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contributor authorF. J. Keller
contributor authorT. Wang
date accessioned2017-05-08T23:48:40Z
date available2017-05-08T23:48:40Z
date copyrightJanuary, 1995
date issued1995
identifier issn0889-504X
identifier otherJOTUEI-28642#154_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/116182
description abstractAttempting to understand the mechanisms of momentum and thermal transports in transitional boundary layers has resulted in the use of conditional sampling to separate the flow into turbulent and nonturbulent portions. The choice of a proper criterion function to discriminate between the two flow conditions is critical. A detailed experimental investigation was performed to determine the effects of different criterion functions on the determination of intermittency for application in heated transitional boundary layers with and without streamwise acceleration. Nine separate criterion functions were investigated for the baseline case without pressure gradient and three cases with streamwise pressure gradient. Inherent differences were found to exist between each criterion function’s turbulence recognition capabilities. The results indicate that using a criterion function based on Reynolds shear stress, (∂uv/∂τ)2 , for turbulent/nonturbulent discrimination in a heated transitional boundary layer is superior to a single velocity or temperature scheme. Peak values in intermittency for the early to midtransitional region were found to occur away from the wall at approximately y/δ = 0.3 for all cases. To match the universal intermittency distribution of Dhawan and Narasimha (1958), the minimum values of intermittency at y / δ ≈ 0.1 should be used as the representative “near-wall” values.
publisherThe American Society of Mechanical Engineers (ASME)
titleEffects of Criterion Functions on Intermittency in Heated Transitional Boundary Layers With and Without Streamwise Acceleration
typeJournal Paper
journal volume117
journal issue1
journal titleJournal of Turbomachinery
identifier doi10.1115/1.2835633
journal fristpage154
journal lastpage165
identifier eissn1528-8900
keywordsBoundary layers
keywordsFunctions
keywordsTurbulence
keywordsPressure gradient
keywordsFlow (Dynamics)
keywordsTemperature
keywordsMomentum
keywordsMechanisms
keywordsStress
keywordsShear (Mechanics) AND Sampling (Acoustical engineering)
treeJournal of Turbomachinery:;1995:;volume( 117 ):;issue: 001
contenttypeFulltext


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