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    Simple Methods for Determining the Virtual Origin of Turbulent Boundary Layers in Hypersonic Flow on Sharp-Edged Flat Plates

    Source: Journal of Applied Mechanics:;1974:;volume( 041 ):;issue: 003::page 551
    Author:
    E. J. Hopkins
    DOI: 10.1115/1.3423346
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: For hypersonic Mach numbers up to about 8, the virtual origin for turbulent skin-friction calculations is shown to be close to the beginning of boundary-layer transition. A simple relationship between the beginning and end of boundary-layer transition is presented.
    keyword(s): Boundary layer turbulence , Flat plates , Hypersonic flow , Boundary layers , Mach number , Turbulence AND Skin friction (Fluid dynamics) ,
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      Simple Methods for Determining the Virtual Origin of Turbulent Boundary Layers in Hypersonic Flow on Sharp-Edged Flat Plates

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    http://yetl.yabesh.ir/yetl1/handle/yetl/164366
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    contributor authorE. J. Hopkins
    date accessioned2017-05-09T01:37:27Z
    date available2017-05-09T01:37:27Z
    date copyrightSeptember, 1974
    date issued1974
    identifier issn0021-8936
    identifier otherJAMCAV-26015#551_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/164366
    description abstractFor hypersonic Mach numbers up to about 8, the virtual origin for turbulent skin-friction calculations is shown to be close to the beginning of boundary-layer transition. A simple relationship between the beginning and end of boundary-layer transition is presented.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleSimple Methods for Determining the Virtual Origin of Turbulent Boundary Layers in Hypersonic Flow on Sharp-Edged Flat Plates
    typeJournal Paper
    journal volume41
    journal issue3
    journal titleJournal of Applied Mechanics
    identifier doi10.1115/1.3423346
    journal fristpage551
    journal lastpage553
    identifier eissn1528-9036
    keywordsBoundary layer turbulence
    keywordsFlat plates
    keywordsHypersonic flow
    keywordsBoundary layers
    keywordsMach number
    keywordsTurbulence AND Skin friction (Fluid dynamics)
    treeJournal of Applied Mechanics:;1974:;volume( 041 ):;issue: 003
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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