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    A Superposition Technique for Predicting Overall Effectiveness With Multiple Sources of Individually Characterized Internal and External Coolant Flows

    Source: Journal of Turbomachinery:;2024:;volume( 146 ):;issue: 012::page 121008-1
    Author:
    Fuqua, Matthew N.
    ,
    Rutledge, James L.
    DOI: 10.1115/1.4065746
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: High-performance gas turbine engines rely on intricate cooling schemes to protect turbine components from the high-temperature freestream gas. Determining the optimal placement of film cooling holes in optimal locations while remaining mindful of the consumption of precious coolant air is therefore an interesting design challenge. For several decades, a method of superposition has been in use that provides a reasonable prediction of the adiabatic effectiveness in a region influenced by multiple rows of film cooling holes acting together if the adiabatic effectiveness distributions resulting from individual rows are already known. This classical superposition technique has been used with success to at least provide a first cut at determining where coolant holes might be placed on turbine components. One of the shortcomings of the method is that it strictly applies only to the prediction of adiabatic effectiveness which is indicative of the adiabatic wall temperature, not the actual surface temperature of the turbine component. Indeed, the overall effectiveness, which is indicative of the actual surface temperature, is somewhat more complicated as it is influenced not only by external cooling but also by internal cooling. In the present work, a method of superposition of overall effectiveness data is proposed, thereby allowing prediction of the actual surface temperature distribution on a component. Experimental results show that it is possible to use knowledge of the overall effectiveness distributions resulting from individual internal cooling and associated film cooling holes acting alone to determine how they are likely going to act when combined. This technique shows promise for a turbine designer to use superposition for actual surface temperature prediction, not just adiabatic wall temperature prediction, and therefore higher quality initial cooling designs.
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      A Superposition Technique for Predicting Overall Effectiveness With Multiple Sources of Individually Characterized Internal and External Coolant Flows

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    contributor authorFuqua, Matthew N.
    contributor authorRutledge, James L.
    date accessioned2024-12-24T18:44:27Z
    date available2024-12-24T18:44:27Z
    date copyright7/23/2024 12:00:00 AM
    date issued2024
    identifier issn0889-504X
    identifier otherturbo_146_12_121008.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4302659
    description abstractHigh-performance gas turbine engines rely on intricate cooling schemes to protect turbine components from the high-temperature freestream gas. Determining the optimal placement of film cooling holes in optimal locations while remaining mindful of the consumption of precious coolant air is therefore an interesting design challenge. For several decades, a method of superposition has been in use that provides a reasonable prediction of the adiabatic effectiveness in a region influenced by multiple rows of film cooling holes acting together if the adiabatic effectiveness distributions resulting from individual rows are already known. This classical superposition technique has been used with success to at least provide a first cut at determining where coolant holes might be placed on turbine components. One of the shortcomings of the method is that it strictly applies only to the prediction of adiabatic effectiveness which is indicative of the adiabatic wall temperature, not the actual surface temperature of the turbine component. Indeed, the overall effectiveness, which is indicative of the actual surface temperature, is somewhat more complicated as it is influenced not only by external cooling but also by internal cooling. In the present work, a method of superposition of overall effectiveness data is proposed, thereby allowing prediction of the actual surface temperature distribution on a component. Experimental results show that it is possible to use knowledge of the overall effectiveness distributions resulting from individual internal cooling and associated film cooling holes acting alone to determine how they are likely going to act when combined. This technique shows promise for a turbine designer to use superposition for actual surface temperature prediction, not just adiabatic wall temperature prediction, and therefore higher quality initial cooling designs.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleA Superposition Technique for Predicting Overall Effectiveness With Multiple Sources of Individually Characterized Internal and External Coolant Flows
    typeJournal Paper
    journal volume146
    journal issue12
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4065746
    journal fristpage121008-1
    journal lastpage121008-9
    page9
    treeJournal of Turbomachinery:;2024:;volume( 146 ):;issue: 012
    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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