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    Effects of Criterion Functions on Intermittency in Heated Transitional Boundary Layers With and Without Streamwise Acceleration

    Source: Journal of Turbomachinery:;1995:;volume( 117 ):;issue: 001::page 154
    Author:
    F. J. Keller
    ,
    T. Wang
    DOI: 10.1115/1.2835633
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Attempting 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.
    keyword(s): Boundary layers , Functions , Turbulence , Pressure gradient , Flow (Dynamics) , Temperature , Momentum , Mechanisms , Stress , Shear (Mechanics) AND Sampling (Acoustical engineering) ,
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      Effects of Criterion Functions on Intermittency in Heated Transitional Boundary Layers With and Without Streamwise Acceleration

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/116182
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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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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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