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Computational Investigation of Fluid Flow 90o Bend Pipe using Finite Volume Approach
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Computational Investigation of Fluid Flow 90o Bend Pipe using Finite Volume Approach
1.
International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395 -0056 Volume: 04 Issue: 06 | June -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 1828 Computational Investigation of Fluid Flow 90o Bend Pipe Using Finite Volume Approach Manish Kumar Rathore 1, Dilbag Singh Mondloe2, Satish Upadhyay3 1M.Tech Scholar, Government Engineering College, Jagdalpur, Chhattisgarh, India 2Assistant professor, Dept. of Mechanical Engineering, GEC Jagdalpur, Chhattisgarh, India 3Lecturer, Dept. of Mechanical Engineering, GEC Jagdalpur, Chhattisgarh, India ---------------------------------------------------------------------***--------------------------------------------------------------------- Abstract - Bend pipe are widely been used in various engineering applications and have significant importance in fluid flow applications. In this paper concentrates on computational analysis of 90o bend pipe using finite volume approach. A two dimensional model of 90o bend has been developed by using ANSYS 14.5 and the hydrodynamic performancecharacteristics hasbeenexaminedandcompared with the same length of straight pipe using Finite volume tool i,e. ANSYS Fluent. The flow separation and boundary layer separation has also been examined for wide range ofReynolds number. At the bend section the friction factor has examined and found that the inner and outer surface has un- symmetrical pattern and at turbulent intensity also varies in comparison with straight pipe. The obtained finite volume results have been compared with the published data and the result shows good agreement. Key Words: 90o bend pipe, CFD, Reynolds number, Turbulence, pressure, velocity, skin friction . 1.INTRODUCTION In the field of heat transfer and fluid flow implementation of bend pipe or curved surface are the effectively techniquesof enhancing heat transfer in various engineering applications with have internal flow applicability. Due to presence of obstacle in the flow region leadstobreak boundary layer and creates turbulence this phenomenon is of substantial important phenomena asitmaystronglyaffect pressure drop, wall friction, heat transfer, occurrence of extreme temperatures, and stability of the flow. when fluid flows in a pipe bend a secondary motion of flowisdeveloped due to the presence of centrifugal force which leads to the formation of secondary flow and as a result the fluid particles near the surface are driven outward. This secondary flow is superimposed on its primary axial flow leading to high velocity at the outer core of the pipe bend. As result of these secondary flow within the pipe the rate turbulence intensity increases, which also increase the friction factor and also affect the other hydrodynamic characteristics. Row 1970 experimentally examined the heat transfer effect in large wavy pipe due to secondary flow which leads to complete interchange of fluid in the wall andthecentral core line. Their work particularly focuses on single phase flow in various pipe bends like 180 U-bend, 45o/45o S-bend attached to the end of a long straight pipe. Janyanti et al 1993 performed CFD analysis to examine the Gas-particle motion in 90o and 1800 circular cross-section pipe bends. They found that the secondary flow induced in the gas phas-e due to curvature affects the motion of the particles which causes the smaller particles to come out of the bend without deposition. Clarke and Finn 2008 numerically investigates the Laminar flow of secondary working fluid such as potassium formate through heat exchanger U-bends and found that heat transfer increases at downstream of the bend. Dhanasekaran 2012 perform CFD analysis of closed-loop steam cooling in a 180-degree bend tube sof advanced gas turbine. Their aims is to validating a CFD model against experimental results ina 180-degreetubebendandapplying the model to predict the mist/steam cooling performance at gas turbine working conditions. The obtained results show that the CFD model can predict the wall temperature within 8% of experimental steam-only flow and16%ofmist/steam flow condition Georgios A. Florides 2013 developed a numerical model for simulating Single and double U-tube ground heat exchangers. The impact of multi-layer substrates on temperature distribution of ground heat exchanger. The model is also modified to allow the study of a double U-tube GHE in a single borehole and the assessment of its efficiency with regard to its building cost. Pedro M. de Oliveira. 2014. Gas–liquid flowsincurvedtubes are found in a number of applications, such as heat exchangers and transport pipes. The present work deals with air–water flow in 180tube bends (curvaturesof6.1, 8.7, and 12.2) that connect two 5-m long 26-mm ID horizontal tubes. The bend lies in the vertical position and the two- phase flow can be set as upward or downward. The straight and curved segments of test section were made from borosilicate glass to enable visual access to the two-phase flow. Chen et al. 2015 experimentally analyzed the effect oflength and bending angle on the cooling performance of flat plate heat pipes (FPHP) it has been observed that optimum liquid filling ratio increases as length of pipe increases. While, shorter pipe had a larger effective thermal conductivity,and
2.
International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395 -0056 Volume: 04 Issue: 06 | June -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 1829 implying more efficiently. The bending of pipe would not affect the optimum liquid filling ratio of a FPHP. Hasanpour et al. 2016 experimentally studied heat transfer and friction factor in a double pipeheat exchangerwhichhas an inner corrugated tube filled with various categories of twisted tapes from conventional tomodified types which include perforated, V-cut and U-cut types. Bhusan et al. 2017 numerically examine the flow and heat transfer characteristics in 180 bend pipe with havingflowof water-fly ash slurry. In their work they considered RNG k-ε turbulence model. The pressure drop and heat transfer has been examined for multiphase flow using finite volume approach. Different exact and approximate techniques have also been used to solve the different problems in fluid mechanics [19-26].Other significant works with the implementation of keε turbulence model were studied by Cardwell et al. 2011 and Walker 2005. Different approach was proposed by Johansen et al. 2003, Pinson and Wang 1999, Zimparov 2004 and Zhu and Kuznetsov 2005 to study the influence of the rough wall by using the modified mixed length model.Apart from these many research has carried out the research in the field of Magneto hydrodynamic flow (MHD) to explore the effect of magnetic field on the boundary layer flow control [27-32]. 1.1 Mathematical Modeling For the fluid flow through pipe, duct and channel the conventional governing equations are the Navier–Stokes equations can be written in the most useful form for the development of the finite volume method: ( ) Mx Du p div gradu S Dt x (1) ( ) My Dv p div gradv S Dt y (2) ( ) Mz Dw p div gradw S Dt z (3) Governing equations of the flow of a compressible Newtonian fluid Continuity ( ) 0div u x x-momentum ( ) ( ) ( ) Mx u p div uu div gradu S x x (4) y-momentum ( ) ( ) ( ) My v p div vu div gradv S y y (5) z-momentum ( ) ( ) ( ) Mz w p div wu div gradw S z z (6) Energy ( ) ( ) ( ) i i div iu pdivu div kgradT S t (7) Using various correlation FEV results are been compared analytically 2 2 f h LV h f D g Where, f is the friction factor for fully developed laminar flow L: length of the channel, duct, pipe V: mean velocity of the flow d: diameter of the pipe f is the friction factor for fully developed laminar flow: 64 Re f (For Re<2000) Re avgu d Cf is the skin friction coefficient or Fanning’s friction factor. For Hagen-Poiseuille flow: 21 16 2 Re f wall avgC l u For turbulent flow: 10 1 18.7 1.74 2.0log Re p Rf f Moody’s Chart R: radius of the channel, duct, pipe εp: degree of roughness (for smooth channel, duct, pipe, εp=0) Re : Completely rough channel, duct, pipe. 1.2 Methodology The ANSYS 14.5 finite element program was used for analyzing flow in 90o bend Pipe and straight Pipe. For this purpose, the key points were first created and then line and spline segments were formed. The lines were combined to create an area. Finally, this area was extruded a Wemodeled the 90o bend Pipe and straight Pipe. Fig -1: Model Geometry
3.
International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395 -0056 Volume: 04 Issue: 06 | June -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 1830 Fig -2: Mesh Model The modeled 90o bend pipeandstraightpipe wasdiscretized into multiple of 105 i.e. 22950 elements with 23332 nodes and the mesh is fine and structured which can be seen from figure 2. The developed geometry for the simulation (FEV analysis) is been taken form Dutta et al. [15] which is taken as base paper for the proposed work. 2. RESULTS AND DISCUSSIONS The governing equations of the problem were solved, numerically, using a Element method, and finite Volume method (FVM) used in order to calculate the Hydrodynamic characteristics of a 90o bend Pipe and straight Pipe. As a result of a grid independence study, a grid size of 106 was found to model accurately the Hydrodynamic performance characteristics are described in the corresponding results. The accuracy of the computational model was verified by comparing results from the present study with those obtained by Dutta et al. [15], sudo et al. [13] , Kim et al. [14] and Tanaka et al. [12] whose works are based on experimental, and FVM results. On considering base paper as Dutta et al.[35] the measurements of velocities were performed at a Reynolds number of 6 × 104 for the validation and the result are as plotted in fig 3.Figure 6 illustrates the pressure drop across Bend pipe at high Reynolds number. It has been observed that the pressure across the Bend pipe continuously goes on decreasing from inlet to outlet. It is interesting to know that across the pipe bending region the variation in pressure has been seen in term of increase and decrease. Fig -3: Validation of Velocity magnitude of 90o bend Pipe Fig -4: Contour Plot of turbulent intensity Bend pipe
4.
International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395 -0056 Volume: 04 Issue: 06 | June -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 1831 Fig -5: Contour Plot of turbulent intensity Straight Pipe Fig -6: Static pressure distributions across Bend pipe Figure 7 shows the pressure drop across straight pipe at high Reynolds number. It has been observed that the pressure significantly decreases throughout the pipelength. It is interesting to know that in straight channel this drop in pressure is linear throughout the pipe length, which can be evident from figure 7 while in Bend pipe the drop in pressure is linear but have different slope in different direction. Figure 8 and 10 shows the skin friction coefficient across Bend pipe and straight pipe. It has been seen that in 90o bend pipe, at the inner radius region i.e. (elbow_win) experiences higher rate of friction has compared to outer radius region i.e. (elbow_wout) this is due to higher wall shear stress across inner radius region. While in Straight pipe the nature of skin frictioncoefficientremainsamein top and bottom wall and experiences equal rate of skin friction coefficient. Fig -7: Static pressure distribution across Straight Pipe The un symmetrical nature of skin friction coefficient at the wall of bend pipe is due to having different turbulence intensity at the inner radius region i.e. (elbow_win) and outer radius region i.e. (elbow_wout).This can be seen from figure 9. While in straight pipe the nature of skin friction coefficient at the wall i.e. top and bottom wall is same. This can be seen from figure 10 Fig -8: skin friction coefficient across Bend pipe Figure 11 shows the influence of Reynolds number on Skin Friction coefficient. It has seen that as Reynolds number increases skin friction increases. This is because of occurrence of turbulence in flow which results in increase in friction. The contour plot of turbulence intensitycanbeseen from figure 4 and 5
5.
International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395 -0056 Volume: 04 Issue: 06 | June -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 1832 Fig -9: skin friction coefficient across the bend section Fig -10: skin friction coefficient across Straight Pipe Fig -11: Influence of Reynolds number on Skin friction coefficient Furthermore the trend of discrepancy is same for both the pipes i.e. 90o bend pipe and straight pipe. But the 90o bend pipe has higher rate of friction. It has also been seen that on comparing the skin friction coefficient straight pipe has 98.65% less friction has compared to bend pipe at high Reynolds number. 2.2 CONCLUSION On the basis of developed computational model of 90o bend pipe and straight pipe following conclusionshasbeendrawn which as follows: The developed computational model of 90o bend pipe has been compared with the result of experimental and computation work of available literature and the result shows similar trend. Increase in Reynoldsnumber,theskinfrictionfactor increases simultaneously. The turbulence intensity within the90o bendpipeis more has compared to straight pipe. The pressure drop in straight pipe is continuously linear, while in 90o bend pipe at the bend section sudden increase and decrease has been seen. Implementing bend in pipe results in increase in rate of turbulence. Therefore, in heat exchanger where high turbulence is required bend pipe are widely been used. The nature of skin friction coefficient across the inner radius region and outer radius region is un symmetrical. While in straight pipe the nature of skin friction coefficient is symmetrical at top and bottom wall. The straight pipe has 98.65% less friction has compared to bend pipe at high Reynolds number. REFERENCES [1] Rowe M. Measurements and computationsofflowinpipe bends. J Fluid Mech 1970;43:771-783. [2] Jayanti S, Wang MJ, Mayinger F.Gas-particleflowthrough bends. IMechE C461 1993;24:161-166. [3] Clarke R, Finn DP. Numerical investigation of the influence of heat exchanger U-bends on temperature profile and heat transfer of secondary working fluids. In: 5th European thermal-Sci. Conf., The Netherlands; 2008. p. 1-8. [4] T.S. Dhanasekaran, Ting Wang, Numerical model validation and prediction of mist/steam coolingina 180- degree bend tube: International Journal ofHeatandMass Transfer 55 (2012) 3818–3828 [5] Georgios A. Florides , Paul Christodoulides, Panayiotis Pouloupatis, Single and double U-tube ground heat exchangers in multiple-layer substrates; Applied Energy 102 (2013) 364–373 [6] Pedro M. de Oliveira, Jader R. Barbosa Jr. Pressure drop and gas holdup in air–water flow in 180_ return bends:
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of Engineering and Technology (IRJET) e-ISSN: 2395 -0056 Volume: 04 Issue: 06 | June -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 1833 International Journal of Multiphase Flow 61 (2014) 83– 93 [7] Jung-Shun Chen, Jung-Hua Chou, The length and bending angle effects on the cooling performanceofflatplateheat pipes, International Journal of Heat and Mass Transfer, Volume 90, November 2015, Pages 848-856 [8] A. Hasanpour, M. Farhadi , K. 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