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    Intermittent Flow and Thermal Structures of Accelerating Transitional Boundary Layers: Part 2—Fluctuation Quantities

    Source: Journal of Turbomachinery:;1999:;volume( 121 ):;issue: 001::page 106
    Author:
    T. Wang
    ,
    F. J. Keller
    DOI: 10.1115/1.2841217
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The conditionally sampled fluctuation quantities of nonaccelerating and accelerating heated transitional boundary layers were analyzed. The results indicated that the values of u′, υ′, uv , and ut , in the turbulent part of the transitional flow were higher than those values in the fully developed turbulent flow. These higher values were believed to be manifestations of the vigorous activities involved in the transition process. The contributions to the unconditioned u′ by “mean-step” change due to the alternating behavior between turbulent and nonturbulent flows are about 20 percent in the near-wall region, but are negligible for Y+ > 30. The turbulent part uv values are higher than the fully turbulent and unconditioned values in the inner boundary layer but lower in the outer boundary layer. The mean-step change has negligible effect on unconditioned uv values. As acceleration increases, both u′ and t′ in the turbulent part are suppressed; however, turbulent part u′ is still higher than the unconditioned u′ Acceleration promotes streamwise Reynolds heat flux (ut ) transport in both turbulent and nonturbulent parts. A second peak of the turbulent part ut occurs at around Y+ = 120 as acceleration increases. The turbulent part eddy viscosity values are much lower than those in the fully turbulent flow.
    keyword(s): Flow (Dynamics) , Boundary layers , Turbulence , Eddies (Fluid dynamics) , Viscosity , Fully developed turbulent flow AND Heat flux ,
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      Intermittent Flow and Thermal Structures of Accelerating Transitional Boundary Layers: Part 2—Fluctuation Quantities

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    http://yetl.yabesh.ir/yetl1/handle/yetl/123066
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    contributor authorT. Wang
    contributor authorF. J. Keller
    date accessioned2017-05-09T00:01:21Z
    date available2017-05-09T00:01:21Z
    date copyrightJanuary, 1999
    date issued1999
    identifier issn0889-504X
    identifier otherJOTUEI-28668#106_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/123066
    description abstractThe conditionally sampled fluctuation quantities of nonaccelerating and accelerating heated transitional boundary layers were analyzed. The results indicated that the values of u′, υ′, uv , and ut , in the turbulent part of the transitional flow were higher than those values in the fully developed turbulent flow. These higher values were believed to be manifestations of the vigorous activities involved in the transition process. The contributions to the unconditioned u′ by “mean-step” change due to the alternating behavior between turbulent and nonturbulent flows are about 20 percent in the near-wall region, but are negligible for Y+ > 30. The turbulent part uv values are higher than the fully turbulent and unconditioned values in the inner boundary layer but lower in the outer boundary layer. The mean-step change has negligible effect on unconditioned uv values. As acceleration increases, both u′ and t′ in the turbulent part are suppressed; however, turbulent part u′ is still higher than the unconditioned u′ Acceleration promotes streamwise Reynolds heat flux (ut ) transport in both turbulent and nonturbulent parts. A second peak of the turbulent part ut occurs at around Y+ = 120 as acceleration increases. The turbulent part eddy viscosity values are much lower than those in the fully turbulent flow.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleIntermittent Flow and Thermal Structures of Accelerating Transitional Boundary Layers: Part 2—Fluctuation Quantities
    typeJournal Paper
    journal volume121
    journal issue1
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2841217
    journal fristpage106
    journal lastpage112
    identifier eissn1528-8900
    keywordsFlow (Dynamics)
    keywordsBoundary layers
    keywordsTurbulence
    keywordsEddies (Fluid dynamics)
    keywordsViscosity
    keywordsFully developed turbulent flow AND Heat flux
    treeJournal of Turbomachinery:;1999:;volume( 121 ):;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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