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    Instability of a Premix Burner With Nonmonotonic Pressure Drop Characteristic

    Source: Journal of Engineering for Gas Turbines and Power:;2003:;volume( 125 ):;issue: 001::page 20
    Author:
    W. Polifke
    ,
    A. Fischer
    ,
    T. Sattelmayer
    DOI: 10.1115/1.1519267
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Instabilities in combustion systems have frequently been reported to occur when slight changes in operating conditions lead to significant and abrupt changes in flame shape or flame position, i.e., changes in the mode of flame stabilization. The present paper offers an explanation and mathematical model of this observation. The analysis rests on the assumption that changes in the mode of flame stabilization are accompanied by a significant variation of the pressure drop across burner and flame, such that the pressure drop-flow rate characteristic locally displays a negative slope. In the limit of low frequencies (Helmholtz mode), it is then straightforward to show that an oscillatory instability can result from such behavior. An analytical stability criterion is derived, relating the nondimensionalized gradient of the pressure drop characteristic to the Helmholtz number of the burner. The physical mechanism of the instability is explained, and it is observed that the Rayleigh criterion need not be satisfied for this kind of instability to occur. In order to extend the stability analysis to higher frequencies, the transfer matrix for a burner with nonmonotonic pressure drop is derived in the limit of low Mach number and negligible fluctuations of the rate of heat release. The transfer matrix is employed in stability analysis based on a linear acoustic model of a combustion system. Experimental results obtained with an externally premixed swirl burner are presented. The pressure drop characteristic, the observed onset of instability and the instability frequency match the model predictions very well.
    keyword(s): Pressure , Stability , Flow (Dynamics) , Acoustics , Combustion chambers , Flames , Pressure drop , Mechanisms , Fluctuations (Physics) , Combustion systems , Heat AND Nozzles ,
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      Instability of a Premix Burner With Nonmonotonic Pressure Drop Characteristic

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    http://yetl.yabesh.ir/yetl1/handle/yetl/128406
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorW. Polifke
    contributor authorA. Fischer
    contributor authorT. Sattelmayer
    date accessioned2017-05-09T00:10:16Z
    date available2017-05-09T00:10:16Z
    date copyrightJanuary, 2003
    date issued2003
    identifier issn1528-8919
    identifier otherJETPEZ-26819#20_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/128406
    description abstractInstabilities in combustion systems have frequently been reported to occur when slight changes in operating conditions lead to significant and abrupt changes in flame shape or flame position, i.e., changes in the mode of flame stabilization. The present paper offers an explanation and mathematical model of this observation. The analysis rests on the assumption that changes in the mode of flame stabilization are accompanied by a significant variation of the pressure drop across burner and flame, such that the pressure drop-flow rate characteristic locally displays a negative slope. In the limit of low frequencies (Helmholtz mode), it is then straightforward to show that an oscillatory instability can result from such behavior. An analytical stability criterion is derived, relating the nondimensionalized gradient of the pressure drop characteristic to the Helmholtz number of the burner. The physical mechanism of the instability is explained, and it is observed that the Rayleigh criterion need not be satisfied for this kind of instability to occur. In order to extend the stability analysis to higher frequencies, the transfer matrix for a burner with nonmonotonic pressure drop is derived in the limit of low Mach number and negligible fluctuations of the rate of heat release. The transfer matrix is employed in stability analysis based on a linear acoustic model of a combustion system. Experimental results obtained with an externally premixed swirl burner are presented. The pressure drop characteristic, the observed onset of instability and the instability frequency match the model predictions very well.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleInstability of a Premix Burner With Nonmonotonic Pressure Drop Characteristic
    typeJournal Paper
    journal volume125
    journal issue1
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.1519267
    journal fristpage20
    journal lastpage27
    identifier eissn0742-4795
    keywordsPressure
    keywordsStability
    keywordsFlow (Dynamics)
    keywordsAcoustics
    keywordsCombustion chambers
    keywordsFlames
    keywordsPressure drop
    keywordsMechanisms
    keywordsFluctuations (Physics)
    keywordsCombustion systems
    keywordsHeat AND Nozzles
    treeJournal of Engineering for Gas Turbines and Power:;2003:;volume( 125 ):;issue: 001
    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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