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    Film Cooling Effectiveness and Mass/Heat Transfer Coefficient Downstream of One Row of Discrete Holes

    Source: Journal of Turbomachinery:;1999:;volume( 121 ):;issue: 002::page 225
    Author:
    R. J. Goldstein
    ,
    P. Jin
    ,
    R. L. Olson
    DOI: 10.1115/1.2841305
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A special naphthalene sublimation technique is used to study the film cooling performance downstream of one row of holes of 35 deg inclination angle with 3d hole spacing and relatively small hole length to diameter ratio (L/d = 6.3). Both film cooling effectiveness and mass/heat transfer coefficient are determined for blowing rates from 0.5 to 2.0 with density ratio of 1.0. The mass transfer coefficient is measured using pure air film injection, while the film cooling effectiveness is derived from comparison of mass transfer coefficients obtained following injection of naphthalene-vapor-saturated air with those from pure air injection. This technique enables one to obtain detailed local information on film cooling performance. The laterally averaged and local film cooling effectiveness agree with previous experiments. The difference between mass/heat transfer coefficients and previous heat transfer results indicates that conduction error may play an important role in the earlier heat transfer measurements.
    keyword(s): Cooling , Heat transfer coefficients , Mass transfer , Heat transfer , Density , Vapors , Measurement , Heat conduction AND Errors ,
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      Film Cooling Effectiveness and Mass/Heat Transfer Coefficient Downstream of One Row of Discrete Holes

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/123030
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    • Journal of Turbomachinery

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    contributor authorR. J. Goldstein
    contributor authorP. Jin
    contributor authorR. L. Olson
    date accessioned2017-05-09T00:01:17Z
    date available2017-05-09T00:01:17Z
    date copyrightApril, 1999
    date issued1999
    identifier issn0889-504X
    identifier otherJOTUEI-28669#225_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/123030
    description abstractA special naphthalene sublimation technique is used to study the film cooling performance downstream of one row of holes of 35 deg inclination angle with 3d hole spacing and relatively small hole length to diameter ratio (L/d = 6.3). Both film cooling effectiveness and mass/heat transfer coefficient are determined for blowing rates from 0.5 to 2.0 with density ratio of 1.0. The mass transfer coefficient is measured using pure air film injection, while the film cooling effectiveness is derived from comparison of mass transfer coefficients obtained following injection of naphthalene-vapor-saturated air with those from pure air injection. This technique enables one to obtain detailed local information on film cooling performance. The laterally averaged and local film cooling effectiveness agree with previous experiments. The difference between mass/heat transfer coefficients and previous heat transfer results indicates that conduction error may play an important role in the earlier heat transfer measurements.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleFilm Cooling Effectiveness and Mass/Heat Transfer Coefficient Downstream of One Row of Discrete Holes
    typeJournal Paper
    journal volume121
    journal issue2
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2841305
    journal fristpage225
    journal lastpage232
    identifier eissn1528-8900
    keywordsCooling
    keywordsHeat transfer coefficients
    keywordsMass transfer
    keywordsHeat transfer
    keywordsDensity
    keywordsVapors
    keywordsMeasurement
    keywordsHeat conduction AND Errors
    treeJournal of Turbomachinery:;1999:;volume( 121 ):;issue: 002
    contenttypeFulltext
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