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An energy method for predicting and suppressing the instability of a three-dimensional thermoacoustic coupling system with a micro-perforated plate

Treść / Zawartość
Identyfikatory
Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
The Micro-Perforated Plate (MPP) is widely used in the noise control field with advantages of high temperature resistance and being suitable for high-speed flow fields. In this paper, an analytical model of the three-dimensional thermoacoustic coupling system suppressed by the MPP is established through the energy principle and Rayleigh-Ritz method. A modified Fourier series will be applied to characterize the sound pressure distribution function to meet arbitrary impedance boundary conditions. Based on the sound intensity and divergence, the energy transmission path and distribution law of energy sources and traps are analyzed. The suppression mechanism of a MPP on the thermoacoustic instability is revealed.
Rocznik
Strony
755--768
Opis fizyczny
Bibliogr. 13 poz., rys., tab.
Twórcy
autor
  • Shanghai Marine Diesel Engine Research Institute, Shanghai, China
  • National Engineering Research Center of Special Equipment and Power System for Ship and Marine Engineering, Shanghai, China
autor
  • Shanghai Marine Diesel Engine Research Institute, Shanghai, China
  • National Engineering Research Center of Special Equipment and Power System for Ship and Marine Engineering, Shanghai, China
autor
  • College of Power and Energy Engineering, Harbin Engineering University, Harbin, China
autor
  • College of Power and Energy Engineering, Harbin Engineering University, Harbin, China
autor
  • College of Power and Energy Engineering, Harbin Engineering University, Harbin, China
autor
  • Shanghai Marine Diesel Engine Research Institute, Shanghai, China
Bibliografia
  • 1. Armitage C.A., Riley A.J., Cant R.S., et al., 2004, Flame transfer function for swirled LPP combustion from experiments and CFD, Proceedings of the ASME Turbo Expo 2004: Power for Land, Sea, and Air, Vol. 1: Turbo Expo, 527-537.
  • 2. Chu M., Xu X., 2016, Acoustic numerical simulation of a micro-perforated panel absorber for combustion instability suppression, Acta Acoustia, 41, 2, 236-242.
  • 3. Dowling A.P., Mahmoudi Y., 2015, Combustion noise, Proceedings of the Combustion Institute, 35, 1, 65-100.
  • 4. Du J.T., Li W.L., Liu Z.G., Xu H.A., Ji Z.L., 2011, Acoustic analysis of a rectangular cavity with general impedance boundary conditions, Journal of the Acoustical Society of America, 130, 2, 807-817.
  • 5. Eldredge J.D., Dowling A.P., 2003, The absorption of axial acoustic waves by a perforated liner with bias flow, Journal of Fluid and Mechanics, 485, 307-335.
  • 6. Lefebvre A.H., Ballal D.R., 2010, Gas Turbine Combustion, CRC Press, 525.
  • 7. Leyko M., Nicoud F., Poinsot T., 2012, Comparison of direct and indirect combustion noise mechanisms in a model combustor, American Institute of Aeronautics and Astronautics Journal, 47, 11, 2709-2716.
  • 8. Ma D.Y., 1975, Theory and design of micro-perforated panel sound absorption structure, Scientia Sinica, 1, 38-50.
  • 9. Schönfeld T., Poinsot T., 1999, Influence of boundary conditions in LES of premixed combustion instabilities, Center for Turbulence Research Annual Research Briefs, 73-84.
  • 10. Schuller T., Durox D., Candel S., 2003, Self-induced combustion oscillations of laminar premixed flames stabilized on annular burners, Combustion and Flame, 135, 4, 525-537.
  • 11. Seo S., 2003, Combustion instability mechanism of a lean premixed gas turbine combustor, Journal of Mechanical Science and Technology, 17, 6, 906-913.
  • 12. Sun X.F., 2010, Thermoacoustic oscillating calculation of longitudinal equivalence frequency and stability in aero-engineafterburner,https://api.semanticscholar.org/CorpusID:111882612
  • 13. Zhang X.Q., 2020, Acoustic Behavior of Micro-Perforated Panels in Grazing Flow, The Hong Kong Polytechnic University.
Uwagi
Opracowanie rekordu ze środków MNiSW, umowa nr POPUL/SP/0154/2024/02 w ramach programu "Społeczna odpowiedzialność nauki II" - moduł: Popularyzacja nauki (2025).
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-d5117cb7-26da-4572-99b5-8df460a13ea6
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