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    Application of the Perforated Plate in Passive Control of the Nonpremixed Swirl Combustion Instability Under Acoustic Excitation

    Source: Journal of Engineering for Gas Turbines and Power:;2019:;volume( 141 ):;issue: 009::page 91007
    Author:
    Meng, Sheng
    ,
    Zhou, Hao
    ,
    Cen, Kefa
    DOI: 10.1115/1.4043848
    Publisher: American Society of Mechanical Engineers (ASME)
    Abstract: Perforated plates are widely used to attenuate noise emission and as acoustic liners in combustion chambers. In this study, the damping performance of the perforated plate located in the combustor inlet section is experimentally and numerically studied. The primary response of nonpremixed swirl flame under 30–400 Hz acoustic excitation with a 445 mm inlet length occurs at 134 Hz and 210 Hz modes. The perforated plate designed for 210 Hz sound absorption with a 328 mm cavity length and an 8.04% porosity is compared to plates with various cavity lengths and different orifice patterns. The acoustic absorption capability of perforated plates is evaluated by the Luong model and tested in an impedance tube. The acoustic measurements show that the sound absorption performance of each plate is strongly affected by the bias flow velocity and cavity length. The combustion results indicate that the installation of perforated plates at the inlet section has two effects: sound attenuation and redistribution of the pressure mode of the combustor. The acoustic mode analysis further demonstrated that, for damping the nonpremixed flame when the combustion instability is caused by the inlet pressure fluctuation, modification of the inlet acoustic mode shape is more efficient than the sound attenuation.
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      Application of the Perforated Plate in Passive Control of the Nonpremixed Swirl Combustion Instability Under Acoustic Excitation

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/4258140
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorMeng, Sheng
    contributor authorZhou, Hao
    contributor authorCen, Kefa
    date accessioned2019-09-18T09:02:20Z
    date available2019-09-18T09:02:20Z
    date copyright6/5/2019 12:00:00 AM
    date issued2019
    identifier issn0742-4795
    identifier othergtp_141_09_091007
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4258140
    description abstractPerforated plates are widely used to attenuate noise emission and as acoustic liners in combustion chambers. In this study, the damping performance of the perforated plate located in the combustor inlet section is experimentally and numerically studied. The primary response of nonpremixed swirl flame under 30–400 Hz acoustic excitation with a 445 mm inlet length occurs at 134 Hz and 210 Hz modes. The perforated plate designed for 210 Hz sound absorption with a 328 mm cavity length and an 8.04% porosity is compared to plates with various cavity lengths and different orifice patterns. The acoustic absorption capability of perforated plates is evaluated by the Luong model and tested in an impedance tube. The acoustic measurements show that the sound absorption performance of each plate is strongly affected by the bias flow velocity and cavity length. The combustion results indicate that the installation of perforated plates at the inlet section has two effects: sound attenuation and redistribution of the pressure mode of the combustor. The acoustic mode analysis further demonstrated that, for damping the nonpremixed flame when the combustion instability is caused by the inlet pressure fluctuation, modification of the inlet acoustic mode shape is more efficient than the sound attenuation.
    publisherAmerican Society of Mechanical Engineers (ASME)
    titleApplication of the Perforated Plate in Passive Control of the Nonpremixed Swirl Combustion Instability Under Acoustic Excitation
    typeJournal Paper
    journal volume141
    journal issue9
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4043848
    journal fristpage91007
    journal lastpage091007-12
    treeJournal of Engineering for Gas Turbines and Power:;2019:;volume( 141 ):;issue: 009
    contenttypeFulltext
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