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contributor authorK. Rued
contributor authorS. Wittig
date accessioned2017-05-08T23:20:14Z
date available2017-05-08T23:20:14Z
date copyrightJanuary, 1985
date issued1985
identifier issn1528-8919
identifier otherJETPEZ-26614#54_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/99869
description abstractHeat transfer and boundary layer measurements were derived from flows over a cooled flat plate with various free-stream turbulence intensities (Tu = 1.6–11 percent), favorable pressure gradients (k = νe /ue 2 •due /dx = 0÷6•10−6 ) and cooling intensities (Tw /Te = 1.0–0.53). Special interest is directed towards the effects of the dominant parameters, including the influence on laminar to turbulent boundary layer transition. It is shown, that free-stream turbulence and pressure gradients are of primary importance. The increase of heat transfer due to wall cooling can be explained primarily by property variations as transition, and the influence of free-stream parameters are not affected.
publisherThe American Society of Mechanical Engineers (ASME)
titleFree-Stream Turbulence and Pressure Gradient Effects on Heat Transfer and Boundary Layer Development on Highly Cooled Surfaces
typeJournal Paper
journal volume107
journal issue1
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.3239697
journal fristpage54
journal lastpage59
identifier eissn0742-4795
keywordsTurbulence
keywordsBoundary layers
keywordsHeat transfer
keywordsPressure gradient
keywordsCooling
keywordsMeasurement
keywordsFlow (Dynamics)
keywordsBoundary layer turbulence AND Flat plates
treeJournal of Engineering for Gas Turbines and Power:;1985:;volume( 107 ):;issue: 001
contenttypeFulltext


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