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contributor authorK. Funazaki
date accessioned2017-05-08T23:51:58Z
date available2017-05-08T23:51:58Z
date copyrightApril, 1996
date issued1996
identifier issn0889-504X
identifier otherJOTUEI-28651#327_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/117869
description abstractMeasurements of wake-affected heat transfer distributions on a flat plate are made by use of a wake generator that consists of a rotating disk and several types of circular cylinder. The main purpose of this study is to construct a wake-induced transition model in terms of an intermittency factor, considering the evolution of the wake-induced turbulent region, a so-called turbulent patch in a distance–time diagram. A comparison between the proposed transition model and the measured heat transfer data reveals that the transition model yields good agreement with the measured data of all test conditions in this study.
publisherThe American Society of Mechanical Engineers (ASME)
titleUnsteady Boundary Layers on a Flat Plate Disturbed by Periodic Wakes: Part I—Measurement of Wake-Affected Heat Transfer and Wake-Induced Transition Model
typeJournal Paper
journal volume118
journal issue2
journal titleJournal of Turbomachinery
identifier doi10.1115/1.2836643
journal fristpage327
journal lastpage336
identifier eissn1528-8900
keywordsHeat transfer
keywordsWakes
keywordsBoundary layers
keywordsFlat plates
keywordsTurbulence
keywordsGenerators
keywordsRotating Disks
keywordsCircular cylinders AND Measurement
treeJournal of Turbomachinery:;1996:;volume( 118 ):;issue: 002
contenttypeFulltext


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