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    Some Boundary Layer-Porous Wall Coupling Effects in Laminar Flows With Surface Injection

    Source: Journal of Engineering for Gas Turbines and Power:;1970:;volume( 092 ):;issue: 003::page 257
    Author:
    D. A. Nealy
    ,
    P. W. McFadden
    DOI: 10.1115/1.3445350
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Using the integral form of the laminar boundary layer thermal energy equation, a method is developed which permits calculation of thermal boundary layer development under more general conditions than heretofore treated in the literature. The local Stanton number is expressed in terms of the thermal convection thickness which reflects the cumulative effects of variable free stream velocity, surface temperature, and injection rate on boundary layer development. The boundary layer calculation is combined with the wall heat transfer problem through a coolant heat balance which includes the effect of axial conduction in the wall. The highly coupled boundary layer and wall heat balance equations are solved simultaneously using relatively straightforward numerical integration techniques. Calculated results exhibit good agreement with existing analytical and experimental results. The present results indicate that nonisothermal wall and axial conduction effects significantly affect local heat transfer rates.
    keyword(s): Heat , Temperature , Heat transfer , Thermal energy , Laminar flow , Heat conduction , Coolants , Boundary layers , Convection , Equations , Thickness AND Thermal boundary layers ,
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      Some Boundary Layer-Porous Wall Coupling Effects in Laminar Flows With Surface Injection

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/142211
    Collections
    • Journal of Engineering for Gas Turbines and Power

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    contributor authorD. A. Nealy
    contributor authorP. W. McFadden
    date accessioned2017-05-09T00:35:54Z
    date available2017-05-09T00:35:54Z
    date copyrightJuly, 1970
    date issued1970
    identifier issn1528-8919
    identifier otherJETPEZ-26687#257_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/142211
    description abstractUsing the integral form of the laminar boundary layer thermal energy equation, a method is developed which permits calculation of thermal boundary layer development under more general conditions than heretofore treated in the literature. The local Stanton number is expressed in terms of the thermal convection thickness which reflects the cumulative effects of variable free stream velocity, surface temperature, and injection rate on boundary layer development. The boundary layer calculation is combined with the wall heat transfer problem through a coolant heat balance which includes the effect of axial conduction in the wall. The highly coupled boundary layer and wall heat balance equations are solved simultaneously using relatively straightforward numerical integration techniques. Calculated results exhibit good agreement with existing analytical and experimental results. The present results indicate that nonisothermal wall and axial conduction effects significantly affect local heat transfer rates.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleSome Boundary Layer-Porous Wall Coupling Effects in Laminar Flows With Surface Injection
    typeJournal Paper
    journal volume92
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3445350
    journal fristpage257
    journal lastpage266
    identifier eissn0742-4795
    keywordsHeat
    keywordsTemperature
    keywordsHeat transfer
    keywordsThermal energy
    keywordsLaminar flow
    keywordsHeat conduction
    keywordsCoolants
    keywordsBoundary layers
    keywordsConvection
    keywordsEquations
    keywordsThickness AND Thermal boundary layers
    treeJournal of Engineering for Gas Turbines and Power:;1970:;volume( 092 ):;issue: 003
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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