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    Flame Response Mechanisms Due to Velocity Perturbations in a Lean Premixed Gas Turbine Combustor

    Source: Journal of Engineering for Gas Turbines and Power:;2011:;volume( 133 ):;issue: 002::page 21503
    Author:
    Brian Jones
    ,
    Jong Guen Lee
    ,
    Bryan D. Quay
    ,
    Domenic A. Santavicca
    DOI: 10.1115/1.4001996
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The response of turbulent premixed flames to inlet velocity fluctuations is studied experimentally in a lean premixed, swirl-stabilized, gas turbine combustor. Overall chemiluminescence intensity is used as a measure of the fluctuations in the flame’s global heat release rate, and hot wire anemometry is used to measure the inlet velocity fluctuations. Tests are conducted over a range of mean inlet velocities, equivalence ratios, and velocity fluctuation frequencies, while the normalized inlet velocity fluctuation (V′/Vmean) is fixed at 5% to ensure linear flame response over the employed modulation frequency range. The measurements are used to calculate a flame transfer function relating the velocity fluctuation to the heat release fluctuation as a function of the velocity fluctuation frequency. At low frequency, the gain of the flame transfer function increases with increasing frequency to a peak value greater than 1. As the frequency is further increased, the gain decreases to a minimum value, followed by a second smaller peak. The frequencies at which the gain is minimum and achieves its second peak are found to depend on the convection time scale and the flame’s characteristic length scale. Phase-synchronized CH∗ chemiluminescence imaging is used to characterize the flame’s response to inlet velocity fluctuations. The observed flame response can be explained in terms of the interaction of two flame perturbation mechanisms, one originating at flame-anchoring point and propagating along the flame front and the other from vorticity field generated in the outer shear layer in the annular mixing section. An analysis of the phase-synchronized flame images show that when both perturbations arrive at the flame at the same time (or phase), they constructively interfere, producing the second peak observed in the gain curves. When the perturbations arrive at the flame 180 degrees out-of-phase, they destructively interfere, producing the observed minimum in the gain curve.
    keyword(s): Flames , Mechanisms AND Transfer functions ,
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      Flame Response Mechanisms Due to Velocity Perturbations in a Lean Premixed Gas Turbine Combustor

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/146084
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorBrian Jones
    contributor authorJong Guen Lee
    contributor authorBryan D. Quay
    contributor authorDomenic A. Santavicca
    date accessioned2017-05-09T00:43:47Z
    date available2017-05-09T00:43:47Z
    date copyrightFebruary, 2011
    date issued2011
    identifier issn1528-8919
    identifier otherJETPEZ-27155#021503_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/146084
    description abstractThe response of turbulent premixed flames to inlet velocity fluctuations is studied experimentally in a lean premixed, swirl-stabilized, gas turbine combustor. Overall chemiluminescence intensity is used as a measure of the fluctuations in the flame’s global heat release rate, and hot wire anemometry is used to measure the inlet velocity fluctuations. Tests are conducted over a range of mean inlet velocities, equivalence ratios, and velocity fluctuation frequencies, while the normalized inlet velocity fluctuation (V′/Vmean) is fixed at 5% to ensure linear flame response over the employed modulation frequency range. The measurements are used to calculate a flame transfer function relating the velocity fluctuation to the heat release fluctuation as a function of the velocity fluctuation frequency. At low frequency, the gain of the flame transfer function increases with increasing frequency to a peak value greater than 1. As the frequency is further increased, the gain decreases to a minimum value, followed by a second smaller peak. The frequencies at which the gain is minimum and achieves its second peak are found to depend on the convection time scale and the flame’s characteristic length scale. Phase-synchronized CH∗ chemiluminescence imaging is used to characterize the flame’s response to inlet velocity fluctuations. The observed flame response can be explained in terms of the interaction of two flame perturbation mechanisms, one originating at flame-anchoring point and propagating along the flame front and the other from vorticity field generated in the outer shear layer in the annular mixing section. An analysis of the phase-synchronized flame images show that when both perturbations arrive at the flame at the same time (or phase), they constructively interfere, producing the second peak observed in the gain curves. When the perturbations arrive at the flame 180 degrees out-of-phase, they destructively interfere, producing the observed minimum in the gain curve.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleFlame Response Mechanisms Due to Velocity Perturbations in a Lean Premixed Gas Turbine Combustor
    typeJournal Paper
    journal volume133
    journal issue2
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4001996
    journal fristpage21503
    identifier eissn0742-4795
    keywordsFlames
    keywordsMechanisms AND Transfer functions
    treeJournal of Engineering for Gas Turbines and Power:;2011:;volume( 133 ):;issue: 002
    contenttypeFulltext
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