TY - GEN
T1 - About an axisymmetric mode and a helical mode in the stable state of a model combustor
AU - Lewalle, Jacques
AU - Ali, Mohd Y.
AU - Boxx, Isaac G.
AU - Geigle, Klaus Peter
AU - Carter, Campbell D.
N1 - Funding Information:
This material is based upon work supported by the Air Force Office of Scientific Research, Air Force Material Command, USAF under Award No. FA9550-16-1-0044.
Funding Information:
This material is based upon work supported by the Air Force Office of Scientific Research, Air Force Material Command, USAF under Award No. FA9550-16-1-0044. C. Carter is supported under the Air Force Windows on the World program.
Publisher Copyright:
© 2018, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2018
Y1 - 2018
N2 - 3-component particle image velocitmetry data from a model swirl combustor are analyzed. Our previous work focused on the spontaneous transition from the stable state to the thermoacoustically excited state. Time-frequency (bandpass filterering) methods revealed a sequence of quasi-periodic modes, intermittent in time and in space. In this paper, we focus on the coexistence and interactions between two modes in the stable regime. The simplest is the axisymmetric mode, with vortex rings as the organizing flow structure. More complicated is the precessing mode, which combines a pair of counter-rotating helical vortices and a precessing recirculating vortex core. Using dynamic mode decomposition (DMD) yields different frequencies for the dominant modes. We reconcile the two methods by noting that DMD yields the fastest growing modes, whereas Fourier-related methods yield energy-dominant modes. We show that, on average, the growth of the helical or the axisymmetric mode precedes its peak energy by one to four periods. We also show that the mode amplitudes are correlated with varying signs across the burner.
AB - 3-component particle image velocitmetry data from a model swirl combustor are analyzed. Our previous work focused on the spontaneous transition from the stable state to the thermoacoustically excited state. Time-frequency (bandpass filterering) methods revealed a sequence of quasi-periodic modes, intermittent in time and in space. In this paper, we focus on the coexistence and interactions between two modes in the stable regime. The simplest is the axisymmetric mode, with vortex rings as the organizing flow structure. More complicated is the precessing mode, which combines a pair of counter-rotating helical vortices and a precessing recirculating vortex core. Using dynamic mode decomposition (DMD) yields different frequencies for the dominant modes. We reconcile the two methods by noting that DMD yields the fastest growing modes, whereas Fourier-related methods yield energy-dominant modes. We show that, on average, the growth of the helical or the axisymmetric mode precedes its peak energy by one to four periods. We also show that the mode amplitudes are correlated with varying signs across the burner.
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U2 - 10.2514/6.2018-1877
DO - 10.2514/6.2018-1877
M3 - Conference contribution
AN - SCOPUS:85044401421
SN - 9781624105241
T3 - AIAA Aerospace Sciences Meeting, 2018
BT - AIAA Aerospace Sciences Meeting
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Aerospace Sciences Meeting, 2018
Y2 - 8 January 2018 through 12 January 2018
ER -