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    An Approximate Solution to the Shuttle Heat-Transfer Losses in a Reciprocating Machine

    Source: Journal of Engineering for Gas Turbines and Power:;1971:;volume( 093 ):;issue: 002::page 177
    Author:
    P. A. Rios
    DOI: 10.1115/1.3445549
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The axial heat transfer due to the oscillatory motion of a long displacer in a cylinder with an axial temperature gradient is treated. The effect of the resistance to heat transfer due to the radial clearance between the displacer and the cylinder is considered, as well as the effect of a limited thermal diffusivity in the walls. A method for the estimation of the effect of the gas flow in the clearance volume is presented. A simple approximate solution is obtained by linearization and application of Fourier series. The effect of radial clearance, material properties, length, and wall thickness on the net heat transfer rate is discussed.
    keyword(s): Heat transfer , Machinery , Clearances (Engineering) , Cylinders , Fourier series , Wall thickness , Temperature gradients , Motion , Electrical resistance , Gas flow , Thermal diffusivity AND Materials properties ,
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      An Approximate Solution to the Shuttle Heat-Transfer Losses in a Reciprocating Machine

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/151111
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorP. A. Rios
    date accessioned2017-05-09T00:56:50Z
    date available2017-05-09T00:56:50Z
    date copyrightApril, 1971
    date issued1971
    identifier issn1528-8919
    identifier otherJETPEZ-26692#177_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/151111
    description abstractThe axial heat transfer due to the oscillatory motion of a long displacer in a cylinder with an axial temperature gradient is treated. The effect of the resistance to heat transfer due to the radial clearance between the displacer and the cylinder is considered, as well as the effect of a limited thermal diffusivity in the walls. A method for the estimation of the effect of the gas flow in the clearance volume is presented. A simple approximate solution is obtained by linearization and application of Fourier series. The effect of radial clearance, material properties, length, and wall thickness on the net heat transfer rate is discussed.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleAn Approximate Solution to the Shuttle Heat-Transfer Losses in a Reciprocating Machine
    typeJournal Paper
    journal volume93
    journal issue2
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3445549
    journal fristpage177
    journal lastpage182
    identifier eissn0742-4795
    keywordsHeat transfer
    keywordsMachinery
    keywordsClearances (Engineering)
    keywordsCylinders
    keywordsFourier series
    keywordsWall thickness
    keywordsTemperature gradients
    keywordsMotion
    keywordsElectrical resistance
    keywordsGas flow
    keywordsThermal diffusivity AND Materials properties
    treeJournal of Engineering for Gas Turbines and Power:;1971:;volume( 093 ):;issue: 002
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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