Heat transfer in production and decay regions of grid-generated turbulence

•Heat transfer experiments are made in grid-turbulence production and decay regions.•Vortex shedding from the grid reduces the heat transfer on the cylinder’s front.•The heat transfer recovery on the cylinder’s back is higher in the production region.•FSG17 sheds less than SSG, and both grids enhanc...

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Veröffentlicht in:International journal of heat and mass transfer 2017-06, Vol.109, p.537-554
Hauptverfasser: Melina, G., Bruce, P.J.K., Hewitt, G.F., Vassilicos, J.C.
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Sprache:eng
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Zusammenfassung:•Heat transfer experiments are made in grid-turbulence production and decay regions.•Vortex shedding from the grid reduces the heat transfer on the cylinder’s front.•The heat transfer recovery on the cylinder’s back is higher in the production region.•FSG17 sheds less than SSG, and both grids enhance the heat transfer more than RG60.•The parameters x∗ and t0/L0 set the heat transfer enhancement on the cylinder. Heat transfer measurements around the centreline circumference of a cylinder in crossflow are performed in a wind tunnel. The cylinder is placed at several stations downstream of three turbulence-generating grids with different geometries and different blockage ratios σg: a regular grid (RG60) with σg=32%, a fractal-square grid (FSG17) with σg=25% and a single-square grid (SSG) with σg=20%. Measurements are performed at 20 stations for 3 nominal Reynolds numbers (based on the diameter D of the cylinder) Re∞=11,100,24,500,37,900. Hot-wire measurements are performed along the centreline, without the cylinder in place, to characterise the flow downstream of the grids. The extent of the turbulence production region, where the turbulence intensity Tu increases with the streamwise distance x from the grid, is higher for SSG and more so for FSG17 than for RG60. The angular profiles of the Nusselt number Nu are measured in the production regions of these two grids and are compared to those obtained in the decay regions, where Tu decreases with x. This comparison is made at locations with approximately same Tu. It is found that, for SSG, Nu/Re0.5 on the front of the cylinder (boundary layer region) is lower in the production region than in the decay region. This is explained by the presence of clear and intense vortex shedding in the production region of SSG which reduces the turbulent fluctuations which are “effective” in enhancing the heat transfer across a laminar boundary layer. For higher Re∞, the values of Nu/Re0.5 on the front of the cylinder are higher in the production region of FSG17 than in that of SSG, despite Tu being higher for SSG. This is consistent with a lower intermittency of the flow for FSG17 caused by the presence of the fractal geometrical iterations. The recovery of Nu on the back of the cylinder (wake region) is appreciably higher in the production region than in the decay region for both FSG17 and for SSG. This can be due to the lower integral length scale ratio Lu/D in the production region and suggests, for the same Re∞, a reducti
ISSN:0017-9310
1879-2189
DOI:10.1016/j.ijheatmasstransfer.2017.02.024