TY - JOUR
T1 - Effect of the flame motion on azimuthal combustion instabilities
AU - Song, Yan
AU - Liu, Xiaokang
AU - Li, Jingxuan
AU - Yang, Lijun
N1 - Publisher Copyright:
© 2022 Elsevier Masson SAS
PY - 2022/11
Y1 - 2022/11
N2 - In the analysis of combustion instabilities in the annular combustors, especially for the azimuthal combustion modes, the flame motion is usually neglected and the flame is typically regarded as a discontinuity at rest. However, this simplicity may cause severe prediction errors for certain conditions. In this paper, the influence of the flame motion on the entropy, vortex, acoustic, and intrinsic modes in the annular combustion chamber is investigated by constructing an analytical model with the flame motion. Meantime, the influence of flame model parameters is also explored. The flame motion can affect both the frequency and growth rate of the entropy mode, but the growth rate is influenced more significantly. This effect can be damped or enlarged by the inlet Mach number depending on which parameter of flame model remains unchanged. The effect of the flame motion on vortex, acoustic, and intrinsic modes remains small when the inlet Mach number is very small. However, the increase of inlet Mach number can enlarge this effect.
AB - In the analysis of combustion instabilities in the annular combustors, especially for the azimuthal combustion modes, the flame motion is usually neglected and the flame is typically regarded as a discontinuity at rest. However, this simplicity may cause severe prediction errors for certain conditions. In this paper, the influence of the flame motion on the entropy, vortex, acoustic, and intrinsic modes in the annular combustion chamber is investigated by constructing an analytical model with the flame motion. Meantime, the influence of flame model parameters is also explored. The flame motion can affect both the frequency and growth rate of the entropy mode, but the growth rate is influenced more significantly. This effect can be damped or enlarged by the inlet Mach number depending on which parameter of flame model remains unchanged. The effect of the flame motion on vortex, acoustic, and intrinsic modes remains small when the inlet Mach number is very small. However, the increase of inlet Mach number can enlarge this effect.
KW - Acoustic mode
KW - Azimuthal combustion instabilities
KW - Entropy mode
KW - Flame motion
KW - Intrinsic mode
KW - Vortex mode
UR - https://www.scopus.com/pages/publications/85140142468
U2 - 10.1016/j.ast.2022.107930
DO - 10.1016/j.ast.2022.107930
M3 - 文章
AN - SCOPUS:85140142468
SN - 1270-9638
VL - 130
JO - Aerospace Science and Technology
JF - Aerospace Science and Technology
M1 - 107930
ER -