Journal Article10.2514/2.1964
Comparison of Heat Transfer Augmentation Techniques
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TL;DR: Ligrani et al. as mentioned in this paper investigated the effects of surface roughness on turbulent boundary layers, transitional phenomena in curved channels, and innovative schemes for internal cooling and surface heat transfer augmentation, such as dimpled surfaces and swirl chambers, as well as a variety of gas turbine heat transfer and blade cooling problems.
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Abstract: Dr. Phil Ligrani is currently Professor of Mechanical Engineering and Director of the Convective Heat Transfer Laboratory at the University of Utah and a Fellow of the American Society of Mechanical Engineers. He has beenworking on convection heat transfer and fluid mechanics research problems since he received his Ph.D. degree from the Department of Mechanical Engineering at Stanford University in 1980. From 1979 to 1982, he was an Assistant Professor in the Turbomachinery Department of the von Karman Institute for Fluid Dynamics, Rhode-Saint-Genese, Belgium. From 1982 to 1984, he worked in the Department of Aeronautics of the Imperial College of Science and Technology, University of London. From 1984 to 1992, he was an Associate Professor in the Department of Mechanical Engineering of the U.S. Naval Postgraduate School. In his research, he has investigated the ultra-small-scale motions that exist near walls in turbulent boundary layers, the effects of surface roughness on turbulent boundary layers, transitional phenomena in curved channels including the development and structure of Dean vortex pairs, and innovative schemes for internal cooling and surface heat transfer augmentation, such as dimpled surfaces and swirl chambers, as well as a variety of gas turbine heat transfer and blade cooling problems. He served as Guest Editor for the journal Measurement Science and Technology from 1998 to 2000, and he will serve as Associate Technical Editor for the Journal of Heat Transfer from 2003 to 2006. He has published approximately 150 journal papers, conference papers, and book chapters. In 1995, he was presented with the "Professor of the Year" award at the University of Utah for outstanding classroom teaching. Some of his other activities and recognitions include a Guest Professorship in 2000 at the Institut fur Thermische Stroemungs-maschinen-Universitaet Karlsruhe, a Visiting Senior Research Fellowship from 1982 to 1983 at the Imperial College of Science and Technology-University of London, a NASA Space Act Tech Brief Award in 1991 for "Development of Subminiature Multi-Sensor Hot-Wire Probes," and the Carl E. and Jessie W. Menneken Faculty Award in 1990 for Excellence in Scientific Research. E-mail: ligrani@mech.utah.edu.
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Citations
Nature-inspired Inverted Fish Scale microscale passages for enhanced heat transfer
Aik Ling Goh,Kim Tiow Ooi +1 more
TL;DR: In this paper, an annular microchannel, with gap size of 300μm, is formed by securing a cylindrical insert of mean diameter 19.4mm within an internal pipe of internal diameter 20mm.
Convective Heat Transfer Enhancement: Mechanisms, Techniques, and Performance Evaluation
Ya-Ling He,Wen-Quan Tao +1 more
TL;DR: The field synergy principle (FSP) as mentioned in this paper was proposed to improve the performance of convective heat transfer by revealing the locations with a bad synergy angle and changing the local structure of the surface.
Experimental investigation of the influence of large-scale vortex structures on heat transfer and drag on a smooth wall
N. A. Kiselev,A G Zditovets,Yu. A. Vinogradov,M. M. Strongin +3 more
- 10 Nov 2017
Abstract: The results of an experimental investigation on the effect of large-scale vortex structures on the heat transfer and drag coefficients on smooth wall are presented. Cylinder of diameter Ø=8 mm was installed in a channel of height H=30 mm. The models were installed at distance of 40 mm from cylinder. The gap Y0 between the wall and the edge of the cylinder varied from 1 to 21 mm. The value of the averaged relative drag coefficient cx/cx0 as well as the relative heat transfer coefficient St/St0 were determined behind the cylinder at different flow velocity and position of cylinder in the channel. The maximum value of cx/cx0=1.48-2.04 (depending on the Reynolds number Rex) is obtained for the case of Y0=11 mm. At Y0=21 mm the shear stress on the wall decreases to cx/cx0=0.00-0.17. At Y0=1-2 mm, negative values of the cx/cx0 are observed. The minimum value cx/cx0=-1.01–-0.71 corresponds to smallest gap Y0=1 mm. The local value St/St0 for Y0=1-2 mm has maximum at distance of 80 mm from cylinder’s axis. With further increase in Y0 to 9 mm, the value of St/St0 decreases along the plate. At Y0=11 mm local maximum is observed at distance of 90 mm from cylinder’s axis. At Y0=21 mm, the values of St/St0=1. The local values of St/St0 varied in range St/St0=1.0 2.5.
Flow and Heat Transfer Characteristics in Latticework Cooling Channels With Dimple Vortex Generators
Yu Rao,Shusheng Zang +1 more
TL;DR: In this article, a comparative numerical study has been conducted on the flow and heat transfer characteristics in the latticework cooling structure with three different subchannel configurations: rectangular sub-channels, U shaped sub-channel, and U-shaped subchannels with dimple vortex generators.
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