Spinning and azimuthally standing acoustic modes in annular combustors

S. Evesque, W. Polifke, C. Pankiewitz

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

53 Scopus citations

Abstract

Damaging combustion instabilities can occur in annular combustors used in low NOx stationary gas turbines. Both spinning and azimuthally standing oscillations have been observed, without a real understanding of the causes of such mode selection. This paper proposes a new quantitative measure, called the spin-ratio, to describe the spinning tendency of an acoustic mode. The spin-ratio is based on an acoustic energy density formulation, in which the acoustic field in the annular combustor is described analytically as the super-position of helical waves travelling in the upstream or downstream direction, and with clockwise or counter-clockwise sense of rotation, respectively. The spin-ratio formulation is applied to study the impact of various parameters (axial mean flow, non-axisymmetric burner arrangement) on the selection of the thermoacoustic mode types in a generic annular combustor configuration. Results are analysed in terms of active control strategies.

Original languageEnglish
Title of host publication9th AIAA/CEAS Aeroacoustics Conference and Exhibit
PublisherAmerican Institute of Aeronautics and Astronautics Inc.
ISBN (Print)9781624101021
DOIs
StatePublished - 2003
Event9th AIAA/CEAS Aeroacoustics Conference and Exhibit, 2003 - Hilton Head, SC, United States
Duration: 12 May 200314 May 2003

Publication series

Name9th AIAA/CEAS Aeroacoustics Conference and Exhibit

Conference

Conference9th AIAA/CEAS Aeroacoustics Conference and Exhibit, 2003
Country/TerritoryUnited States
CityHilton Head, SC
Period12/05/0314/05/03

Fingerprint

Dive into the research topics of 'Spinning and azimuthally standing acoustic modes in annular combustors'. Together they form a unique fingerprint.

Cite this