Heat Transfer Effectiveness and Coefficient of Pressure Drop on the Shell Side of a Staggered Elliptical Tubes Bank

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The effectiveness of heat transfer and the pressure drop coefficient of staggered elliptical tube banks are studied experimentally. The bank consists of 11 elliptical tubes of 0.75 equivalent diameter in an arrangement of 4-3-4. The major and the minor sub-axis of each tube are 24.70 mm and 12.35 mm respectively, and therefore the aspect ratio (AR) of the tube is 2.0. The geometric parameters of the bank are ST = 24.70 mm, SL = 37.00 mm and minimum frontal area B = 12.35 mm. Seven mid-tubes are internally heated by electrical heater of 69.6 Watt each. Experiment is conducted in a sub sonic wind tunnel and run with the wind velocities of 1 m/s 12.6 m/s which correspond with Reynolds number of = 346-6904. The results show that the effectiveness (ε) varied from 2144.44 to 15.26. It decreases exponentially at low Reynolds numbers and tended asymptotically at higher Reynolds number. The coefficient of pressure drop (CΔp) ranges from 7.21 to 4.41 decreases continuously at low Reynolds number and asymptotic at higher one.

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134-139

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January 2014

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© 2014 Trans Tech Publications Ltd. All Rights Reserved

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[1] Terukazu Ota, Shinya Aiba, Tsuneiko Tsuruta, and Masaaki Kaga, 1983, Forced Convection Heat Transfer from an Elliptical Cylinder of Axis Ratio 1: 2, Bulletin of the JSME , Vol. 26, No. 212, 262 - 267.

DOI: 10.1299/jsme1958.26.262

Google Scholar

[2] Terukazu Ota, Hideya Nishiyama., and Yukiyasu Taoka., 1984, Heat Transfer and Flow around an elliptic Cylinder, International Journal Heat and Mass Transfer, Vol. 27, No. 10, 1771-1779.

DOI: 10.1016/0017-9310(84)90159-5

Google Scholar

[3] W.A. Khan, J.R. Culham, and M.M. Yovanovich, 2005, Convection Heat Transfer From Tube banks in Crossflow: Analytical Approach, AIAA 2005-0958, 43rd Aerospace Sciences Meeting and Exhibit, American Institute of Aeronautics and Astronautics, Jan 10-13, (2005).

DOI: 10.2514/6.2005-958

Google Scholar

[4] W.A. Khan, J.R. Culham, and M.M. Yovanovich, 2005, Fluid Flow Around and Heat Transfer from Elliptical Cylinders: Analytical Approach, Journal of Thermophysics and Heat Transfer, Vol. 19, No. 2, 178-185.

DOI: 10.2514/1.10456

Google Scholar

[5] W.A. Khan, J.R. Culham, and M.M. Yovanovich, 2006, Analytical Model for Convection Heat Transfer from Tube Banks, Journal of Thermophysics and Heat Transfer, Vol. 20, No. 4, 720-727.

DOI: 10.2514/1.15453

Google Scholar

[6] K. Kritikos, C. Albanakis., D. Missirlis., Z. Vlahostergios., A. Goulas., and P. Storm., 2010, Investigation of the thermal efficiency of staggered elliptic tube heat exchanger for aeroengine applications, Applied Thermal Engineering, Vol 30, 134-142.

DOI: 10.1016/j.applthermaleng.2009.07.013

Google Scholar

[7] G.P. Merker, and H. Hanke., 1986, Heat Transfer and Pressure Drop on the shell-side of tube-banks having oval-shaped tubes, International Journal Heat Mass Transfer, Vol. 29, No. 12, 1903-(1909).

DOI: 10.1016/0017-9310(86)90008-6

Google Scholar

[8] Zakir Faruquee, David S-K. Ting., Amir Fartaj., Ronald M. Barron., and Rupp Carriveau., 2007, The effect of axis ratio on laminar fluid flow around an elliptical cylinder, International Journal of Heat and Fluid Flow, Vol. 28, 1178-1189.

DOI: 10.1016/j.ijheatfluidflow.2006.11.004

Google Scholar

[9] Li, Zhihua., Jane Davidson, and Susan Mantell., 2005, Numerical Simulation of Flow Field and Heat Transfer of Streamlined Cylinders in Crossflow, Proceeding of HT2005, ASME Summer Heat Transfer Conference.

DOI: 10.1115/ht2005-72024

Google Scholar