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    Flashback in Lean Prevaporized Premixed Combustion: Nonswirling Turbulent Pipe Flow Study

    Source: Journal of Engineering for Gas Turbines and Power:;2003:;volume( 125 ):;issue: 003::page 670
    Author:
    O. Schäfer
    ,
    R. Koch
    ,
    S. Wittig
    DOI: 10.1115/1.1581897
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A fundamental study has been performed on the upstream flame propagation of a turbulent kerosene flame, stabilized in a confined stagnation flow at atmospheric pressure. Besides temperature and equivalence ratio, mixture properties and fluid dynamic parameters have been varied. The flashback phenomenon is discussed in terms of critical mean velocities and additionally based on detailed LDV data at the outlet of the premixing duct. The largest critical velocities uc for flashback are found for the “perfectly” premixed case and equivalence ratios close to stoichiometric, which is in accordance with the theory on laminar flame propagation. In the case of a homogeneous mixture, flashback is determined by the velocity distribution at the outlet of the premixing section. In the undisturbed pipe flow the flame propagates through the wall boundary layer. The data for this case are compared with the theory of side-wall quenching in terms of a critical Peclet number and critical velocity gradients at the wall. Both are deduced from the experimental data. Reducing the velocity on the axis forces the flame to propagate through the center at a velocity predicted by correlations on turbulent flame velocity.
    keyword(s): Flow (Dynamics) , Combustion , Turbulence , Pipe flow , Flames , Combustion chambers , Mixtures , Temperature , Boundary layers , Fuels , Gradients AND Ducts ,
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      Flashback in Lean Prevaporized Premixed Combustion: Nonswirling Turbulent Pipe Flow Study

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    http://yetl.yabesh.ir/yetl1/handle/yetl/128346
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorO. Schäfer
    contributor authorR. Koch
    contributor authorS. Wittig
    date accessioned2017-05-09T00:10:07Z
    date available2017-05-09T00:10:07Z
    date copyrightJuly, 2003
    date issued2003
    identifier issn1528-8919
    identifier otherJETPEZ-26823#670_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/128346
    description abstractA fundamental study has been performed on the upstream flame propagation of a turbulent kerosene flame, stabilized in a confined stagnation flow at atmospheric pressure. Besides temperature and equivalence ratio, mixture properties and fluid dynamic parameters have been varied. The flashback phenomenon is discussed in terms of critical mean velocities and additionally based on detailed LDV data at the outlet of the premixing duct. The largest critical velocities uc for flashback are found for the “perfectly” premixed case and equivalence ratios close to stoichiometric, which is in accordance with the theory on laminar flame propagation. In the case of a homogeneous mixture, flashback is determined by the velocity distribution at the outlet of the premixing section. In the undisturbed pipe flow the flame propagates through the wall boundary layer. The data for this case are compared with the theory of side-wall quenching in terms of a critical Peclet number and critical velocity gradients at the wall. Both are deduced from the experimental data. Reducing the velocity on the axis forces the flame to propagate through the center at a velocity predicted by correlations on turbulent flame velocity.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleFlashback in Lean Prevaporized Premixed Combustion: Nonswirling Turbulent Pipe Flow Study
    typeJournal Paper
    journal volume125
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.1581897
    journal fristpage670
    journal lastpage676
    identifier eissn0742-4795
    keywordsFlow (Dynamics)
    keywordsCombustion
    keywordsTurbulence
    keywordsPipe flow
    keywordsFlames
    keywordsCombustion chambers
    keywordsMixtures
    keywordsTemperature
    keywordsBoundary layers
    keywordsFuels
    keywordsGradients AND Ducts
    treeJournal of Engineering for Gas Turbines and Power:;2003:;volume( 125 ):;issue: 003
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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