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    The Effect of Vane Clocking on the Unsteady Flow Field in a One-and-a-Half Stage Transonic Turbine

    Source: Journal of Turbomachinery:;2008:;volume( 130 ):;issue: 003::page 31022
    Author:
    B. Paradiso
    ,
    E. Göttlich
    ,
    O. Schennach
    ,
    R. Pecnik
    ,
    A. Marn
    ,
    J. Woisetschläger
    DOI: 10.1115/1.2777199
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The current paper presents the results of numerical and experimental clocking investigations performed in a high-pressure transonic turbine with a downstream vane row. The objective was a detailed analysis of shock and wake interactions in such a 1.5-stage machine while clocking the vanes. Therefore, a transient 3D Navier–Stokes calculation was done for two clocking positions, and the three-dimensional results are compared with laser-Doppler-velocimetry measurements at midspan. Additionally, the second vane was equipped with fast response pressure transducers to record the instantaneous surface pressure for 20 different clocking positions at midspan.
    keyword(s): Pressure , Flow (Dynamics) , Wakes , Shock (Mechanics) , Rotors , Turbines , Laser Doppler anemometry , Blades , Suction , Measurement , Unsteady flow , Fluctuations (Physics) AND Light trucks ,
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      The Effect of Vane Clocking on the Unsteady Flow Field in a One-and-a-Half Stage Transonic Turbine

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/139496
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    • Journal of Turbomachinery

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    contributor authorB. Paradiso
    contributor authorE. Göttlich
    contributor authorO. Schennach
    contributor authorR. Pecnik
    contributor authorA. Marn
    contributor authorJ. Woisetschläger
    date accessioned2017-05-09T00:30:48Z
    date available2017-05-09T00:30:48Z
    date copyrightJuly, 2008
    date issued2008
    identifier issn0889-504X
    identifier otherJOTUEI-28748#031022_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/139496
    description abstractThe current paper presents the results of numerical and experimental clocking investigations performed in a high-pressure transonic turbine with a downstream vane row. The objective was a detailed analysis of shock and wake interactions in such a 1.5-stage machine while clocking the vanes. Therefore, a transient 3D Navier–Stokes calculation was done for two clocking positions, and the three-dimensional results are compared with laser-Doppler-velocimetry measurements at midspan. Additionally, the second vane was equipped with fast response pressure transducers to record the instantaneous surface pressure for 20 different clocking positions at midspan.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleThe Effect of Vane Clocking on the Unsteady Flow Field in a One-and-a-Half Stage Transonic Turbine
    typeJournal Paper
    journal volume130
    journal issue3
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2777199
    journal fristpage31022
    identifier eissn1528-8900
    keywordsPressure
    keywordsFlow (Dynamics)
    keywordsWakes
    keywordsShock (Mechanics)
    keywordsRotors
    keywordsTurbines
    keywordsLaser Doppler anemometry
    keywordsBlades
    keywordsSuction
    keywordsMeasurement
    keywordsUnsteady flow
    keywordsFluctuations (Physics) AND Light trucks
    treeJournal of Turbomachinery:;2008:;volume( 130 ):;issue: 003
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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