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    An Inverse Inner-Variable Theory for Separated Turbulent Boundary Layers

    Source: Journal of Fluids Engineering:;1992:;volume( 114 ):;issue: 004::page 543
    Author:
    D. K. Das
    DOI: 10.1115/1.2910066
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An integral method is presented for computing separated and reattached turbulent boundary layers for incompressible two-dimensional flows. This method is a substantial improvement over the inner-variable approach of Das and White (1986), which was based on a direct boundary layer scheme that had several shortcomings. In this new approach, the integral equations have been completely reformulated so that the theory now proceeds in an inverse mode using displacement thickness as input. This new formulation eliminates the need for the second derivative of velocity distribution, which in the past has always been a source of error in all previous inner-variable approaches. Other significant additions are: (a) a single pressure gradient-wake correlation from a large amount of experimental data; and (b) replacement of the wake parameter from the final equations with a more stable parameter, wake velocity. Derivations of integral equations and their final working expressions, in both dimensional and nondimensional forms, are presented in detail. Predictions by this theory for skin friction, freestream velocity, momentum thickness, velocity profile and separation, and reattachment points agree well with experimental data. Sensitivity studies display that the theory is stable against variations in initial conditions, input distributions, and the pressure gradient-wake correlation.
    keyword(s): Boundary layer turbulence , Wakes , Gradients , Integral equations , Thickness , Pressure , Momentum , Flow (Dynamics) , Separation (Technology) , Skin friction (Fluid dynamics) , Displacement , Equations , Errors , Data acquisition systems AND Boundary layers ,
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      An Inverse Inner-Variable Theory for Separated Turbulent Boundary Layers

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    contributor authorD. K. Das
    date accessioned2017-05-08T23:38:39Z
    date available2017-05-08T23:38:39Z
    date copyrightDecember, 1992
    date issued1992
    identifier issn0098-2202
    identifier otherJFEGA4-27071#543_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/110377
    description abstractAn integral method is presented for computing separated and reattached turbulent boundary layers for incompressible two-dimensional flows. This method is a substantial improvement over the inner-variable approach of Das and White (1986), which was based on a direct boundary layer scheme that had several shortcomings. In this new approach, the integral equations have been completely reformulated so that the theory now proceeds in an inverse mode using displacement thickness as input. This new formulation eliminates the need for the second derivative of velocity distribution, which in the past has always been a source of error in all previous inner-variable approaches. Other significant additions are: (a) a single pressure gradient-wake correlation from a large amount of experimental data; and (b) replacement of the wake parameter from the final equations with a more stable parameter, wake velocity. Derivations of integral equations and their final working expressions, in both dimensional and nondimensional forms, are presented in detail. Predictions by this theory for skin friction, freestream velocity, momentum thickness, velocity profile and separation, and reattachment points agree well with experimental data. Sensitivity studies display that the theory is stable against variations in initial conditions, input distributions, and the pressure gradient-wake correlation.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleAn Inverse Inner-Variable Theory for Separated Turbulent Boundary Layers
    typeJournal Paper
    journal volume114
    journal issue4
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.2910066
    journal fristpage543
    journal lastpage553
    identifier eissn1528-901X
    keywordsBoundary layer turbulence
    keywordsWakes
    keywordsGradients
    keywordsIntegral equations
    keywordsThickness
    keywordsPressure
    keywordsMomentum
    keywordsFlow (Dynamics)
    keywordsSeparation (Technology)
    keywordsSkin friction (Fluid dynamics)
    keywordsDisplacement
    keywordsEquations
    keywordsErrors
    keywordsData acquisition systems AND Boundary layers
    treeJournal of Fluids Engineering:;1992:;volume( 114 ):;issue: 004
    contenttypeFulltext
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