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contributor authorR. P. Taylor
contributor authorH. H. Hosni
contributor authorH. W. Coleman
contributor authorJ. K. Taylor
date accessioned2017-05-08T23:39:49Z
date available2017-05-08T23:39:49Z
date copyrightOctober, 1992
date issued1992
identifier issn0889-504X
identifier otherJOTUEI-28625#788_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/111042
description abstractMeasurements of Stanton numbers, velocity profiles, temperature profiles, and turbulence intensity profiles are reported for turbulent flat plate boundary layer flows with a step change in surface roughness. The first 0.9 m length of the test surface is roughened with 1.27-mm-dia hemispheres spaced 2 base diameters apart in a staggered array. The remaining 1.5 m length is smooth. The experiments show that the step change from a rough to a smooth surface has a dramatic effect on the convective heat transfer. In many cases, the Stanton number drops below the smooth-wall correlation immediately downstream of the change in roughness. The Stanton number measurements are compared with predictions using the discrete element method with excellent results.
publisherThe American Society of Mechanical Engineers (ASME)
titleHeat Transfer in the Turbulent Boundary Layer With a Step Change in Surface Roughness
typeJournal Paper
journal volume114
journal issue4
journal titleJournal of Turbomachinery
identifier doi10.1115/1.2928032
journal fristpage788
journal lastpage794
identifier eissn1528-8900
keywordsSurface roughness
keywordsBoundary layer turbulence
keywordsHeat transfer
keywordsMeasurement
keywordsTurbulence
keywordsFlow (Dynamics)
keywordsDiscrete element methods
keywordsFlat plates
keywordsTemperature profiles
keywordsDrops
keywordsBoundary layers AND Convection
treeJournal of Turbomachinery:;1992:;volume( 114 ):;issue: 004
contenttypeFulltext


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