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    Aerodynamic Response of Turbomachinery Blade Rows to Convecting Density Wakes

    Source: Journal of Turbomachinery:;2002:;volume( 124 ):;issue: 002::page 269
    Author:
    H. S. Wijesinghe
    ,
    C. S. Tan
    ,
    E. E. Covert
    DOI: 10.1115/1.1311287
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A two-dimensional computational study was conducted to characterize the density wake induced force and moment fluctuations on a compressor blade row. The flow simulations indicate unsteady blade excitation generated by: (1) density wake fluid directed to the blade suction surface, (2) axial deflection of the blade passage shock wave position and (3) formation of a separation bubble on the blade suction surface. The blade force and moment fluctuation amplitudes are found to scale with the nondimensional density wake width w/c and a nondimensional density parameter ρ*.
    keyword(s): Density , Force , Wakes , Blades , Suction , Fluids , Flow (Dynamics) , Separation (Technology) , Shock waves , Fluctuations (Physics) , Compressors AND Turbomachinery ,
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      Aerodynamic Response of Turbomachinery Blade Rows to Convecting Density Wakes

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/127646
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    • Journal of Turbomachinery

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    contributor authorH. S. Wijesinghe
    contributor authorC. S. Tan
    contributor authorE. E. Covert
    date accessioned2017-05-09T00:09:02Z
    date available2017-05-09T00:09:02Z
    date copyrightApril, 2002
    date issued2002
    identifier issn0889-504X
    identifier otherJOTUEI-28695#269_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/127646
    description abstractA two-dimensional computational study was conducted to characterize the density wake induced force and moment fluctuations on a compressor blade row. The flow simulations indicate unsteady blade excitation generated by: (1) density wake fluid directed to the blade suction surface, (2) axial deflection of the blade passage shock wave position and (3) formation of a separation bubble on the blade suction surface. The blade force and moment fluctuation amplitudes are found to scale with the nondimensional density wake width w/c and a nondimensional density parameter ρ*.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleAerodynamic Response of Turbomachinery Blade Rows to Convecting Density Wakes
    typeJournal Paper
    journal volume124
    journal issue2
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.1311287
    journal fristpage269
    journal lastpage274
    identifier eissn1528-8900
    keywordsDensity
    keywordsForce
    keywordsWakes
    keywordsBlades
    keywordsSuction
    keywordsFluids
    keywordsFlow (Dynamics)
    keywordsSeparation (Technology)
    keywordsShock waves
    keywordsFluctuations (Physics)
    keywordsCompressors AND Turbomachinery
    treeJournal of Turbomachinery:;2002:;volume( 124 ):;issue: 002
    contenttypeFulltext
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian
     
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian