TY - JOUR
T1 - Experimental research on dynamic response characteristics of lean premixed flame excited by acoustic standing wave
AU - Lou, Yue
AU - Li, Yikai
AU - Yang, Ziming
AU - Chen, Haiyan
AU - Zhu, Ming
N1 - Publisher Copyright:
© 2024
PY - 2024/8
Y1 - 2024/8
N2 - 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.
AB - 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.
KW - Aerospace propulsion
KW - Combustion characteristics
KW - Standing wave
KW - Thermoacoustic instability
UR - http://www.scopus.com/inward/record.url?scp=85196285654&partnerID=8YFLogxK
U2 - 10.1016/j.ast.2024.109276
DO - 10.1016/j.ast.2024.109276
M3 - Article
AN - SCOPUS:85196285654
SN - 1270-9638
VL - 151
JO - Aerospace Science and Technology
JF - Aerospace Science and Technology
M1 - 109276
ER -