Tracking of acoustic and intrinsic modes for thermoacoustic systems with a general flame model

被引:0
作者
Orchini, Alessandro [1 ]
Cronqvist, Frida [2 ]
von Saldern, Jakob G. R. [3 ]
Humbert, Sylvain C. [4 ]
Moeck, Jonas [2 ]
机构
[1] TU Berlin, Chair Nonlinear Thermo Fluid Mech, ISTA, Berlin, Germany
[2] NTNU Trondheim, Dept Energy & Proc Engn, Trondheim, Norway
[3] TU Berlin, Lab Flow Instabil & Dynam, ISTA, Berlin, Germany
[4] TU Berlin, Chair Expt Fluid Dynam, ISTA, Berlin, Germany
关键词
Combustion dynamics; Thermoacoustic oscillations; Flame response; Intrinsic modes; Eigenvalue tracking; INSTABILITIES; OSCILLATIONS; COMBUSTORS;
D O I
10.1016/j.combustflame.2025.113998
中图分类号
O414.1 [热力学];
学科分类号
摘要
Ina thermoacoustic feedback loop, the flame gain parameter can be used to measure the coupling strength between the acoustic field and the flame response. In this study, it is shown for an arbitrary flame model that the thermoacoustic solutions in the zero-coupling limit split into two distinct sets: modes of (i) acoustic and (ii) intrinsic (ITA) origin. This result was previously shown in a rigorous manner only for n-tau flame models, which are special in the sense that they have ITA poles only at infinity. Consequently, all thermoacoustic eigenvalues can generally be calculated from the acoustic and intrinsic poles using continuation methods. In this study, we provide an explicit eigenvalue tracking scheme based on the integration of the local eigenvalue sensitivity to the flame gain parameter. The initial conditions required for integration are considered in detail. While the acoustic poles can be determined directly via Helmholtz solvers, the intrinsic poles are less trivial since they depend on the flame model. An asymptotic expansion of a generic transfer function is derived that is representative of all common flame models. It provides the necessary estimates for the intrinsic poles as the flame gain approaches zero in terms of the Lambert W function. This approach represents an explicit scheme that guarantees to find all thermoacoustic eigenvalues. The methodology is demonstrated using a simple Rijke tube network model and an experimentally determined state-space model of an annular setup.
引用
收藏
页数:11
相关论文
共 38 条
  • [1] Thermal versus acoustic response of velocity sensitive premixed flames
    Bomberg, S.
    Emmert, T.
    Polifke, W.
    [J]. PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2015, 35 : 3185 - 3192
  • [2] Intrinsic thermoacoustic modes in an annular combustion chamber
    Buschmann, Philip E.
    Mensah, Georg A.
    Moeck, Jonas P.
    [J]. COMBUSTION AND FLAME, 2020, 214 : 251 - 262
  • [3] Solution of Thermoacoustic Eigenvalue Problems With a Noniterative Method
    Buschmann, Philip E.
    Mensah, Georg A.
    Nicoud, Franck
    Moeck, Jonas P.
    [J]. JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 2020, 142 (03):
  • [4] Combustion dynamics and control: Progress and challenges
    Candel, S
    [J]. PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2002, 29 (01) : 1 - 28
  • [5] Analytical stability bound for delayed second-order systems with repeating poles using Lambert function W
    Chen, YQ
    Moore, KL
    [J]. AUTOMATICA, 2002, 38 (05) : 891 - 895
  • [6] On the Lambert W function
    Corless, RM
    Gonnet, GH
    Hare, DEG
    Jeffrey, DJ
    Knuth, DE
    [J]. ADVANCES IN COMPUTATIONAL MATHEMATICS, 1996, 5 (04) : 329 - 359
  • [7] Crocco L., 1965, 10 S INT COMBUSTION, P1101, DOI [10.1016/S0082-0784(65)80249-1, DOI 10.1016/S0082-0784(65)80249-1]
  • [8] Culick F.E.C., 2006, RTO AG-AVT-039, P664
  • [9] Acoustic analysis of gas turbine combustors
    Dowling, AP
    Stow, SR
    [J]. JOURNAL OF PROPULSION AND POWER, 2003, 19 (05) : 751 - 764
  • [10] Nonlinear self-excited oscillations of a ducted flame
    Dowling, AP
    [J]. JOURNAL OF FLUID MECHANICS, 1997, 346 : 271 - 290