Modeling and quantification of acoustic damping induced by vortex shedding in non-compact thermoacoustic systems

Thomas Hofmeister, Tobias Hummel, Bruno Schuermans, Thomas Sattelmayer

Publikation: Beitrag in Buch/Bericht/KonferenzbandKonferenzbeitragBegutachtung

1 Zitat (Scopus)

Abstract

This paper presents a methodology to compute acoustic damping rates of transversal, high-frequency modes induced by vortex-shedding. The acoustic damping rate presents one key quantity for the assessment of the linear thermoacoustic stability of gas turbine combustors. State of the art network models – as employed to calculate damping rates in low-frequency, longitudinal systems – cannot fulfill this task due to the acoustic non-compactness encountered in the high-frequency regime. Furthermore, it is yet unclear, whether direct eigensolutions of the Linearized Euler Equations (LEE), which capture the mechanism of vortex shedding, yield correct damping rate results constituted by the implicit presence of acoustic as well as hydrodynamic contributions in these solutions. The methodology’s applicability to technically relevant systems is demonstrated by a validation test case using a lab-scale, swirl-stabilized combustion system.

OriginalspracheEnglisch
TitelCombustion, Fuels, and Emissions
Herausgeber (Verlag)American Society of Mechanical Engineers (ASME)
ISBN (elektronisch)9780791858615
DOIs
PublikationsstatusVeröffentlicht - 2019
VeranstaltungASME Turbo Expo 2019: Turbomachinery Technical Conference and Exposition, GT 2019 - Phoenix, USA/Vereinigte Staaten
Dauer: 17 Juni 201921 Juni 2019

Publikationsreihe

NameProceedings of the ASME Turbo Expo
Band4A-2019

Konferenz

KonferenzASME Turbo Expo 2019: Turbomachinery Technical Conference and Exposition, GT 2019
Land/GebietUSA/Vereinigte Staaten
OrtPhoenix
Zeitraum17/06/1921/06/19

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