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    Similarity Analysis for Nonequilibrium Turbulent Boundary Layers*

    Source: Journal of Fluids Engineering:;2004:;volume( 126 ):;issue: 005::page 827
    Author:
    Luciano Castillo
    ,
    Xia Wang
    DOI: 10.1115/1.1789527
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In his now classical paper on pressure gradient turbulent boundary layers, Clauser concluded that equilibrium flows were very special flows difficult to achieve experimentally and that few flows were actually in equilibrium [1]. However, using similarity analysis of the Navier–Stokes equations, Castillo and George [2] defined an equilibrium flow as one where the pressure parameter, Λ=[δ/(ρU∞2dδ/dx)](dP∞/dx), was a constant. They further showed that most flows were in equilibrium and the exceptions were nonequilibrium flows where Λ≠constant. Using the equations of motion and similarity analysis, it will be shown that even nonequilibrium flows, as those over airfoils or with sudden changes on the external pressure gradient, are in equilibrium state, but only locally. Moreover, in the case of airfoils where the external pressure gradient changes from favorable to zero then to adverse, three distinctive regions are identified. Each region is given by a constant value of Λθ, and each region remains in equilibrium with Λθ=constant, respectively.
    keyword(s): Equilibrium (Physics) , Boundary layers , Boundary layer turbulence , Pressure , Flow (Dynamics) , Nonequilibrium flow , Pressure gradient , Reynolds number , Gradients AND Thickness ,
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      Similarity Analysis for Nonequilibrium Turbulent Boundary Layers*

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/130193
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    contributor authorLuciano Castillo
    contributor authorXia Wang
    date accessioned2017-05-09T00:13:20Z
    date available2017-05-09T00:13:20Z
    date copyrightSeptember, 2004
    date issued2004
    identifier issn0098-2202
    identifier otherJFEGA4-27201#827_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/130193
    description abstractIn his now classical paper on pressure gradient turbulent boundary layers, Clauser concluded that equilibrium flows were very special flows difficult to achieve experimentally and that few flows were actually in equilibrium [1]. However, using similarity analysis of the Navier–Stokes equations, Castillo and George [2] defined an equilibrium flow as one where the pressure parameter, Λ=[δ/(ρU∞2dδ/dx)](dP∞/dx), was a constant. They further showed that most flows were in equilibrium and the exceptions were nonequilibrium flows where Λ≠constant. Using the equations of motion and similarity analysis, it will be shown that even nonequilibrium flows, as those over airfoils or with sudden changes on the external pressure gradient, are in equilibrium state, but only locally. Moreover, in the case of airfoils where the external pressure gradient changes from favorable to zero then to adverse, three distinctive regions are identified. Each region is given by a constant value of Λθ, and each region remains in equilibrium with Λθ=constant, respectively.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleSimilarity Analysis for Nonequilibrium Turbulent Boundary Layers*
    typeJournal Paper
    journal volume126
    journal issue5
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.1789527
    journal fristpage827
    journal lastpage834
    identifier eissn1528-901X
    keywordsEquilibrium (Physics)
    keywordsBoundary layers
    keywordsBoundary layer turbulence
    keywordsPressure
    keywordsFlow (Dynamics)
    keywordsNonequilibrium flow
    keywordsPressure gradient
    keywordsReynolds number
    keywordsGradients AND Thickness
    treeJournal of Fluids Engineering:;2004:;volume( 126 ):;issue: 005
    contenttypeFulltext
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