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contributor authorXiaohua Wu
contributor authorPaul A. Durbin
date accessioned2017-05-09T00:03:37Z
date available2017-05-09T00:03:37Z
date copyrightJuly, 2000
date issued2000
identifier issn0889-504X
identifier otherJOTUEI-28679#442_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/124462
description abstractTurbulent wakes swept across a flat plate boundary layer simulate the phenomenon of wake-induced bypass transition. Benchmark data from a direct numerical simulation of this process are presented and compared to Reynolds-averaged predictions. The data are phase-averaged skin friction and mean velocities. The predictions and data are found to agree in many important respects. One discrepancy is a failure to reproduce the skin friction overshoot following transition. [S0889-504X(00)00503-1]
publisherThe American Society of Mechanical Engineers (ASME)
titleBoundary Layer Transition Induced by Periodic Wakes
typeJournal Paper
journal volume122
journal issue3
journal titleJournal of Turbomachinery
identifier doi10.1115/1.1303076
journal fristpage442
journal lastpage449
identifier eissn1528-8900
keywordsFlow (Dynamics)
keywordsTurbulence
keywordsWakes
keywordsBoundary layers
keywordsComputation AND Skin friction (Fluid dynamics)
treeJournal of Turbomachinery:;2000:;volume( 122 ):;issue: 003
contenttypeFulltext


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