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contributor authorRama Govindarajan
contributor authorR. Narasimha
date accessioned2017-05-08T23:35:56Z
date available2017-05-08T23:35:56Z
date copyrightMarch, 1991
date issued1991
identifier issn0098-2202
identifier otherJFEGA4-27056#147_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/108775
description abstractAn analysis of procedures in current use for prediction of transition onset location shows that they are generally in poor agreement with data obtained in test facilities at low freestream turbulence levels. It has been shown elsewhere that under such conditions transition is driven by residual nonturbulent disturbances in the facility. A method is developed for taking such disturbances into account by defining an equivalent free-stream turbulence intensity; values for this parameter are derived for each facility from which onset data are available. A new correlation incorporating this effect is shown to be in good agreement with all available data on two-dimensional flows with pressure gradient. The correlation suggests that the onset Reynolds number (based on boundary-layer thickness) depends inversely on the total disturbance level when the latter is low.
publisherThe American Society of Mechanical Engineers (ASME)
titleThe Role of Residual Nonturbulent Disturbances on Transition Onset in Two-Dimensional Boundary Layers
typeJournal Paper
journal volume113
journal issue1
journal titleJournal of Fluids Engineering
identifier doi10.1115/1.2926488
journal fristpage147
journal lastpage149
identifier eissn1528-901X
keywordsBoundary layers
keywordsTurbulence
keywordsReynolds number
keywordsFlow (Dynamics)
keywordsPressure gradient
keywordsTest facilities AND Thickness
treeJournal of Fluids Engineering:;1991:;volume( 113 ):;issue: 001
contenttypeFulltext


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