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    A Resistive Model to Characterize Overall Effectiveness Influenced by Multiple Coolant Temperatures

    Source: Journal of Turbomachinery:;2022:;volume( 145 ):;issue: 002::page 21004-1
    Author:
    Rutledge, James L.
    ,
    Fuqua, Matthew N.
    ,
    Polanka, Marc D.
    ,
    Baker, William P.
    DOI: 10.1115/1.4055530
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The surface temperature of a film cooled turbine hot gas path component is typically nondimensionalized according to the overall effectiveness. This nondimensionalization scheme takes advantage of the fact that the surface temperature must be bounded by the coolant temperature and the freestream recovery temperature. Additional complexity arises when the surface temperature is influenced by the addition of a second coolant stream. While the surface temperature remains bounded by the cooler of the two coolant streams, the presence of the warmer stream means that the resulting overall effectiveness is now a function not only of the appropriately nondimensionalized coolant and freestream flowrates, but an additional nondimensional parameter that describes the relative difference in the two coolant temperatures. Previously, it was thought that experiments or computational fluid dynamics simulations would be required to discern this effect. In the present work, however, we introduce a linear resistive model that is based upon the exact solution to the energy equation and which accounts for the effect of any number of independent sources that influence the surface temperature. The model’s efficacy was demonstrated using experimental data acquired on conducting models in which two rows of holes ejected coolant from two independent plenums at two different temperatures.
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      A Resistive Model to Characterize Overall Effectiveness Influenced by Multiple Coolant Temperatures

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4291498
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    contributor authorRutledge, James L.
    contributor authorFuqua, Matthew N.
    contributor authorPolanka, Marc D.
    contributor authorBaker, William P.
    date accessioned2023-08-16T18:08:41Z
    date available2023-08-16T18:08:41Z
    date copyright10/11/2022 12:00:00 AM
    date issued2022
    identifier issn0889-504X
    identifier otherturbo_145_2_021004.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4291498
    description abstractThe surface temperature of a film cooled turbine hot gas path component is typically nondimensionalized according to the overall effectiveness. This nondimensionalization scheme takes advantage of the fact that the surface temperature must be bounded by the coolant temperature and the freestream recovery temperature. Additional complexity arises when the surface temperature is influenced by the addition of a second coolant stream. While the surface temperature remains bounded by the cooler of the two coolant streams, the presence of the warmer stream means that the resulting overall effectiveness is now a function not only of the appropriately nondimensionalized coolant and freestream flowrates, but an additional nondimensional parameter that describes the relative difference in the two coolant temperatures. Previously, it was thought that experiments or computational fluid dynamics simulations would be required to discern this effect. In the present work, however, we introduce a linear resistive model that is based upon the exact solution to the energy equation and which accounts for the effect of any number of independent sources that influence the surface temperature. The model’s efficacy was demonstrated using experimental data acquired on conducting models in which two rows of holes ejected coolant from two independent plenums at two different temperatures.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleA Resistive Model to Characterize Overall Effectiveness Influenced by Multiple Coolant Temperatures
    typeJournal Paper
    journal volume145
    journal issue2
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4055530
    journal fristpage21004-1
    journal lastpage21004-10
    page10
    treeJournal of Turbomachinery:;2022:;volume( 145 ):;issue: 002
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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