Numerical Simulation on Heat Transfer Enhancement in Channel by Triangular Ribs
Commenced in January 2007
Frequency: Monthly
Edition: International
Paper Count: 33122
Numerical Simulation on Heat Transfer Enhancement in Channel by Triangular Ribs

Authors: Tuqa Abdulrazzaq, Hussein Togun, M. K. A. Ariffin, S. N. Kazi, NM Adam, S. Masuri

Abstract:

Turbulent heat transfer to fluid flow through channel with triangular ribs of different angles are presented in this paper. Ansys 14 ICEM and Ansys 14 Fluent are used for meshing process and solving Navier stokes equations respectively. In this investigation three angles of triangular ribs with the range of Reynolds number varied from 20000 to 60000 at constant surface temperature are considered. The results show that the Nusselt number increases with the increase of Reynolds number for all cases at constant surface temperature. According to the profile of local Nusselt number on ribs walled of channel, the peak is at the midpoint between the two ribs. The maximum value of average Nusselt number is obtained for triangular ribs of angel 60°and at Reynolds number of 60000 compared to the Nusselt number for the ribs of angel 90° and 45° and at same Reynolds number. The recirculation regions generated by the ribs corresponding to the velocity streamline show the largest recirculation region at triangular ribs of angle 60° which also provides the highest enhancement of heat transfer.

Keywords: Ribs channel, Turbulent flow, Heat transfer enhancement, Recirculation flow.

Digital Object Identifier (DOI): doi.org/10.5281/zenodo.1086505

Procedia APA BibTeX Chicago EndNote Harvard JSON MLA RIS XML ISO 690 PDF Downloads 3212

References:


[1] S.W. Perry AE, Joubert PN Rough wall turbulent boundary layers, Journal of Fluid Mech 37 (1969) 383–413.
[2] M.F.a.S.O. F. Durst, Experimental and Computational Investigation of the Two-Dimensional Channel Flow Over Two Fences in Tandem, Journal of Fluids Engineering 110 (1) (1988) 48-54.
[3] H.J. Liou TM, Turbulent heat transfers augmentation and friction in periodic fully developed channel flows, ASME J Heat Transfer 114 (1992) 56–64.
[4] T.-M. Liou, J.-J. Hwang, Effect of ridge shapes on turbulent heat transfer and friction in a rectangular channel, International Journal of Heat and Mass Transfer, 36(4) (1993) 931-940.
[5] Y.M. Zhang, Gu, W. Z., and Han, J. C, Heat transfer and friction in rectangular channels with ribbed or ribbed-grooved walls, ASME Journal of Heat Transfer, 116 (1994) 58-65.
[6] A. Murata, S. Mochizuki, Comparison between laminar and turbulent heat transfer in a stationary square duct with transverse or angled rib turbulators, International Journal of Heat and Mass Transfer, 44(6) (2001) 1127-1141.
[7] H.C. J. Ahn, J. S. Lee, , Large eddy simulation of flow and heat transfer in a channel roughened by square or semicircle ribs, ASME J. Turbomach., 127 ( 2005) 263-269.
[8] G. Tanda, Heat transfer in rectangular channels with transverse and Vshaped broken ribs, International Journal of Heat and Mass Transfer, 47(2) (2004) 229-243.
[9] V. SriHarsha, S.V. Prabhu, R.P. Vedula, Influence of rib height on the local heat transfer distribution and pressure drop in a square channel with 90° continuous and 60° V-broken ribs, Applied Thermal Engineering, 29(11–12) (2009) 2444-2459.
[10] P. Promvonge, Heat transfer and pressure drop in a channel with multiple 60° V-baffles, International Communications in Heat and Mass Transfer, 37(7) (2010) 835-840.
[11] A. Gupta, V. SriHarsha, S.V. Prabhu, R.P. Vedula, Local heat transfer distribution in a square channel with 90° continuous, 90° saw tooth profiled and 60° broken ribs, Experimental Thermal and Fluid Science, 32(4) (2008) 997-1010.
[12] C. Thianpong, T. Chompookham, S. Skullong, P. Promvonge, Thermal characterization of turbulent flow in a channel with isosceles triangular ribs, International Communications in Heat and Mass Transfer, 36(7) (2009) 712-717.
[13] S. Caliskan, S. Baskaya, Experimental investigation of impinging jet array heat transfer from a surface with V-shaped and convergentdivergent ribs, International Journal of Thermal Sciences, 59(0) (2012) 234-246.