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    Estimating Over Temperature and Its Duration in a Flat Plate With Sudden Changes in Heating and Cooling

    Source: Journal of Turbomachinery:;2016:;volume( 138 ):;issue: 006::page 61007
    Author:
    Lee, Chien
    ,
    Shih, Tom I
    ,
    Mark Bryden, Kenneth
    DOI: 10.1115/1.4032306
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: When the operating condition of a gas turbine engine changes from one steadystate to another, the cooling must ensure that the solid's temperatures never exceed the maximum allowable throughout the transient process. Exceeding the maximum allowable temperature is possible even though cooling is increased to compensate for the increase in heating because there is a time lag in how the solid responds to changes in its convective heating and cooling environments. In this paper, a closedform solution (referred to as the 1D model) is derived to estimate the over temperature and its duration in a flat plate subjected to sudden changes in heating and cooling rates. For a given change in heating rate, the 1D model can also be used to estimate the minimum cooling needed to ensure that the new steadystate temperature will not exceed the maximum allowable. In addition, this model can estimate the temperature the material must be cooled to before imposing a sudden increase in heat load to ensure no over temperature throughout the transient process. Comparisons with the exact solutions show the 1D model to be accurate within 0.1%. This 1D model was generalized for application to problems in multidimensions. The generalized model was used to estimate the duration of over temperature in a twodimensional problem involving variable heat transfer coefficient (HTC) on the cooled side of a flat plate and provided results that match the exact solution within 5%.
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      Estimating Over Temperature and Its Duration in a Flat Plate With Sudden Changes in Heating and Cooling

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    contributor authorLee, Chien
    contributor authorShih, Tom I
    contributor authorMark Bryden, Kenneth
    date accessioned2017-05-09T01:34:10Z
    date available2017-05-09T01:34:10Z
    date issued2016
    identifier issn0889-504X
    identifier otherturbo_138_06_061007.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/162773
    description abstractWhen the operating condition of a gas turbine engine changes from one steadystate to another, the cooling must ensure that the solid's temperatures never exceed the maximum allowable throughout the transient process. Exceeding the maximum allowable temperature is possible even though cooling is increased to compensate for the increase in heating because there is a time lag in how the solid responds to changes in its convective heating and cooling environments. In this paper, a closedform solution (referred to as the 1D model) is derived to estimate the over temperature and its duration in a flat plate subjected to sudden changes in heating and cooling rates. For a given change in heating rate, the 1D model can also be used to estimate the minimum cooling needed to ensure that the new steadystate temperature will not exceed the maximum allowable. In addition, this model can estimate the temperature the material must be cooled to before imposing a sudden increase in heat load to ensure no over temperature throughout the transient process. Comparisons with the exact solutions show the 1D model to be accurate within 0.1%. This 1D model was generalized for application to problems in multidimensions. The generalized model was used to estimate the duration of over temperature in a twodimensional problem involving variable heat transfer coefficient (HTC) on the cooled side of a flat plate and provided results that match the exact solution within 5%.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleEstimating Over Temperature and Its Duration in a Flat Plate With Sudden Changes in Heating and Cooling
    typeJournal Paper
    journal volume138
    journal issue6
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4032306
    journal fristpage61007
    journal lastpage61007
    identifier eissn1528-8900
    treeJournal of Turbomachinery:;2016:;volume( 138 ):;issue: 006
    contenttypeFulltext
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