Numerical prediction of thermoacoustic instabilities in a three-dimensional combustor model
2019 (English)In: 25th AIAA/CEAS Aeroacoustics Conference, 2019, American Institute of Aeronautics and Astronautics Inc, AIAA , 2019Conference paper, Published paper (Refereed)
Abstract [en]
In this paper, the numerical work focus on prediction of the thermoacoustic instabilities for a three-dimensional combustor model. A numerical methodology solving the Helmholtz equation with the Flame Describing Function (FDF) in frequency domain is used. In the present numerical work, the in-house numerical code is first examined by the Ri-jke tube benchmark case with the planar flame in a variation of n and τ in one-dimensional n-τ model. Afterwards, the numerical work is extended to simulate the thermoacoustic instabilities of a three-dimensional combustor. The experimental determined FDF is applied in the simulations, which takes into account the non-linear behavior of the flame. In the paper, the eigenfrequencies of the system are presented as numerical results, which are compared with the experimental data.
Place, publisher, year, edition, pages
American Institute of Aeronautics and Astronautics Inc, AIAA , 2019.
Keywords [en]
Aeroacoustics, Combustors, Frequency domain analysis, Thermoacoustics, Combustor modeling, Eigen frequencies, Flame describing functions, Nonlinear behavior, Numerical methodologies, Numerical predictions, Numerical results, Thermoacoustic instability, Numerical models
National Category
Fluid Mechanics Energy Engineering
Identifiers
URN: urn:nbn:se:kth:diva-274833DOI: 10.2514/6.2019-2738Scopus ID: 2-s2.0-85095970611OAI: oai:DiVA.org:kth-274833DiVA, id: diva2:1444771
Conference
25th AIAA/CEAS Aeroacoustics Conference, 2019, 20-23 May 2019, Delft, Netherlands
Note
QC 20200622
Part of ISBN 9781624105883
2020-06-222020-06-222025-02-09Bibliographically approved