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    Simulation of Instantaneous Heat Transfer in Spark Ignition Internal Combustion Engines: Unsteady Thermal Boundary Layer Modeling

    Source: Journal of Engineering for Gas Turbines and Power:;2011:;volume( 133 ):;issue: 002::page 22802
    Author:
    David R. Buttsworth
    ,
    Abdalla Agrira
    ,
    Ray Malpress
    ,
    Talal Yusaf
    DOI: 10.1115/1.4001080
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Simulation of internal combustion engine heat transfer using low-dimensional thermodynamic modeling often relies on quasisteady heat transfer correlations. However, unsteady thermal boundary layer modeling could make a useful contribution because of the inherent unsteadiness of the internal combustion engine environment. Previous formulations of the unsteady energy equations for internal combustion engine thermal boundary layer modeling appear to imply that it is necessary to adopt the restrictive assumption that isentropic processes occur in the gas external to the thermal boundary layer. Such restrictions are not required and we have investigated if unsteady modeling can improve the simulation of crank-resolved heat transfer. A modest degree of success is reported for the present modeling, which relies on a constant effective turbulent thermal conductivity. Improvement in the unsteady thermal boundary layer simulations is expected in the future when the temporal and spatial variations in effective turbulent conductivity are correctly modeled.
    keyword(s): Heat transfer , Engines , Simulation , Internal combustion engines , Modeling , Equations , Heat flux , Thermal boundary layers AND Pressure ,
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      Simulation of Instantaneous Heat Transfer in Spark Ignition Internal Combustion Engines: Unsteady Thermal Boundary Layer Modeling

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/146099
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorDavid R. Buttsworth
    contributor authorAbdalla Agrira
    contributor authorRay Malpress
    contributor authorTalal Yusaf
    date accessioned2017-05-09T00:43:49Z
    date available2017-05-09T00:43:49Z
    date copyrightFebruary, 2011
    date issued2011
    identifier issn1528-8919
    identifier otherJETPEZ-27155#022802_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/146099
    description abstractSimulation of internal combustion engine heat transfer using low-dimensional thermodynamic modeling often relies on quasisteady heat transfer correlations. However, unsteady thermal boundary layer modeling could make a useful contribution because of the inherent unsteadiness of the internal combustion engine environment. Previous formulations of the unsteady energy equations for internal combustion engine thermal boundary layer modeling appear to imply that it is necessary to adopt the restrictive assumption that isentropic processes occur in the gas external to the thermal boundary layer. Such restrictions are not required and we have investigated if unsteady modeling can improve the simulation of crank-resolved heat transfer. A modest degree of success is reported for the present modeling, which relies on a constant effective turbulent thermal conductivity. Improvement in the unsteady thermal boundary layer simulations is expected in the future when the temporal and spatial variations in effective turbulent conductivity are correctly modeled.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleSimulation of Instantaneous Heat Transfer in Spark Ignition Internal Combustion Engines: Unsteady Thermal Boundary Layer Modeling
    typeJournal Paper
    journal volume133
    journal issue2
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4001080
    journal fristpage22802
    identifier eissn0742-4795
    keywordsHeat transfer
    keywordsEngines
    keywordsSimulation
    keywordsInternal combustion engines
    keywordsModeling
    keywordsEquations
    keywordsHeat flux
    keywordsThermal boundary layers AND Pressure
    treeJournal of Engineering for Gas Turbines and Power:;2011:;volume( 133 ):;issue: 002
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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