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    Detailed Heat Transfer Coefficient Measurements and Thermal Analysis at Engine Conditions of a Pedestal With Fillet Radii

    Source: Journal of Turbomachinery:;1995:;volume( 117 ):;issue: 002::page 290
    Author:
    Z. Wang
    ,
    P. T. Ireland
    ,
    T. V. Jones
    DOI: 10.1115/1.2835658
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The heat transfer coefficient over the surface of a pedestal with fillet radii has been measured using thermochromic liquid crystals and the transient heat transfer method. The tests were performed at engine representative Reynolds numbers for a geometry typical of those used in turbine blade cooling systems. The heat conduction process that occurs in the engine was subsequently modeled numerically with a finite element discretization of the solid pedestal. The measured heat transfer coefficients were used to derive the exact boundary conditions applicable to the engine. The temperature field within the pedestal, calculated using the correct heat transfer coefficient distribution, is compared to that calculated using an area-averaged heat transfer coefficient. Metal temperature differences of 90 K are predicted across the blade wall.
    keyword(s): Measurement , Engines , Thermal analysis , Heat transfer coefficients , Temperature , Liquid crystals , Metals , Cooling systems , Transient heat , Reynolds number , Heat conduction , Turbine blades , Finite element analysis , Blades , Boundary-value problems AND Geometry ,
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      Detailed Heat Transfer Coefficient Measurements and Thermal Analysis at Engine Conditions of a Pedestal With Fillet Radii

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/116160
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    • Journal of Turbomachinery

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    contributor authorZ. Wang
    contributor authorP. T. Ireland
    contributor authorT. V. Jones
    date accessioned2017-05-08T23:48:38Z
    date available2017-05-08T23:48:38Z
    date copyrightApril, 1995
    date issued1995
    identifier issn0889-504X
    identifier otherJOTUEI-28643#290_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/116160
    description abstractThe heat transfer coefficient over the surface of a pedestal with fillet radii has been measured using thermochromic liquid crystals and the transient heat transfer method. The tests were performed at engine representative Reynolds numbers for a geometry typical of those used in turbine blade cooling systems. The heat conduction process that occurs in the engine was subsequently modeled numerically with a finite element discretization of the solid pedestal. The measured heat transfer coefficients were used to derive the exact boundary conditions applicable to the engine. The temperature field within the pedestal, calculated using the correct heat transfer coefficient distribution, is compared to that calculated using an area-averaged heat transfer coefficient. Metal temperature differences of 90 K are predicted across the blade wall.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleDetailed Heat Transfer Coefficient Measurements and Thermal Analysis at Engine Conditions of a Pedestal With Fillet Radii
    typeJournal Paper
    journal volume117
    journal issue2
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2835658
    journal fristpage290
    journal lastpage297
    identifier eissn1528-8900
    keywordsMeasurement
    keywordsEngines
    keywordsThermal analysis
    keywordsHeat transfer coefficients
    keywordsTemperature
    keywordsLiquid crystals
    keywordsMetals
    keywordsCooling systems
    keywordsTransient heat
    keywordsReynolds number
    keywordsHeat conduction
    keywordsTurbine blades
    keywordsFinite element analysis
    keywordsBlades
    keywordsBoundary-value problems AND Geometry
    treeJournal of Turbomachinery:;1995:;volume( 117 ):;issue: 002
    contenttypeFulltext
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