Cross-frequency coupling during thermoacoustic oscillations in a pressurized aeronautical gas turbine model combustor
نویسندگان
چکیده
This paper demonstrates cross-frequency coupling between pressure, heat release rate, fuel spray and velocity oscillations in a model aeronautical gas turbine combustor operating at pressure of approximately 10 atm. Heat rate was characterized by kHz chemiluminescence (CL) imaging several species. Stereoscopic particle image velocimetry laser Mie scattering from the droplets were used to measure dynamics, respectively, 5 kHz. The fluctuations dominated frequency f0, whereas spray, CL oscillated 2f0. All non-stationary, exhibiting temporal changes amplitude. Comparing time evolution dominant frequencies amplitudes indicated behaviour consistent with mutually coupled unsynchronized self-oscillators; observed dynamics are variations reactive strength. Specifically, increases ca. 2f0 away 1:2 harmonic ratio (increased detuning) correlated decreases power f0 oscillations. corresponding nonreacting flow had natural hydrodynamic mode slightly greater than Hence, data acoustic ‘pulling’ towards ratio.
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ژورنال
عنوان ژورنال: Proceedings of the Combustion Institute
سال: 2021
ISSN: ['1873-2704', '1540-7489']
DOI: https://doi.org/10.1016/j.proci.2020.06.177