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contributor authorB. R. White
date accessioned2017-05-08T23:11:19Z
date available2017-05-08T23:11:19Z
date copyrightDecember, 1981
date issued1981
identifier issn0098-2202
identifier otherJFEGA4-26977#624_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/94677
description abstractThis paper presents experimental wind-tunnel data that show the universal logarithmic velocity profile for zero-pressure-gradient turbulent boundary layer flows is valid for values of momentum-deficit Reynolds numbers Rθ as low as 600. However, for values of Rθ between 425 and 600, the von Kármán and additive constants vary and are shown to be functions of Rθ and shape factor H. Furthermore, the viscous sublayer in the range 425<Rθ <600 can no longer maintain its characteristically small size. It is forced to grow, due to viscous effects, into a super sublayer (6-9 percent of the boundary layer height) that greatly exceeds conventional predictions of sublayer heights.
publisherThe American Society of Mechanical Engineers (ASME)
titleLow-Reynolds-Number Turbulent Boundary Layers
typeJournal Paper
journal volume103
journal issue4
journal titleJournal of Fluids Engineering
identifier doi10.1115/1.3241782
journal fristpage624
journal lastpage630
identifier eissn1528-901X
keywordsBoundary layer turbulence
keywordsFunctions
keywordsGradients
keywordsShapes
keywordsWind tunnels
keywordsPressure
keywordsMomentum
keywordsFlow (Dynamics)
keywordsReynolds number AND Boundary layers
treeJournal of Fluids Engineering:;1981:;volume( 103 ):;issue: 004
contenttypeFulltext


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