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    An Investigation in the Numerical Approach to Solve the Heat Transfer Phenomenon in Gas Turbine

    Source: Journal of Energy Resources Technology:;2021:;volume( 143 ):;issue: 008::page 080805-1
    Author:
    Kumar, Sourabh
    ,
    Amano, Ryoichi S.
    DOI: 10.1115/1.4050081
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The gas turbine engine's extreme conditions need a robust design to produce efficient energy and for reliable operation. Flow and thermal analysis are essential for complex aerodynamic and thermodynamic interaction during turbine performance. There is a need to understand and predict the temperature to make the gas turbine engine efficient. This paper will outline the numerical methods applied for primary cooling methods in gas turbine blades. These include impinging leading-edge cooling, internal cooling in the midsection, and pin fin in the trailing edge. The main objective of this paper is to understand the numerical research done on improving gas turbine cooling. The emphasis will be on understanding the present computational fluid dynamics (CFD) techniques applied for gas turbine cooling and further development. This paper briefly outlines the new conjugate heat transfer–based CFD modeling techniques that have evolved over the years due to recent computing power development.
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      An Investigation in the Numerical Approach to Solve the Heat Transfer Phenomenon in Gas Turbine

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4278494
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    contributor authorKumar, Sourabh
    contributor authorAmano, Ryoichi S.
    date accessioned2022-02-06T05:39:37Z
    date available2022-02-06T05:39:37Z
    date copyright3/4/2021 12:00:00 AM
    date issued2021
    identifier issn0195-0738
    identifier otherjert_143_8_080805.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4278494
    description abstractThe gas turbine engine's extreme conditions need a robust design to produce efficient energy and for reliable operation. Flow and thermal analysis are essential for complex aerodynamic and thermodynamic interaction during turbine performance. There is a need to understand and predict the temperature to make the gas turbine engine efficient. This paper will outline the numerical methods applied for primary cooling methods in gas turbine blades. These include impinging leading-edge cooling, internal cooling in the midsection, and pin fin in the trailing edge. The main objective of this paper is to understand the numerical research done on improving gas turbine cooling. The emphasis will be on understanding the present computational fluid dynamics (CFD) techniques applied for gas turbine cooling and further development. This paper briefly outlines the new conjugate heat transfer–based CFD modeling techniques that have evolved over the years due to recent computing power development.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleAn Investigation in the Numerical Approach to Solve the Heat Transfer Phenomenon in Gas Turbine
    typeJournal Paper
    journal volume143
    journal issue8
    journal titleJournal of Energy Resources Technology
    identifier doi10.1115/1.4050081
    journal fristpage080805-1
    journal lastpage080805-11
    page11
    treeJournal of Energy Resources Technology:;2021:;volume( 143 ):;issue: 008
    contenttypeFulltext
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