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    Nonlinear Phenomena in Thermoacoustic Systems With Premixed Flames

    Source: Journal of Engineering for Gas Turbines and Power:;2013:;volume( 135 ):;issue: 006::page 61502
    Author:
    Kashinath, Karthik
    ,
    Hemchandra, Santosh
    ,
    Juniper, Matthew P.
    DOI: 10.1115/1.4023305
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Nonlinear analysis of thermoacoustic instability is essential for the prediction of the frequencies, amplitudes, and stability of limit cycles. Limit cycles in thermoacoustic systems are reached when the energy input from driving processes and energy losses from damping processes balance each other over a cycle of the oscillation. In this paper, an integral relation for the rate of change of energy of a thermoacoustic system is derived. This relation is analogous to the wellknown Rayleigh criterion in thermoacoustics, however, it can be used to calculate the amplitudes of limit cycles and their stability. The relation is applied to a thermoacoustic system of a ducted slotstabilized 2D premixed flame. The flame is modeled using a nonlinear kinematic model based on the Gequation, while the acoustics of planar waves in the tube are governed by linearized momentum and energy equations. Using openloop forced simulations, the flame describing function (FDF) is calculated. The gain and phase information from the FDF is used with the integral relation to construct a cyclic integral rate of change of energy (CIRCE) diagram that indicates the amplitude and stability of limit cycles. This diagram is also used to identify the types of bifurcation the system exhibits and to find the minimum amplitude of excitation needed to reach a stable limit cycle from another linearly stable state for singlemode thermoacoustic systems. Furthermore, this diagram shows precisely how the choice of velocity model and the amplitudedependence of the gain and the phase of the FDF influence the nonlinear dynamics of the system. Time domain simulations of the coupled thermoacoustic system are performed with a Galerkin discretization for acoustic pressure and velocity. Limit cycle calculations using a single mode, along with twenty modes, are compared against predictions from the CIRCE diagram. For the single mode system, the time domain calculations agree well with the frequency domain predictions. The heat release rate is highly nonlinear but, because there is only a single acoustic mode, this does not affect the limit cycle amplitude. For the twentymode system, however, the higher harmonics of the heat release rate and acoustic velocity interact, resulting in a larger limit cycle amplitude. Multimode simulations show that, in some situations, the contribution from higher harmonics to the nonlinear dynamics can be significant and must be considered for an accurate and comprehensive analysis of thermoacoustic systems.
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      Nonlinear Phenomena in Thermoacoustic Systems With Premixed Flames

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    http://yetl.yabesh.ir/yetl1/handle/yetl/151620
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    contributor authorKashinath, Karthik
    contributor authorHemchandra, Santosh
    contributor authorJuniper, Matthew P.
    date accessioned2017-05-09T00:58:17Z
    date available2017-05-09T00:58:17Z
    date issued2013
    identifier issn1528-8919
    identifier othergtp_135_6_061502.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/151620
    description abstractNonlinear analysis of thermoacoustic instability is essential for the prediction of the frequencies, amplitudes, and stability of limit cycles. Limit cycles in thermoacoustic systems are reached when the energy input from driving processes and energy losses from damping processes balance each other over a cycle of the oscillation. In this paper, an integral relation for the rate of change of energy of a thermoacoustic system is derived. This relation is analogous to the wellknown Rayleigh criterion in thermoacoustics, however, it can be used to calculate the amplitudes of limit cycles and their stability. The relation is applied to a thermoacoustic system of a ducted slotstabilized 2D premixed flame. The flame is modeled using a nonlinear kinematic model based on the Gequation, while the acoustics of planar waves in the tube are governed by linearized momentum and energy equations. Using openloop forced simulations, the flame describing function (FDF) is calculated. The gain and phase information from the FDF is used with the integral relation to construct a cyclic integral rate of change of energy (CIRCE) diagram that indicates the amplitude and stability of limit cycles. This diagram is also used to identify the types of bifurcation the system exhibits and to find the minimum amplitude of excitation needed to reach a stable limit cycle from another linearly stable state for singlemode thermoacoustic systems. Furthermore, this diagram shows precisely how the choice of velocity model and the amplitudedependence of the gain and the phase of the FDF influence the nonlinear dynamics of the system. Time domain simulations of the coupled thermoacoustic system are performed with a Galerkin discretization for acoustic pressure and velocity. Limit cycle calculations using a single mode, along with twenty modes, are compared against predictions from the CIRCE diagram. For the single mode system, the time domain calculations agree well with the frequency domain predictions. The heat release rate is highly nonlinear but, because there is only a single acoustic mode, this does not affect the limit cycle amplitude. For the twentymode system, however, the higher harmonics of the heat release rate and acoustic velocity interact, resulting in a larger limit cycle amplitude. Multimode simulations show that, in some situations, the contribution from higher harmonics to the nonlinear dynamics can be significant and must be considered for an accurate and comprehensive analysis of thermoacoustic systems.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleNonlinear Phenomena in Thermoacoustic Systems With Premixed Flames
    typeJournal Paper
    journal volume135
    journal issue6
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4023305
    journal fristpage61502
    journal lastpage61502
    identifier eissn0742-4795
    treeJournal of Engineering for Gas Turbines and Power:;2013:;volume( 135 ):;issue: 006
    contenttypeFulltext
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