2016
DOI: 10.1016/j.jcp.2016.07.032
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Stability analysis of thermo-acoustic nonlinear eigenproblems in annular combustors. Part I. Sensitivity

Abstract: We present an adjoint-based method for the calculation of eigenvalue perturbations in nonlinear, degenerate and non self-adjoint eigenproblems. This method is applied to a thermo-acoustic annular combustor network, the stability of which is governed by a nonlinear eigenproblem. We calculate the first-and second-order sensitivities of the growth rate and frequency to geometric, flow and flame parameters. Three different configurations are analysed. The benchmark sensitivities are obtained by finite difference, … Show more

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Cited by 32 publications
(52 citation statements)
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References 46 publications
(98 reference statements)
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“…The adjoint sensitivity framework was applied in [162] to thermoacoustic networks, which are used in the preliminary design of aero-engines and gas turbines for power generation. Adjoint methods were developed to accelerate uncertainty quantification of thermoacoustic stability in an annular-combustor network [163] and in a turbulent swirled combustor [164], where first-and second-order corrections for nonlinear degenerate eigenproblems were used [165]. The first implementations of an adjoint Helmholtz solver can be found for a turbulent swirl combustor in [164] and a two-dimensional annular combustor in [166].…”
Section: Thermoacousticsmentioning
confidence: 99%
See 1 more Smart Citation
“…The adjoint sensitivity framework was applied in [162] to thermoacoustic networks, which are used in the preliminary design of aero-engines and gas turbines for power generation. Adjoint methods were developed to accelerate uncertainty quantification of thermoacoustic stability in an annular-combustor network [163] and in a turbulent swirled combustor [164], where first-and second-order corrections for nonlinear degenerate eigenproblems were used [165]. The first implementations of an adjoint Helmholtz solver can be found for a turbulent swirl combustor in [164] and a two-dimensional annular combustor in [166].…”
Section: Thermoacousticsmentioning
confidence: 99%
“…The substitution of the modal decomposition (54) into the governing equations, in general, results in a nonlinear eigenproblem (NEP) [40,163,165], in contrast to most cases in hydrodynamic stability where linear eigenproblems 19 govern the stability. The nonlinear eigenproblem reads…”
Section: Nonlinear Eigenproblemmentioning
confidence: 99%
“…The thermoacoustic stability problem is generally non-Hermitian because of the flame response term and dissipative boundary conditions. On numerical discretization or travelling-wave decomposition [5], thermoacoustic stability is governed by a nonlinear eigenvalue problem [6,7] L(ω; ε)p = 0,…”
Section: Thermoacoustic Instabilitiesmentioning
confidence: 99%
“…On the one hand, eigenvalues of single-flame longitudinal thermoacoustic systems are typically simple [5,8]. On the other hand, systems with discrete rotational symmetry, such as annular and can-annular combustors, feature semi-simple degenerate eigenvalues [6,9], with fewer simple eigenvalues.…”
Section: Eigenvalue Classificationmentioning
confidence: 99%
“…The aim of this paper is to reduce such a computational effort by combining first-and second-order adjoint-based eigenvalue sensitivities (Section 2), detailed in Part I of this paper [16], with a standard Monte Carlo method (Section 3) and a Monte Carlo method integrated with Active Subspace Identification (Section 4) to predict the probabilities that two annular-combustor configurations are unstable.…”
Section: Introductionmentioning
confidence: 99%