Research Article  Open Access
Siddharth D. Mhaske, Soby P. Sunny, Sachin L. Borse, Yash B. Parikh, "Thermohydraulic Performance of a Series of InLine Noncircular Ducts in a Parallel Plate Channel", Journal of Thermodynamics, vol. 2014, Article ID 670129, 10 pages, 2014. https://doi.org/10.1155/2014/670129
Thermohydraulic Performance of a Series of InLine Noncircular Ducts in a Parallel Plate Channel
Abstract
Heat transfer and fluid flow characteristics for twodimensional laminar flow at low Reynolds number for five inline ducts of various nonconventional crosssections in a parallel plate channel are studied in this paper. The governing equations were solved using finitevolume method. Commercial CFD software, ANSYS Fluent 14.5, was used to solve this problem. A total of three different nonconventional, noncircular crosssection ducts and their characteristics are compared with those of circular crosssection ducts. Shape2 ducts offered minimum flow resistance and maximum heat transfer rate most of the time. Shape3 ducts at Re < 100 and Shape2 ducts at Re > 100 can be considered to give out the optimum results.
1. Introduction
The heat transfer enhancement in most of the engineering applications is a never ending process. The need for better heat transfer rate and low flow resistance has led to extensive research in the field of heat exchangers. Higher heat transfer rate and low pumping power are desirable properties of a heat exchanger. The duct shape and its arrangement highly influence flow characteristics in a heat exchanger. Flow past cylinders, especially circular, flat, oval, and diamond arranged in a parallel plate channel, were extensively studied by Bahaidarah et al. [1–3]. They carried domain discretization in bodyfitted coordinate system while the governing equations were solved using a finitevolume technique. Chhabra [4] studied bluff bodies of different shapes like circle, ellipse, square, semicircle, equilateral triangle, and square submerged in nonNewtonian fluids. Kundu et al. [5, 6] investigated fluid flow and heat transfer coefficient experimentally over a series of inline circular cylinders in parallel plates using two different aspect ratios for intermediate range of Re 220 to 2800. Grannis and Sparrow [7] obtained numerical solutions for the fluid flow in a heat exchanger consisting of an array of diamondshaped pin fins. Implementation of the model was accomplished using the finite element method. Tanda [8] performed experiments on fluid flow and heat transfer for a rectangular channel with arrays of diamond shaped elements. Both inline and staggered fin arrays were considered in his study. Jeng [9] experimentally investigated pressure drop and heat transfer of an inline diamond shaped pinfin array in a rectangular duct. Terukazu et al. [10] studied the heat transfer characteristics and flow behaviours around an elliptic cylinder at high Reynolds number. Gera et al. [11] numerically investigated a twodimensional unsteady flow past a square cylinder for the Reynolds number (Re) considered in the range of 50–250. The features of the flow past the square cylinder were observed using CFD. Olawore and Odesola [12] numerically investigated twodimensional unsteady flow past a rectangular cylinder. The effect of vortical structure and pressure distribution around the section of rectangular cylinders are studied in their work. Chen et al. [13, 14] analysed flow and conjugate heat transfer in a highperformance finned oval tube heat exchanger element and calculated them for a thermally and hydrodynamically developing threedimensional laminar flow. Computations were performed with a finitevolume method based on the SIMPLEC algorithm.
Zdravistch et al. [15] numerically predicted fluid flow and heat transfer around staggered and inline tube banks and found out close agreement experimental test cases. Tahseen et al. [16] conducted numerical study of the twodimensional forced convection heat transfer across three inline flat tubes confined in a parallel plate channel, the flow under incompressible and steadystate conditions. They solved the system in the bodyfitted coordinates (BFC) using the finitevolume method (FVM). Gautier et al. [17] proposed a new set of boundary conditions to improve the representation of the infinite flow domain.
Conventional tube/duct shapes have been investigated for fluid flow and heat transfer characteristics. In this paper, twodimensional, steady state, laminar flow over nonconventional noncircular (Shape1, Shape2, and Shape3) inline ducts confined in a parallel plate channel is considered. The different geometries investigated are Circular, Shape1, Shape2, and Shape3. Only representative cases are discussed in this paper.
2. Mathematical Formulation
The governing mass, momentum, and energy conservation equations [1] for steady incompressible flow of a Newtonian fluid are expressed as
Commercial CFD software, ANSYS Fluent 14.5, was used to solve the governing equations. The pressurevelocity coupling is done by semiimplicit method for pressure linked equations (SIMPLE) scheme.
The grid for all the cases is generated using the Automatic Method with all Quadrilateral elements in the Mesh Component System of the ANSYS Fluent 14.5 software. In the numerical simulation, the grid of 11,000 nodes is found to be fair enough for grid independent solution. Refining the grid proved to be unnecessary, resulting in utilizing more computer resources. Figure 2 shows the grid generated for all the configurations.
3. Geometric Configuration
A total of four different duct crosssections, namely, Circular, Shape1, Shape2, and Shape3 were analysed. The five inline ducts were confined in a parallel plate channel. The distance between two consecutive ducts was kept constant. , , and ratio (shown in Figure 1) kept constant for all crosssections of the ducts. The height of obstruction is kept constant; that is, the diameter () of circular crosssection duct is taken for all the other crosssections (see Figure 1). The unobstructed length of the pipe before the first and the last module is kept as one module length and three module lengths, respectively, so that the flow is fully developed. It is also ensured that the flow is fully developed when it enters the channel. The ducts and the parallel plate channel walls were assumed to be of infinite extent in the direction, that is, perpendicular to the paper. Hence, the flow could be considered as twodimensional. Since, the geometry is symmetric along the axis, only the lower half portion is considered for the computation purpose.
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4. Boundary Conditions
Figure 3 represents the schematic of the boundary conditions for all the crosssections used. A fully developed flow with velocity profile () and with temperature () was assigned for the flow at inlet. The temperature was kept different from that of the plate and duct walls. A no slip () boundary condition was given to the plate and duct surface. The surface temperatures of the plates and the ducts were taken to be constant (). At the symmetry, normal component of velocity and normal gradient of other velocity components were taken as zero. At the outflow boundary, there is no change in velocity across boundary.
5. Validation
The parallel plate channel problem corresponds to the rectangular duct with infinite aspect ratio. The calculated value of Nusselt number is 7.541. Comparing the calculated Nusselt number with that of the theoretical Nusselt number value of 7.54 [18] shows that our computed values are in good agreement with those of the theoretical values.
Using the geometric parameters and for circular crosssection, the normalized pressure drop (), and Nusselt number for third module of the parallel plate channel, when compared with the values of Kundu et al. [5], shows good agreement between both the values.
6. Results and Discussions
The numerical simulation was carried out for Reynolds number ranging from 25 to 350 and Prandtl number was taken as 0.74.
6.1. Onset of Recirculation
For any duct shape, no separation of flow was observed below Re = 30. Circular duct displayed the signs of recirculation at the lowest Re value (Re = 32) [1]. The Shape1 ducts displayed the onset of recirculation at Re value of 48; Shape2 ducts showed the signs of onset of recirculation at Re = 60, while the Shape3 showed the signs of recirculation just under Re = 40.
As the values of Reynolds number are increased, the recirculation region starts increasing. At Re = 150, the length of the recirculation region is slightly smaller than the distance between the two consecutive ducts in the flow direction, while, at Re = 350, the length of the recirculation region is greater than the distance between the two consecutive ducts. Since there is no obstruction to the flow downstream of the last duct, the elliptic behaviour of the flow is observed as shown in Figures 5–8.
6.2. Fluid Flow Characteristics
From Figures 5, 6, 7, and 8, we can observe that the streamlines past the ducts 1–4 are similar in nature. Thus, the streamwise velocity distributions at the module inlets (see Figure 9) and normalized pressure drop Figure 4 and module average Nusselt number for each module (Table 2) confirm the existence of periodically fully developed flow downstream of the second module. As the flow is periodically fully developed for the inner modules, it is sufficient to study one inner module so as to understand the essential of flow physics. In present study, we have selected module 3. Small variations for the first and the last modules are observed due to the end effects.
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Figure 10 shows the normalized (dimensionless) pressure drop () as a function of Reynolds number. We can observe that, as the value of Re increases, there is descend in normalized pressure drop for all the ducts presented in this study.
The ratio of normalized pressure drop for noncircular duct module () to that for the circular duct module () is shown in Figure 11. The Shape1 ducts present pressure drop almost similar to that of the Circular ducts due to their geometric similarity. Shape 2 ducts present lowest pressure drop ratio (), which means that they offer lower resistance to flow than the circular ducts till Re = 300 resulting in lower pumping power requirement. Shape3 ducts present lower values till Re = 150, but, after Re = 150, they increase significantly, resulting in more pumping power.
6.3. Heat Transfer Characteristics
Figure 12 presents the module average Nusselt number as a function of Re for module 3 for Shape1, Shape2, Shape3, and Circular ducts Table 1. The Nusselt number for Re < 50 increases rapidly as the Re increases. Till Re = 50, there is no significant difference in Nusselt number values for different crosssection ducts, which implies that the duct shape has very little effect on heat transfer rate at Re < 50. At higher values of Re the recirculation of the flow takes place. These recirculation vortices do not transfer heat energy to the main stream of flow. Hence, their contribution to heat transfer is very less. At Re < 50, the Nu is almost the same for various crosssection ducts but, after Re = 50, the Nusselt number varies significantly with the crosssection of the duct. Circular crosssection ducts present the least Nu values till Re = 250, while Shape2 crosssection ducts present the highest Nu values after Re = 250.

Figure 13 presents the heat transfer enhancement ratio (Nu^{+}) as a function of Re for module 3 for Shape1, Shape2, and Shape3 ducts. Nu^{+} is the ratio of Nusselt number for noncircular duct module (Nu) to that for the circular duct module (). It represents how effective the heat transfer rate will be using the noncircular ducts as compared to the circular ducts. For Re < 50, all the ducts show similar Nu^{+} values. Shape2 ducts show least Nu^{+} values at Re < 200 but, after Re = 200, they rise up significantly giving highest Nu^{+} values as compared to their counter parts. Shape1 ducts show constant drop in the Nu^{+} values and, at Re > 250, they have heat transfer rate less than the circular ducts.
Figure 14 presents the heat transfer performance ratio () as a function of Re for module 3 for Shape1, Shape2, and Shape3 ducts. represents heat transfer enhancement per unit increase in pumping power. The Shape1 ducts performed poorly as compared to Circular ducts at Re > 250. Shape3 ducts presented good results at Re < 100 but then they presented a constant drop in the values, while Shape2 ducts displayed promising results after Re = 100.
7. Conclusion
In an environment where the heat transfer rate and pumping power is critical, Shape2 ducts show promising results as compared to their counterparts. The duct shape has very little influence on the heat transfer rate at low Reynolds number. For optimal design of a heat exchanger for heat transfer enhancement per unit increase in pumping power, Reynolds number and crosssection of the duct must be carefully chosen. So, for heat exchanger, Shape3 ducts at Re < 100 and Shape2 ducts at Re > 100 can be considered to give out the optimum results.
Nomenclature
Area of heat transfer surfaces in a module (m^{2})  
Specific heat (J/kg K)  
Blockage height of a tube inside the channel (m)  
Module friction factor  
Module friction factor for circular tubes  
Height of the channel (m)  
Module length (m)  
Thermal conductivity (W/m·K)  
Length of the tube crosssection along the flow direction (m)  
Module average Nusselt number  
Module average Nusselt number for the reference case of circular tubes  
Heat transfer enhancement ratio ()  
Heat transfer performance ratio  
Mass flow rate (kg/s)  
Pressure (Pa)  
Reynolds number (VH/)  
Temperature (K)  
Average of module inlet bulk temperature and module outlet bulk temperature (K)  
Temperature of heat transfer surfaces (K)  
Velocity at the channel inlet (m/s)  
Velocity field  
Vertical distance from the channel bottom (m)  
Pressure drop across a module (Pa)  
Normalized pressure drop ()  
Change in bulk temperature across a module (K)  
Dynamic viscosity (N·s/m^{2})  
Density  
Del operator. 
Conflict of Interests
The authors declare that there is no conflict of interests regarding the publication of this paper.
Acknowledgments
The authors would like to present their sincere gratitude towards the Faculty of Mechanical Engineering in Symbiosis Institute of Technology, Pune, and Rajarshi Shahu College of Engineering, Pune.
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Copyright
Copyright © 2014 Siddharth D. Mhaske et al. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.