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    Analysis of the Temperature Profile of Ceramic Composite Materials Exposed to Combined Conduction–Radiation Between Concentric Cylinders

    Source: Journal of Engineering for Gas Turbines and Power:;1998:;volume( 120 ):;issue: 002::page 271
    Author:
    A. Tremante
    ,
    F. Malpica
    DOI: 10.1115/1.2818115
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A numerical study is made of the thermal characteristics of semitransparent materials exposed to simultaneous conduction and radiation between concentric cylinders. 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. Through the use of a gray model and the two-flux method, specialized equations are developed that generate a system of nonlinear ordinary differential equations. To facilitate the solution of this system, an iterative strategy is adopted. In order to demonstrate the versatility and accuracy of the proposed methodology, the results of several numerical experiments are presented and compared with benchmark solutions.
    keyword(s): Heat conduction , Ceramic composites , Cylinders , Radiation (Physics) , Temperature profiles , High temperature , Engines , Compressors , Equations , Nuclear reactors , Space vehicles , Differential equations , Turbines , Radiative heat transfer , Composite materials , Ceramics AND Control systems ,
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      Analysis of the Temperature Profile of Ceramic Composite Materials Exposed to Combined Conduction–Radiation Between Concentric Cylinders

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/120430
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorA. Tremante
    contributor authorF. Malpica
    date accessioned2017-05-08T23:56:35Z
    date available2017-05-08T23:56:35Z
    date copyrightApril, 1998
    date issued1998
    identifier issn1528-8919
    identifier otherJETPEZ-26778#271_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/120430
    description abstractA numerical study is made of the thermal characteristics of semitransparent materials exposed to simultaneous conduction and radiation between concentric cylinders. 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. Through the use of a gray model and the two-flux method, specialized equations are developed that generate a system of nonlinear ordinary differential equations. To facilitate the solution of this system, an iterative strategy is adopted. In order to demonstrate the versatility and accuracy of the proposed methodology, the results of several numerical experiments are presented and compared with benchmark solutions.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleAnalysis of the Temperature Profile of Ceramic Composite Materials Exposed to Combined Conduction–Radiation Between Concentric Cylinders
    typeJournal Paper
    journal volume120
    journal issue2
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2818115
    journal fristpage271
    journal lastpage275
    identifier eissn0742-4795
    keywordsHeat conduction
    keywordsCeramic composites
    keywordsCylinders
    keywordsRadiation (Physics)
    keywordsTemperature profiles
    keywordsHigh temperature
    keywordsEngines
    keywordsCompressors
    keywordsEquations
    keywordsNuclear reactors
    keywordsSpace vehicles
    keywordsDifferential equations
    keywordsTurbines
    keywordsRadiative heat transfer
    keywordsComposite materials
    keywordsCeramics AND Control systems
    treeJournal of Engineering for Gas Turbines and Power:;1998:;volume( 120 ):;issue: 002
    contenttypeFulltext
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