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    A Reduced Order Model of the Mean Properties of a Turbulent Wall Boundary Layer at a Zero Pressure Gradient

    Source: Journal of Fluids Engineering:;2014:;volume( 136 ):;issue: 003::page 31103
    Author:
    Xu, Lei
    ,
    Rusak, Zvi
    ,
    Castillo, Luciano
    DOI: 10.1115/1.4026418
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A novel twoequations model for computing the flow properties of a spatiallydeveloping, incompressible, zeropressuregradient, turbulent boundary layer over a smooth, flat wall is developed. The mean streamwise velocity component inside the boundary layer is described by the Reynoldsaveraged Navier–Stokes equation where the Reynolds shear stress is given by an extended mixinglength model. The nondimensional form of the mixing length is described by a polynomial function in terms of the nondimensional wall normal coordinate. Moreover, a stream function approach is applied with a leadingorder term described by a similarity function. Two ordinary differential equations are derived for the solution of the similarity function along the wall normal coordinate and for its streamwise location. A numerical integration scheme of the model equations is developed and enables the solution of flow properties. The coefficients of the mixinglength polynomial function are modified at each streamwise location as part of solution iterations to satisfy the wall and farfield boundary conditions and adjust the local boundary layer thickness, خ´99.4, to a location where streamwise speed is 99.4% of the farfield streamwise velocity. The elegance of the present approach is established through the successful solution of the various flow properties across the boundary layer (i.e., mean streamwise velocity, viscous stress, Reynolds shear stress, skin friction coefficient, and growth rate of boundary layer among others) from the laminar regime all the way to the fully turbulent regime. It is found that results agree with much available experimental data and direct numerical simulations for a wide range of Reخ¸ based on the momentum thickness (Reخ¸) from 15 up to 106, except for the transition region from laminar to turbulent flow. Furthermore, results shed light on the von Kأ،rmأ،n constant as a function of Reخ¸, the possible fourlayer nature of the mean streamwise velocity profile, the universal profiles of the streamwise velocity and the Reynolds shear stress at high Reخ¸, and the scaling laws at the outer region.
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      A Reduced Order Model of the Mean Properties of a Turbulent Wall Boundary Layer at a Zero Pressure Gradient

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    http://yetl.yabesh.ir/yetl1/handle/yetl/154950
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    contributor authorXu, Lei
    contributor authorRusak, Zvi
    contributor authorCastillo, Luciano
    date accessioned2017-05-09T01:08:26Z
    date available2017-05-09T01:08:26Z
    date issued2014
    identifier issn0098-2202
    identifier otherfe_136_03_031103.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/154950
    description abstractA novel twoequations model for computing the flow properties of a spatiallydeveloping, incompressible, zeropressuregradient, turbulent boundary layer over a smooth, flat wall is developed. The mean streamwise velocity component inside the boundary layer is described by the Reynoldsaveraged Navier–Stokes equation where the Reynolds shear stress is given by an extended mixinglength model. The nondimensional form of the mixing length is described by a polynomial function in terms of the nondimensional wall normal coordinate. Moreover, a stream function approach is applied with a leadingorder term described by a similarity function. Two ordinary differential equations are derived for the solution of the similarity function along the wall normal coordinate and for its streamwise location. A numerical integration scheme of the model equations is developed and enables the solution of flow properties. The coefficients of the mixinglength polynomial function are modified at each streamwise location as part of solution iterations to satisfy the wall and farfield boundary conditions and adjust the local boundary layer thickness, خ´99.4, to a location where streamwise speed is 99.4% of the farfield streamwise velocity. The elegance of the present approach is established through the successful solution of the various flow properties across the boundary layer (i.e., mean streamwise velocity, viscous stress, Reynolds shear stress, skin friction coefficient, and growth rate of boundary layer among others) from the laminar regime all the way to the fully turbulent regime. It is found that results agree with much available experimental data and direct numerical simulations for a wide range of Reخ¸ based on the momentum thickness (Reخ¸) from 15 up to 106, except for the transition region from laminar to turbulent flow. Furthermore, results shed light on the von Kأ،rmأ،n constant as a function of Reخ¸, the possible fourlayer nature of the mean streamwise velocity profile, the universal profiles of the streamwise velocity and the Reynolds shear stress at high Reخ¸, and the scaling laws at the outer region.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleA Reduced Order Model of the Mean Properties of a Turbulent Wall Boundary Layer at a Zero Pressure Gradient
    typeJournal Paper
    journal volume136
    journal issue3
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.4026418
    journal fristpage31103
    journal lastpage31103
    identifier eissn1528-901X
    treeJournal of Fluids Engineering:;2014:;volume( 136 ):;issue: 003
    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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