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    Contribution of Thermal Radiation to the Temperature Profile of Ceramic Composite Materials

    Source: Journal of Engineering for Gas Turbines and Power:;1994:;volume( 116 ):;issue: 003::page 583
    Author:
    A. Tremante
    ,
    F. Malpica
    DOI: 10.1115/1.2906859
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The steady energy transfer equation for simultaneous conduction and radiation in an absorbing, emitting, and nonscattering gray planar medium is studied theoretically. For extremely high-temperature applications, where radiative transfer plays an important role, ceramic-matrix composites, considered as semitransparent materials, are being explored for potential use in turbine and compressor components, spacecraft structures, engine control systems, and nuclear reactors. Exact solution of the above-mentioned radiative problems is seldom possible and time-consuming numerical approximations are then used. A technique combining an accurate physical formulation, the two-flux model, coupled to a fast numerical procedure for the calculation of the temperature and heat fluxes is described.
    keyword(s): Heat , Temperature , Energy transformation , Radiative heat transfer , Composite materials , Ceramics , Control systems , Radiation (Physics) , Engines , Compressors , Heat conduction , Ceramic composites , Flux (Metallurgy) , Thermal radiation , Turbines , Approximation , Equations , Nuclear reactors , Space vehicles , Temperature profiles AND High temperature ,
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      Contribution of Thermal Radiation to the Temperature Profile of Ceramic Composite Materials

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/113547
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorA. Tremante
    contributor authorF. Malpica
    date accessioned2017-05-08T23:44:06Z
    date available2017-05-08T23:44:06Z
    date copyrightJuly, 1994
    date issued1994
    identifier issn1528-8919
    identifier otherJETPEZ-26729#583_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/113547
    description abstractThe steady energy transfer equation for simultaneous conduction and radiation in an absorbing, emitting, and nonscattering gray planar medium is studied theoretically. For extremely high-temperature applications, where radiative transfer plays an important role, ceramic-matrix composites, considered as semitransparent materials, are being explored for potential use in turbine and compressor components, spacecraft structures, engine control systems, and nuclear reactors. Exact solution of the above-mentioned radiative problems is seldom possible and time-consuming numerical approximations are then used. A technique combining an accurate physical formulation, the two-flux model, coupled to a fast numerical procedure for the calculation of the temperature and heat fluxes is described.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleContribution of Thermal Radiation to the Temperature Profile of Ceramic Composite Materials
    typeJournal Paper
    journal volume116
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2906859
    journal fristpage583
    journal lastpage586
    identifier eissn0742-4795
    keywordsHeat
    keywordsTemperature
    keywordsEnergy transformation
    keywordsRadiative heat transfer
    keywordsComposite materials
    keywordsCeramics
    keywordsControl systems
    keywordsRadiation (Physics)
    keywordsEngines
    keywordsCompressors
    keywordsHeat conduction
    keywordsCeramic composites
    keywordsFlux (Metallurgy)
    keywordsThermal radiation
    keywordsTurbines
    keywordsApproximation
    keywordsEquations
    keywordsNuclear reactors
    keywordsSpace vehicles
    keywordsTemperature profiles AND High temperature
    treeJournal of Engineering for Gas Turbines and Power:;1994:;volume( 116 ):;issue: 003
    contenttypeFulltext
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