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    Aeroelastic Characteristics of a Cascade of Mistuned Blades in Subsonic and Supersonic Flows

    Source: Journal of Vibration and Acoustics:;1983:;volume( 105 ):;issue: 004::page 425
    Author:
    R. E. Kielb
    ,
    K. R. V. Kaza
    DOI: 10.1115/1.3269124
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An investigation of the effects of mistuning on flutter and forced response of a cascade in subsonic and supersonic flows is presented. The aerodynamic and structural coupling between the bending and torsional motions and the aerodynamic coupling between the blades are included. It is shown that frequency mistuning always has a beneficial effect on flutter. Additionally, the results indicate that frequency mistuning may have either a beneficial or an adverse effect on forced response, depending on the engine order of the excitation and Mach number.
    keyword(s): Cascades (Fluid dynamics) , Blades , Supersonic flow , Flutter (Aerodynamics) , Mach number , Motion AND Engines ,
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      Aeroelastic Characteristics of a Cascade of Mistuned Blades in Subsonic and Supersonic Flows

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/97802
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    • Journal of Vibration and Acoustics

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    contributor authorR. E. Kielb
    contributor authorK. R. V. Kaza
    date accessioned2017-05-08T23:16:45Z
    date available2017-05-08T23:16:45Z
    date copyrightOctober, 1983
    date issued1983
    identifier issn1048-9002
    identifier otherJVACEK-28959#425_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/97802
    description abstractAn investigation of the effects of mistuning on flutter and forced response of a cascade in subsonic and supersonic flows is presented. The aerodynamic and structural coupling between the bending and torsional motions and the aerodynamic coupling between the blades are included. It is shown that frequency mistuning always has a beneficial effect on flutter. Additionally, the results indicate that frequency mistuning may have either a beneficial or an adverse effect on forced response, depending on the engine order of the excitation and Mach number.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleAeroelastic Characteristics of a Cascade of Mistuned Blades in Subsonic and Supersonic Flows
    typeJournal Paper
    journal volume105
    journal issue4
    journal titleJournal of Vibration and Acoustics
    identifier doi10.1115/1.3269124
    journal fristpage425
    journal lastpage433
    identifier eissn1528-8927
    keywordsCascades (Fluid dynamics)
    keywordsBlades
    keywordsSupersonic flow
    keywordsFlutter (Aerodynamics)
    keywordsMach number
    keywordsMotion AND Engines
    treeJournal of Vibration and Acoustics:;1983:;volume( 105 ):;issue: 004
    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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