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contributor authorK. Funazaki
date accessioned2017-05-08T23:51:59Z
date available2017-05-08T23:51:59Z
date copyrightApril, 1996
date issued1996
identifier issn0889-504X
identifier otherJOTUEI-28651#337_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/117870
description abstractAs the second part of the study, detailed hot-wire anemometry measurements of wake-affected boundary layers on the flat plate are made. These measurements are organized in order, first, to check the standpoint of the modeling of the wake-induced transition proposed in Part I, and second, to observe wake–boundary layer interaction in detail from a viewpoint of direct and indirect effect of the wake passage upon turbulent spot generation within the boundary layer, as described by Walker (1993). The validity of the presumed state of the wake-affected boundary layer in the distance–time domain, which constitutes the basis of the transition model, is confirmed to great extent. However, it is also found that the criterion for the onset of the wake-induced transition adopted in Part I should be reconsidered. Some successful attempts are therefore made to specify the transition onset.
publisherThe American Society of Mechanical Engineers (ASME)
titleUnsteady Boundary Layers on a Flat Plate Disturbed by Periodic Wakes: Part II—Measurements of Unsteady Boundary Layers and Discussion
typeJournal Paper
journal volume118
journal issue2
journal titleJournal of Turbomachinery
identifier doi10.1115/1.2836644
journal fristpage337
journal lastpage344
identifier eissn1528-8900
keywordsMeasurement
keywordsWakes
keywordsBoundary layers
keywordsFlat plates
keywordsModeling
keywordsTurbulence AND Wire
treeJournal of Turbomachinery:;1996:;volume( 118 ):;issue: 002
contenttypeFulltext


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