Experimental research on dynamic response characteristics of lean premixed flame excited by acoustic standing wave

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Abstract

The compact combustor holds great potential in the aerospace field. However, it faces challenges in terms of interaction between acoustic waves and flames, which affects combustion efficiency and intensity. In this study, the dynamic response of lean premixed flames under the excitation of a transverse standing wave acoustic field with different frequencies and amplitudes. The results indicate that the flame's response frequency is consistent with the excitation frequency. Decreasing the sound wave frequency and increasing the sound amplitude both lead to an increase in flame area oscillation, thereby enhancing the heat release rate. However, excessively high sound pressure values can enhance fuel diffusion, resulting in a reduction in flame area or even local flame extinction, which significantly decreases flame intensity. This research provides valuable insights into the behavior of lean premixed flames under acoustic excitation, contributing to the optimization of combustion processes and improvement of efficiency and performance in compact combustors.

Original languageEnglish
Article number109276
JournalAerospace Science and Technology
Volume151
DOIs
Publication statusPublished - Aug 2024

Keywords

  • Aerospace propulsion
  • Combustion characteristics
  • Standing wave
  • Thermoacoustic instability

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