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    Acoustic Resonance in Aeroengine Intake Ducts

    Source: Journal of Turbomachinery:;2004:;volume( 126 ):;issue: 003::page 432
    Author:
    A. J. Cooper
    ,
    A. B. Parry
    ,
    N. Peake
    DOI: 10.1115/1.1776586
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A theoretical model is used to investigate the effect of geometry, flow conditions and acoustic lining on the occurrence of acoustic resonance within aeroengine ducts. Semi-analytical methods are used to demonstrate that two types of acoustic resonance can be excited. The first is an intake resonance arising due to axial variation of the intake shape and the presence of swirling flow downstream of the rotor. The second occurs as a result of mode trapping between the rotor and stator. Such resonance phenomena may be relevant to the destabilization of the fan and the onset of flutter and rotating stall.
    keyword(s): Resonance , Flow (Dynamics) , Acoustics , Rotors , Ducts , Stators , Shapes , Waves AND Swirling flow ,
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      Acoustic Resonance in Aeroengine Intake Ducts

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/130981
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    • Journal of Turbomachinery

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    contributor authorA. J. Cooper
    contributor authorA. B. Parry
    contributor authorN. Peake
    date accessioned2017-05-09T00:14:40Z
    date available2017-05-09T00:14:40Z
    date copyrightJuly, 2004
    date issued2004
    identifier issn0889-504X
    identifier otherJOTUEI-28711#432_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/130981
    description abstractA theoretical model is used to investigate the effect of geometry, flow conditions and acoustic lining on the occurrence of acoustic resonance within aeroengine ducts. Semi-analytical methods are used to demonstrate that two types of acoustic resonance can be excited. The first is an intake resonance arising due to axial variation of the intake shape and the presence of swirling flow downstream of the rotor. The second occurs as a result of mode trapping between the rotor and stator. Such resonance phenomena may be relevant to the destabilization of the fan and the onset of flutter and rotating stall.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleAcoustic Resonance in Aeroengine Intake Ducts
    typeJournal Paper
    journal volume126
    journal issue3
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.1776586
    journal fristpage432
    journal lastpage441
    identifier eissn1528-8900
    keywordsResonance
    keywordsFlow (Dynamics)
    keywordsAcoustics
    keywordsRotors
    keywordsDucts
    keywordsStators
    keywordsShapes
    keywordsWaves AND Swirling flow
    treeJournal of Turbomachinery:;2004:;volume( 126 ):;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
    yabeshDSpacePersian