YaBeSH Engineering and Technology Library

    • Journals
    • PaperQuest
    • YSE Standards
    • YaBeSH
    • Login
    View Item 
    •   YE&T Library
    • ASME
    • Journal of Engineering for Gas Turbines and Power
    • View Item
    •   YE&T Library
    • ASME
    • Journal of Engineering for Gas Turbines and Power
    • View Item
    • All Fields
    • Source Title
    • Year
    • Publisher
    • Title
    • Subject
    • Author
    • DOI
    • ISBN
    Advanced Search
    JavaScript is disabled for your browser. Some features of this site may not work without it.

    Archive

    Spatiotemporal Characterization of a Conical Swirler Flow Field Under Strong Forcing

    Source: Journal of Engineering for Gas Turbines and Power:;2009:;volume( 131 ):;issue: 003::page 31504
    Author:
    D. Greenblatt
    ,
    C. O. Paschereit
    ,
    A. Lacarelle
    ,
    T. Faustmann
    ,
    O. Lehmann
    ,
    D. M. Luchtenburg
    ,
    B. R. Noack
    DOI: 10.1115/1.2982139
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In this study, a spatiotemporal characterization of forced and unforced flows of a conical swirler is performed based on particle image velocimetry (PIV) and laser Doppler anemometry (LDA). The measurements are performed at a Reynolds number of 33,000 and a swirl number of 0.71. Axisymmetric forcing is applied to approximate the effects of thermoacoustic instabilities on the flow field at the burner inlet and outlet. The actuation frequencies are set at the natural flow frequency (Strouhal number Stf≈0.92) and two higher frequencies (Stf≈1.3 and 1.55) that are not harmonically related to the natural frequency. Phase-averaged measurement are used as a first step to visualize the coherent flow structures. Second, proper orthogonal decomposition (POD) is applied to the PIV data to characterize the effect of the actuation on the fluctuating flow. Measurements indicate a typical natural flow instability of helical nature in the unforced case. The associated induced pressure and flow oscillations travel upstream to the swirler inlet where generally fuel is injected. This observation is of critical importance with respect to the stability of the combustion. Harmonic actuation at different frequencies and amplitudes does not affect the mean velocity profile at the outlet, while the coherent velocity fluctuations are strongly influenced at both the inlet and outlet. On one hand, the dominant helical mode is replaced by an axisymmetric vortex ring if the flow is forced at the natural flow frequency. On the other hand, the natural flow frequency prevails at the outlet under forcing at higher frequencies and POD analysis indicates that the helical structure is still present. The presented results give new insight into the flow dynamics of a swirling flow burner under strong forcing.
    keyword(s): Flow (Dynamics) AND Oscillations ,
    • Download: (2.127Mb)
    • Show Full MetaData Hide Full MetaData
    • Get RIS
    • Item Order
    • Go To Publisher
    • Price: 5000 Rial
    • Statistics

      Spatiotemporal Characterization of a Conical Swirler Flow Field Under Strong Forcing

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/140459
    Collections
    • Journal of Engineering for Gas Turbines and Power

    Show full item record

    contributor authorD. Greenblatt
    contributor authorC. O. Paschereit
    contributor authorA. Lacarelle
    contributor authorT. Faustmann
    contributor authorO. Lehmann
    contributor authorD. M. Luchtenburg
    contributor authorB. R. Noack
    date accessioned2017-05-09T00:32:40Z
    date available2017-05-09T00:32:40Z
    date copyrightMay, 2009
    date issued2009
    identifier issn1528-8919
    identifier otherJETPEZ-27066#031504_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/140459
    description abstractIn this study, a spatiotemporal characterization of forced and unforced flows of a conical swirler is performed based on particle image velocimetry (PIV) and laser Doppler anemometry (LDA). The measurements are performed at a Reynolds number of 33,000 and a swirl number of 0.71. Axisymmetric forcing is applied to approximate the effects of thermoacoustic instabilities on the flow field at the burner inlet and outlet. The actuation frequencies are set at the natural flow frequency (Strouhal number Stf≈0.92) and two higher frequencies (Stf≈1.3 and 1.55) that are not harmonically related to the natural frequency. Phase-averaged measurement are used as a first step to visualize the coherent flow structures. Second, proper orthogonal decomposition (POD) is applied to the PIV data to characterize the effect of the actuation on the fluctuating flow. Measurements indicate a typical natural flow instability of helical nature in the unforced case. The associated induced pressure and flow oscillations travel upstream to the swirler inlet where generally fuel is injected. This observation is of critical importance with respect to the stability of the combustion. Harmonic actuation at different frequencies and amplitudes does not affect the mean velocity profile at the outlet, while the coherent velocity fluctuations are strongly influenced at both the inlet and outlet. On one hand, the dominant helical mode is replaced by an axisymmetric vortex ring if the flow is forced at the natural flow frequency. On the other hand, the natural flow frequency prevails at the outlet under forcing at higher frequencies and POD analysis indicates that the helical structure is still present. The presented results give new insight into the flow dynamics of a swirling flow burner under strong forcing.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleSpatiotemporal Characterization of a Conical Swirler Flow Field Under Strong Forcing
    typeJournal Paper
    journal volume131
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2982139
    journal fristpage31504
    identifier eissn0742-4795
    keywordsFlow (Dynamics) AND Oscillations
    treeJournal of Engineering for Gas Turbines and Power:;2009:;volume( 131 ):;issue: 003
    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