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contributor authorR. B. Rivir
contributor authorJ. P. Johnston
contributor authorJ. K. Eaton
date accessioned2017-05-08T23:45:54Z
date available2017-05-08T23:45:54Z
date copyrightJanuary, 1994
date issued1994
identifier issn0889-504X
identifier otherJOTUEI-28634#57_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/114586
description abstractFluid dynamics and heat transfer measurements were performed for a separation bubble formed on a smooth, flat, constant-heat-flux plate. The separation was induced by an adverse pressure gradient created by deflection of the opposite wall of the wind tunnel. The heat transfer rate was found to decline monotonically approaching the separation point and reach a broad minimum approximately 60 percent below zero-pressure-gradient levels. The heat transfer rate increased rapidly approaching reattachment with a peak occurring slightly downstream of the mean reattachment point. The opposite wall shape was varied to reduce the applied adverse pressure gradient. The heat transfer results were similar as long as the pressure gradient was sufficient to cause full separation of the boundary layer.
publisherThe American Society of Mechanical Engineers (ASME)
titleHeat Transfer on a Flat Surface Under a Region of Turbulent Separation
typeJournal Paper
journal volume116
journal issue1
journal titleJournal of Turbomachinery
identifier doi10.1115/1.2928278
journal fristpage57
journal lastpage62
identifier eissn1528-8900
keywordsHeat transfer
keywordsSeparation (Technology)
keywordsTurbulence
keywordsPressure gradient
keywordsShapes
keywordsWind tunnels
keywordsBubbles
keywordsBoundary layers
keywordsDeflection
keywordsGradients
keywordsMeasurement
keywordsPressure
keywordsFluid dynamics AND Heat
treeJournal of Turbomachinery:;1994:;volume( 116 ):;issue: 001
contenttypeFulltext


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