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

被引:0
|
作者
Lou, Yue [1 ]
Li, Yikai [1 ,2 ]
Yang, Ziming [1 ]
Chen, Haiyan [1 ]
Zhu, Ming [1 ]
机构
[1] Beijing Inst Technol, Sch Mech Engn, Beijing 100081, Peoples R China
[2] Beijing Inst Technol, Chongqing Innovat Ctr, Chongqing 401120, Peoples R China
基金
中国国家自然科学基金; 北京市自然科学基金;
关键词
Thermoacoustic instability; Aerospace propulsion; Standing wave; Combustion characteristics; DIFFUSION FLAME; COMBUSTION INSTABILITIES; JET; FLOW; VISUALIZATION; ENHANCEMENT; DIAGNOSTICS; BEHAVIORS; STABILITY;
D O I
10.1016/j.ast.2024.109276
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
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.
引用
收藏
页数:12
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