TY - JOUR
T1 - Modal Decomposition Analysis of Combustion Instability Due to External Perturbation in a Mesoscale Burner Array
AU - Choi, Jeongan
AU - Rajasegar, Rajavasanth
AU - Liu, Qili
AU - Lee, Tonghun
AU - Yoo, Jihyung
N1 - • Office of Naval Research (Grant No. N00014-17-1-2538; Funder ID: 10.13039/100000006).
The authors of this work would like to acknowledge the support of Office of Naval Research through ONR Grant No. N00014-17-1-2538 with Dr. Steven Martens as program manager.
PY - 2022/5/1
Y1 - 2022/5/1
N2 - In this work, the growth regime of combustion instability was studied by analyzing 10 kHz OH planar laser-induced fluorescence (PLIF) images through a combination of dynamic mode decomposition (DMD) and spectral proper orthogonal decomposition (SPOD) methods. Combustion instabilities were induced in a mesoscale burner array through an external speaker at an imposed perturbation frequency of 210 Hz. During the transient growth phase of combustion instability, 10 kHz OH PLIF imaging was employed to capture spatially and temporally resolved flame dynamics. Increased acoustic perturbations prevented flame reignition in the central recirculation zone and eventually led to the flame being extinguished inward from the outer burner array elements. Coherent modes and their growth rates were obtained from DMD spectral analyses of high-speed OH PLIF images. Positive growth rates were observed at the forcing frequency during the growth regime. Coherent structures, closely associated with thermoacoustic instability, were extracted using an appropriate SPOD filter operation to identify mode structures that correlate to physical phenomena such as shear layer instability and flame response to longitudinal acoustic forcing. Overall, a combination of DMD and SPOD was shown to be effective at analyzing the onset and propagation of combustion instabilities, particularly under transient burner operations.
AB - In this work, the growth regime of combustion instability was studied by analyzing 10 kHz OH planar laser-induced fluorescence (PLIF) images through a combination of dynamic mode decomposition (DMD) and spectral proper orthogonal decomposition (SPOD) methods. Combustion instabilities were induced in a mesoscale burner array through an external speaker at an imposed perturbation frequency of 210 Hz. During the transient growth phase of combustion instability, 10 kHz OH PLIF imaging was employed to capture spatially and temporally resolved flame dynamics. Increased acoustic perturbations prevented flame reignition in the central recirculation zone and eventually led to the flame being extinguished inward from the outer burner array elements. Coherent modes and their growth rates were obtained from DMD spectral analyses of high-speed OH PLIF images. Positive growth rates were observed at the forcing frequency during the growth regime. Coherent structures, closely associated with thermoacoustic instability, were extracted using an appropriate SPOD filter operation to identify mode structures that correlate to physical phenomena such as shear layer instability and flame response to longitudinal acoustic forcing. Overall, a combination of DMD and SPOD was shown to be effective at analyzing the onset and propagation of combustion instabilities, particularly under transient burner operations.
KW - coherent modes
KW - dynamic mode decomposition
KW - mesoscale burner array
KW - planar laser induced fluorescence
KW - spectral proper orthogonal decomposition
KW - swirl stabilized flame
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U2 - 10.1115/1.4053445
DO - 10.1115/1.4053445
M3 - Article
AN - SCOPUS:85125458199
SN - 0742-4795
VL - 144
JO - Journal of Engineering for Gas Turbines and Power
JF - Journal of Engineering for Gas Turbines and Power
IS - 5
M1 - 051011 EN
ER -