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contributor authorJ. P. Gostelow
contributor authorA. R. Blunden
date accessioned2017-05-08T23:31:18Z
date available2017-05-08T23:31:18Z
date copyrightOctober, 1989
date issued1989
identifier issn0889-504X
identifier otherJOTUEI-28598#366_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/106125
description abstractBoundary layer transition was measured on a flat plate for four different turbulence levels. A range of adverse pressure gradients was imposed for one of these. The zero pressure gradient results were in agreement with accepted data for transition inception, length, and turbulent spot formation rate. They were also well represented by Narasimha’s universal intermittency distribution. A surprisingly strong similarity was also exhibited by intermittency distributions under adverse pressure gradients. Dimensionless velocity profiles were reasonable for the zero pressure gradient cases but difficulties with skin-friction prediction were experienced under adverse pressure gradient conditions. For this moderate turbulence level the transition inception Reynolds number remained reasonably constant with pressure gradient. Transition lengths, however, were greatly reduced by the imposition of even a weak adverse pressure gradient. This was associated with a strong increase in turbulent spot formation rate.
publisherThe American Society of Mechanical Engineers (ASME)
titleInvestigations of Boundary Layer Transition in an Adverse Pressure Gradient
typeJournal Paper
journal volume111
journal issue4
journal titleJournal of Turbomachinery
identifier doi10.1115/1.3262281
journal fristpage366
journal lastpage374
identifier eissn1528-8900
keywordsBoundary layers
keywordsPressure gradient
keywordsTurbulence
keywordsReynolds number
keywordsSkin friction (Fluid dynamics) AND Flat plates
treeJournal of Turbomachinery:;1989:;volume( 111 ):;issue: 004
contenttypeFulltext


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