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    Measurement of Gust Response on a Turbine Cascade

    Source: Journal of Turbomachinery:;1997:;volume( 119 ):;issue: 002::page 238
    Author:
    A. P. Kurkov
    ,
    B. L. Lucci
    DOI: 10.1115/1.2841106
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The paper presents benchmark experimental data on a gust response of an annular turbine cascade. The experiment was particularly designed to provide data for comparison with the results of a typical linearized gust-response analysis. Reduced frequency, Mach number, and incidence were varied independently. Except for the lowest reduced frequency, the gust velocity distribution was nearly sinusoidal. For the high-inlet-velocity series of tests, the cascade was near choking. The mean flow was documented by measuring blade surface pressures and the cascade exit flow. High-response pressure transducers were used to measure the unsteady pressure distribution. Inlet-velocity components and turbulence parameters were measured using hot wire. In addition to the synchronous time-averaged pressure spectra, typical power spectra are included for several representative conditions.
    keyword(s): Cascades (Fluid dynamics) , Turbines , Pressure , Flow (Dynamics) , Spectra (Spectroscopy) , Turbulence , Wire , Pressure transducers , Mach number AND Blades ,
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      Measurement of Gust Response on a Turbine Cascade

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    http://yetl.yabesh.ir/yetl1/handle/yetl/119629
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    contributor authorA. P. Kurkov
    contributor authorB. L. Lucci
    date accessioned2017-05-08T23:55:09Z
    date available2017-05-08T23:55:09Z
    date copyrightApril, 1997
    date issued1997
    identifier issn0889-504X
    identifier otherJOTUEI-28659#238_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/119629
    description abstractThe paper presents benchmark experimental data on a gust response of an annular turbine cascade. The experiment was particularly designed to provide data for comparison with the results of a typical linearized gust-response analysis. Reduced frequency, Mach number, and incidence were varied independently. Except for the lowest reduced frequency, the gust velocity distribution was nearly sinusoidal. For the high-inlet-velocity series of tests, the cascade was near choking. The mean flow was documented by measuring blade surface pressures and the cascade exit flow. High-response pressure transducers were used to measure the unsteady pressure distribution. Inlet-velocity components and turbulence parameters were measured using hot wire. In addition to the synchronous time-averaged pressure spectra, typical power spectra are included for several representative conditions.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleMeasurement of Gust Response on a Turbine Cascade
    typeJournal Paper
    journal volume119
    journal issue2
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2841106
    journal fristpage238
    journal lastpage246
    identifier eissn1528-8900
    keywordsCascades (Fluid dynamics)
    keywordsTurbines
    keywordsPressure
    keywordsFlow (Dynamics)
    keywordsSpectra (Spectroscopy)
    keywordsTurbulence
    keywordsWire
    keywordsPressure transducers
    keywordsMach number AND Blades
    treeJournal of Turbomachinery:;1997:;volume( 119 ):;issue: 002
    contenttypeFulltext
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