Investigation of Flow Uniformity and Pressure Recovery in a Turning Diffuser by Means of Baffles

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Turning diffuser is an engineering device that is widely used in the industry to reduce the flow velocity as well as change the direction of the flow. Having a curvature shape causes its performance to decrease in terms of pressure recovery (Cp) and flow uniformity (σu). Therefore, this study presents the work done in designing baffles to be installed in the turning diffuser with ratio of AR=2.16 to improve the flow uniformity and pressure recovery. It also aims to investigate the mechanism of flow structure and pressure recovery in turning diffusers by means of turning baffles. The results with varying inflow Reynolds number (Rein) between 5.786E+04 1.775E+05 have been experimentally tested and compared with previous study. Particle image velocimetry (PIV) was used to determine the flow uniformity. On the other hand, a digital manometer provided the average static pressure of the inlet and outlet of turning diffuser. The best produced pressure recovery of Cp=0.526 were recorded when the system were operated at the highest Reynolds number tested Rein=1.775E+05. This result shows an improvement up to 54.625% deviation from previous study with Cp=0.239. The flow uniformity also shows an improvement of 47.127% deviation from previous study at the same Rein with σu=3.235 as compared to previous study σu=6.12.

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526-530

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December 2013

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© 2014 Trans Tech Publications Ltd. All Rights Reserved

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[1] El-Askary, W.A., and Nasr, M., 2009, Performance of a Bend Diffuser System: Experimental and Numerical Studies, Journal of Computer & Fluids, 38, pp.160-170.

DOI: 10.1016/j.compfluid.2008.01.003

Google Scholar

[2] Modi, P.P., and Jayanti, S., 2004, Pressure Losses and Flow Maldistribution in Ducts with Sharp Bends, Chem. Eng. Res. Des., 82, pp.321-331.

DOI: 10.1205/026387604322870435

Google Scholar

[3] Fox, R., and Kline, S., 1962, Flow Regime Data and Design Methods for Curved Subsonic Diffusers, ASME J. Basic Eng., 84, pp.303-312.

DOI: 10.1115/1.3657308

Google Scholar

[4] Lindgren, B., and Johansson, A. V., 2002, Design and Evaluation of a Low-Speed Wind-Tunnel with Expanding Corners, Technical Report No. TRITA-MEK, 2002: 14, Dept. of Mechanics, KTH, SE-100 44 Stockholm, Sweden.

Google Scholar

[5] Farsimadan, E., Mokhtarzadeh-Dehghan, M.R., 2010, An Experimental Study of the Turbulence Quantities in the Boundary Layer and Near-Wake of an Airfoil Placed at Upstream of a 90° bend, Journal of Exp. Thermal and Fluid Science, 34, pp.979-991.

DOI: 10.1016/j.expthermflusci.2010.02.005

Google Scholar

[6] Nakano, T., Fujisawa, N., Oguma, Y., Takagi, Y., and Lee, S., 2007, Experimental Study on Flow and Noise Characteristics of NACA0018 Airfoil, Journal of Wind Engineering, 95, pp.511-531.

DOI: 10.1016/j.jweia.2006.11.002

Google Scholar

[7] Chong, T. P., Joseph, P. F., and Davies P.O.A.L., 2008, A parametric Study of Passive Flow Control for a Short, High Area Ratio 90 Degree Curved Diffuser, ASME J. Fluids Eng., 130(11), pp.212-220.

DOI: 10.1115/1.2969447

Google Scholar

[8] Majumdar, B., Mohan, R., Singh, S. N., and Agrawal, D. P., 1998, Experimental Study of Flow in a High Aspect Ratio 90 Degree Curved Diffuser, ASME J. Fluids Eng., 120(1), pp.83-89.

DOI: 10.1115/1.2819668

Google Scholar

[9] Nordin, N., Raghavan, V. R, Othamn, S., and Karim, Z.A.A., 2012, Compatibility of 3-D Turning Diffusers by Means of Varying Area Ratios and Outlet-Inlet Configurations, ARPN Journal of Engineering and Applied Sciences, 7, ISSN 1819-6608.

Google Scholar

[10] Nordin N., Raghavan, V.R., Othman, S., and Karim, Z.A.A., 2012 Numerical Investigation of Turning Diffuser Performance by Varying Geometric and Operating Parameters, Journal of Applied Mechanics and Materials, 229, p.2086-(2093).

DOI: 10.4028/www.scientific.net/amm.229-231.2086

Google Scholar

[11] Nordin N., Raghavan, V.R., Othman, S., and Karim, Z.A.A., 2012, Experimental Investigation of Turning Diffuser Performance by Varying Inflow Reynolds Number, Post Graduate Symposium, Universiti Teknologi Petronas, Perak, Malaysia.

DOI: 10.53369/dtoc3606

Google Scholar

[12] Nordin N., Raghavan, V.R., Othman, S., and Karim, Z.A.A., 2012, Design and Development of Low Subsonic Wind Tunnel for Turning Diffuser Application, Journal of Advance Materials Research, 614, pp.586-591.

DOI: 10.4028/www.scientific.net/amr.614-615.586

Google Scholar

[13] Kim. J., Moin P., and Moser R., 1987 Turbulence statistics in fully developed channel flow at low Reynolds number, J. Fluid Mech., 177, pp.133-136.

DOI: 10.1017/s0022112087000892

Google Scholar