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    Influence of Free-Stream Turbulence on Boundary Layer Transition in Favorable Pressure Gradients

    Source: Journal of Engineering for Gas Turbines and Power:;1982:;volume( 104 ):;issue: 004::page 743
    Author:
    M. F. Blair
    DOI: 10.1115/1.3227340
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Results from an experimental study of large-scale, two-dimensional incompressible transitional boundary layer flows are presented. Tests were conducted on a heated flat wall with a zero pressure gradient and for two levels of “sink” streamwise acceleration; k = ν/U2 ∂U/∂x = 0.2 or 0.75 × 10−6 . Free-stream turbulence intensity levels ranged from approximately 0.7 to 5 percent with limited data obtained outside these values. Convective heat-transfer distributions, laminar, transitional, and fully turbulent boundary layer mean velocity and temperature profile data, and free-stream turbulence intensity distributions are presented. Boundary layer integral quantities and shape factors are also given. Transition onset Reynolds number data obtained for this program agreed well with the results of other experimental and theoretical studies for both zero pressure gradient and accelerating flows. Comparisons of the profile data and wall heat-transfer distribution data indicated that fully turbulent mean velocity profiles were achieved upstream of fully turbulent wall heat-transfer rates.
    keyword(s): Turbulence , Boundary layers , Pressure gradient , Heat transfer , Flow (Dynamics) , Reynolds number , Shapes , Temperature profiles AND Boundary layer turbulence ,
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      Influence of Free-Stream Turbulence on Boundary Layer Transition in Favorable Pressure Gradients

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    http://yetl.yabesh.ir/yetl1/handle/yetl/95725
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    contributor authorM. F. Blair
    date accessioned2017-05-08T23:13:08Z
    date available2017-05-08T23:13:08Z
    date copyrightOctober, 1982
    date issued1982
    identifier issn1528-8919
    identifier otherJETPEZ-26777#743_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/95725
    description abstractResults from an experimental study of large-scale, two-dimensional incompressible transitional boundary layer flows are presented. Tests were conducted on a heated flat wall with a zero pressure gradient and for two levels of “sink” streamwise acceleration; k = ν/U2 ∂U/∂x = 0.2 or 0.75 × 10−6 . Free-stream turbulence intensity levels ranged from approximately 0.7 to 5 percent with limited data obtained outside these values. Convective heat-transfer distributions, laminar, transitional, and fully turbulent boundary layer mean velocity and temperature profile data, and free-stream turbulence intensity distributions are presented. Boundary layer integral quantities and shape factors are also given. Transition onset Reynolds number data obtained for this program agreed well with the results of other experimental and theoretical studies for both zero pressure gradient and accelerating flows. Comparisons of the profile data and wall heat-transfer distribution data indicated that fully turbulent mean velocity profiles were achieved upstream of fully turbulent wall heat-transfer rates.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleInfluence of Free-Stream Turbulence on Boundary Layer Transition in Favorable Pressure Gradients
    typeJournal Paper
    journal volume104
    journal issue4
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3227340
    journal fristpage743
    journal lastpage750
    identifier eissn0742-4795
    keywordsTurbulence
    keywordsBoundary layers
    keywordsPressure gradient
    keywordsHeat transfer
    keywordsFlow (Dynamics)
    keywordsReynolds number
    keywordsShapes
    keywordsTemperature profiles AND Boundary layer turbulence
    treeJournal of Engineering for Gas Turbines and Power:;1982:;volume( 104 ):;issue: 004
    contenttypeFulltext
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