TY - GEN
T1 - Spinning and azimuthally standing acoustic modes in annular combustors
AU - Evesque, S.
AU - Polifke, W.
AU - Pankiewitz, C.
PY - 2003
Y1 - 2003
N2 - 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.
AB - 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.
UR - http://www.scopus.com/inward/record.url?scp=85086615670&partnerID=8YFLogxK
U2 - 10.2514/6.2003-3182
DO - 10.2514/6.2003-3182
M3 - Conference contribution
AN - SCOPUS:85086615670
SN - 9781624101021
T3 - 9th AIAA/CEAS Aeroacoustics Conference and Exhibit
BT - 9th AIAA/CEAS Aeroacoustics Conference and Exhibit
PB - American Institute of Aeronautics and Astronautics Inc.
T2 - 9th AIAA/CEAS Aeroacoustics Conference and Exhibit, 2003
Y2 - 12 May 2003 through 14 May 2003
ER -