Please use this identifier to cite or link to this item: http://buratest.brunel.ac.uk/handle/2438/8945
Title: Heat transfer from the stagnation area of a heated cylinder at Re(D) = 140,000 affected by free-stream turbulence
Authors: Wissink, JG
Rodi, W
Keywords: Heat transfer;Free-stream turbulence;Stagnation region flow
Issue Date: 2011
Publisher: Elsevier
Citation: International Journal of Heat and Mass Transfer, 54(11-12), 2535 - 2541, 2011
Abstract: The effect of free-stream grid-turbulence on the flow around and heat transfer from the stagnation region of a circular cylinder was studied using direct numerical simulations (DNS). Simulations with and without free-stream fluctuations were carried out at a Reynolds number of Re(D) = 140,000 (based on the inflow velocity and the cylinder diameter D), which is in the higher subcritical range. A splitter plate was introduced behind the cylinder to counteract the formation of a vortex street. To resolve the flow up to 746.5 million grid points were employed. Compared to the fully laminar simulation, the addition of Tu = 30% grid turbulence at the inflow plane was found to lead to an increase in heat transfer at the stagnation line of the cylinder of 66%. A very good agreement was obtained with the correlations of Dullenkopf and Mayle [K. Dullenkopf, R. Mayle, The effects of incident turbulence and moving wakes on laminar heat transfer in gas turbines, ASME J. Turbomach. 116 (1994) 23–28; K. Dullenkopf, R. Mayle, An account of free-stream-turbulence length scale on laminar heat transfer, ASME J. Turbomach. 117 (1995) 401–406].
Description: This is the post-print version of the final paper published in International Journal of Heat and Mass Transfer. The published article is available from the link below. Changes resulting from the publishing process, such as peer review, editing, corrections, structural formatting, and other quality control mechanisms may not be reflected in this document. Changes may have been made to this work since it was submitted for publication. Copyright @ 2011 Elsevier B.V.
URI: http://www.sciencedirect.com/science/article/pii/S0017931011000639
http://bura.brunel.ac.uk/handle/2438/8945
DOI: http://dx.doi.org/10.1016/j.ijheatmasstransfer.2011.02.008
ISSN: 0017-9310
Appears in Collections:Mechanical and Aerospace Engineering
Dept of Mechanical Aerospace and Civil Engineering Research Papers

Files in This Item:
File Description SizeFormat 
Fulltext.pdf2.5 MBAdobe PDFView/Open


Items in BURA are protected by copyright, with all rights reserved, unless otherwise indicated.