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Uncertainty quantification of growth rates of thermoacoustic instability by an adjoint Helmholtz solver

Accepted version
Peer-reviewed

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Type

Article

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Authors

Silva, CF 
Runte, T 
Polifke, W 

Abstract

Thermoacoustic instabilities are often calculated with Helmholtz solvers combined with a low-order model for the flame dynamics. Typically, such a formulation leads to an eigenvalue problem in which the eigenvalue appears under nonlinear terms, such as exponentials related to the time delays that result from the flame model. The objective of the present paper is to quantify uncertainties in thermoacoustic stability analysis with a Helmholtz solver and its adjoint. This approach is applied to the model of a combustion test rig with a premixed swirl burner. The nonlinear eigenvalue problem and its adjoint are solved by an in-house adjoint Helmholtz solver, based on an axisymmetric finite-volume discretization. In addition to first-order correction terms of the adjoint formulation, as they are often used in the literature, second-order terms are also taken into account. It is found that one particular second-order term has significant impact on the accuracy of the predictions. Finally, the probability density function (PDF) of the growth rate in the presence of uncertainties in the input parameters is calculated with a Monte Carlo approach. The uncertainties considered concern the gain and phase of the flame response, the outlet acoustic reflection coefficient, and the plenum geometry. It is found that the second-order adjoint method gives quantitative agreement with results based on the full nonlinear eigenvalue problem, while requiring much fewer computations.

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Keywords

40 Engineering, 4017 Mechanical Engineering, 4002 Automotive Engineering

Journal Title

Journal of Engineering for Gas Turbines and Power

Conference Name

Journal ISSN

0742-4795
1528-8919

Volume Title

139

Publisher

The American Society of Mechanical Engineers
Sponsorship
Technological foundations for the design of thermally and mechanically highly loaded components of future space transportation systems (SFB TR40), Royal Academy of Engineering Research Fellowships Scheme