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    A Method for the Calculation of 3D Boundary Layers on Practical Wing Configurations

    Source: Journal of Fluids Engineering:;1981:;volume( 103 ):;issue: 001::page 104
    Author:
    J. P. F. Lindhout
    ,
    G. Moek
    ,
    E. De Boer
    ,
    B. Van Den Berg
    DOI: 10.1115/1.3240755
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper gives a description of a calculation method for 3D turbulent and laminar boundary layers on nondevelopable surfaces. A simple eddy viscosity model is incorporated in the method. Special attention is given to the organization of the computations to circumvent as much as possible stepsize limitations. The method is also able to proceed the computation around separated flow regions. The method has been applied to the laminar boundary layer flow over a flat plate with attached cylinder, and to a turbulent boundary layer flow over an airplane wing.
    keyword(s): Boundary layers , Wings , Flow (Dynamics) , Computation , Cylinders , Flat plates , Aircraft , Boundary layer turbulence , Turbulence , Eddies (Fluid dynamics) AND Viscosity ,
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      A Method for the Calculation of 3D Boundary Layers on Practical Wing Configurations

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/94760
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    • Journal of Fluids Engineering

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    contributor authorJ. P. F. Lindhout
    contributor authorG. Moek
    contributor authorE. De Boer
    contributor authorB. Van Den Berg
    date accessioned2017-05-08T23:11:31Z
    date available2017-05-08T23:11:31Z
    date copyrightMarch, 1981
    date issued1981
    identifier issn0098-2202
    identifier otherJFEGA4-26968#104_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/94760
    description abstractThis paper gives a description of a calculation method for 3D turbulent and laminar boundary layers on nondevelopable surfaces. A simple eddy viscosity model is incorporated in the method. Special attention is given to the organization of the computations to circumvent as much as possible stepsize limitations. The method is also able to proceed the computation around separated flow regions. The method has been applied to the laminar boundary layer flow over a flat plate with attached cylinder, and to a turbulent boundary layer flow over an airplane wing.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleA Method for the Calculation of 3D Boundary Layers on Practical Wing Configurations
    typeJournal Paper
    journal volume103
    journal issue1
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.3240755
    journal fristpage104
    journal lastpage111
    identifier eissn1528-901X
    keywordsBoundary layers
    keywordsWings
    keywordsFlow (Dynamics)
    keywordsComputation
    keywordsCylinders
    keywordsFlat plates
    keywordsAircraft
    keywordsBoundary layer turbulence
    keywordsTurbulence
    keywordsEddies (Fluid dynamics) AND Viscosity
    treeJournal of Fluids Engineering:;1981:;volume( 103 ):;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
    yabeshDSpacePersian