Effect of an azimuthal mean flow on the structure and stability of thermoacoustic modes in an annular combustor model with electroacoustic feedback
| dc.contributor.author | Humbert, Sylvain C. | |
| dc.contributor.author | Moeck, Jonas P. | |
| dc.contributor.author | Orchini, Alessandro | |
| dc.contributor.author | Paschereit, Christian Oliver | |
| dc.date.accessioned | 2022-05-23T13:04:53Z | |
| dc.date.available | 2022-05-23T13:04:53Z | |
| dc.date.issued | 2021-01-11 | |
| dc.description | Copyright © 2020 ASME | en |
| dc.description.abstract | Thermoacoustic oscillations in axisymmetric annular combustors are generally coupled by degenerate azimuthal modes, which can be of standing or spinning nature. Symmetry breaking due to the presence of a mean azimuthal flow splits the degenerate thermoacoustic eigenvalues, resulting in pairs of counter-spinning modes with close but distinct frequencies and growth rates. In the present study, experiments have been performed using an annular system where the thermoacoustic feedback due to the flames is mimicked by twelve identical electroacoustic feedback loops. The mean azimuthal flow is generated by fans. We investigate the standing/spinning nature of the oscillations as a function of the azimuthal Mach number for two types of initial states, and how the stability of the system is affected by the mean azimuthal flow. It is found that spinning, standing or mixed modes can be encountered at very low Mach number, but increas ing the mean velocity promotes one spinning direction. At sufficiently high Mach number, only spinning modes are observed in the limit cycle oscillations. In some cases, the initial conditions have a significant impact on the final state of the system. It is found that the presence of a mean azimuthal flow increases the acoustic damping. This has a beneficial effect on stability: it often reduces the amplitude of the self-sustained oscillations, and can even suppress them in some cases. However, we observe that the suppression of a mode due to the mean flow may destabilize another one. We discuss our findings in relation with an existing low-order model | en |
| dc.description.sponsorship | EC/H2020/765998/EU/Annular Instabilities and Transient Phenomena in Gas Turbine Combustors/ANNULIGhT | en |
| dc.identifier.isbn | 978-0-7918-8413-3 | |
| dc.identifier.uri | https://depositonce.tu-berlin.de/handle/11303/16967 | |
| dc.identifier.uri | http://dx.doi.org/10.14279/depositonce-15746 | |
| dc.language.iso | en | en |
| dc.rights.uri | http://rightsstatements.org/vocab/InC/1.0/ | en |
| dc.subject.ddc | 620 Ingenieurwissenschaften und zugeordnete Tätigkeiten | de |
| dc.subject.other | thermoacoustic oscillations | en |
| dc.subject.other | electroacoustic feedback | en |
| dc.subject.other | annular combustor | en |
| dc.subject.other | azimuthal mean flow | en |
| dc.subject.other | acoustic damping | en |
| dc.title | Effect of an azimuthal mean flow on the structure and stability of thermoacoustic modes in an annular combustor model with electroacoustic feedback | en |
| dc.type | Conference Object | en |
| dc.type.version | publishedVersion | en |
| dcterms.bibliographicCitation.doi | 10.1115/GT2020-16091 | en |
| dcterms.bibliographicCitation.originalpublishername | ASME | en |
| dcterms.bibliographicCitation.originalpublisherplace | New York, NY | en |
| dcterms.bibliographicCitation.proceedingstitle | ASME Turbo Expo 2020: Turbomachinery Technical Conference and Exposition | en |
| tub.accessrights.dnb | free | en |
| tub.affiliation | Fak. 5 Verkehrs- und Maschinensysteme::Inst. Strömungsmechanik und Technische Akustik (ISTA)::FG Experimentelle Strömungsmechanik | de |
| tub.affiliation.faculty | Fak. 5 Verkehrs- und Maschinensysteme | de |
| tub.affiliation.group | FG Experimentelle Strömungsmechanik | de |
| tub.affiliation.institute | Inst. Strömungsmechanik und Technische Akustik (ISTA) | de |
| tub.publisher.universityorinstitution | Technische Universität Berlin | en |