffles which flow in axillary such that the place due to the narrowing of the flow section in this area. while transverse baffles promotes the appearance of an undesirable recirculation zone. Figure 6. Velocity distribution. Figure 7.Streamlines for velocity distribution.

3.3 Turbulent kinetic energy (k) and Turbulent eddy dissipation (ε) The distribution of turbulent kinetic energy (k) is given by fig.8, it is clear that the flow has a turbulent kinetic energy throughout their trajectory. There is a considerable increase of turbulent kinetic energy in baffles small. Turbulent eddy dissipation (ε) is given in Fig 9. This dissipation varies between 6,03.10-6 m2/s3 and 1,32.10-1 m2/s3. There is a significant dissipation over the vicinity of the small baffles. Figure 8.Turbulent kinetic energy (k) Figure 9.Turbulent eddy dissipation (ε) 4 Conclusions From the various viewpoints encountered in the study of solar air collectors, it becomes evident that the introduction of suitable baffles in solar air collectors increases the couple efficiency increase in temperature. These baffles, placed in the air channel situated between the insulator and the absorber, have the particularity of extending the trajectory of the circulation, to keep the caloporting air constantly in contact with the absorber, and finally to play the role of wings and improving the heat transfer from the absorber to the caloporting air. There is a good agreement between the experimental and simulated results for outlet air temperatures. Although there are some small discrepancies due to some experimental imperfectness matters, we still have a good confidence in the CFD simulation program that can be used in the future for more complex solar collector problem. Références [1] Nunner, W., 1958, Laws of Flow in Rough Pipes, VDI ForschHft B 455, 5 39 (A.E.R.E. Lib. Trans. 786).

[2] Dipprey, D.F., Sabersky, R.H., 1963, Heat and momentum in smooth and rough tubes at various Prenatal numbers, Int. J. Heat Mass Transfer 6, 329 353. [3] Webb, R.L., Eckert, E.R.G., 1972, Application of rough surfaces of heat exchanger design, Int. J. Heat Mass Transfer, 5, 1647 1658 [4] Han, J.C., 1984, Heat transfer and friction in a channel with two opposite rib roughened walls, Int. J. Heat Transfer, 106, 774 781 [5] Hosni, M.H., Hugh, W.C., Robert, P.T., 1991, Measurement and calculations of rough wall heat transfer in the turbulent boundary layer, Int. J. Heat Mass Transfer, 34, 1067 1082 [6] S.V. Karmare, A.N. Tikekar, Analysis of fluid flow and heat transfer in a rib grit roughened surface solar air heater using CFD, Solar Energy, 84 (2010) 409 417 [7] Chongjie Wang Zhenzhong Guan Xueyi Zhao Delin Wang, Numerical Simulation Study on Transpired Solar Air Collector, Renewable Energy Resources and a Greener Future, Vol.VIII-3-4,2006. [8] Moummi Abdelhafid, Etude globale et locale du rôle de la géométrie dans l optimisation des capteurs solaires plans à air. Phd thesis, université de Valenciennes et du Hainaut cambresis, France, 1994.