TY - JOUR
T1 - 声场扰动下预混旋流管状火焰动态响应特性
AU - Yu, Xiao
AU - Zhao, Xiaoyao
AU - Ma, Kang
AU - Wang, Ningfei
AU - Li, Shuiqing
AU - Shi, Baolu
N1 - Publisher Copyright:
© 2020, Editorial Department of Journal of Aerospace Power. All right reserved.
PY - 2020/8/1
Y1 - 2020/8/1
N2 - To investigate the combustion instability of the premixed swirling tubular flame, the responses characteristics of methane/air premixed flames to longitudinal acoustic field was experimentally studied with different air volume flow rates and methane equivalent ratios. The dynamic response range of flame to different acoustic frequencies was revealed,and the variation of flame structure,acoustic pressure and OH* fluctuations under acoustics perturbation were studied. The results showed that the flame presented the low-pass filtering characteristic, demonstrating very weak response to the high acoustic frequency. For middle and low acoustic frequency, the flame was forced to oscillate at the same frequency, and even quenched at a lower acoustic frequency. In addition, the low-pass filtering behaviors were slightly affected by the flow rate and equivalent ratio. According to the calculated extinction strain rate, near lean extinction limit (e.g., equivalence ratio equaling to 0.65), the flame was much sensitive to middle acoustic frequency owing to low extinction strain rate, generally presenting flame lift-off.
AB - To investigate the combustion instability of the premixed swirling tubular flame, the responses characteristics of methane/air premixed flames to longitudinal acoustic field was experimentally studied with different air volume flow rates and methane equivalent ratios. The dynamic response range of flame to different acoustic frequencies was revealed,and the variation of flame structure,acoustic pressure and OH* fluctuations under acoustics perturbation were studied. The results showed that the flame presented the low-pass filtering characteristic, demonstrating very weak response to the high acoustic frequency. For middle and low acoustic frequency, the flame was forced to oscillate at the same frequency, and even quenched at a lower acoustic frequency. In addition, the low-pass filtering behaviors were slightly affected by the flow rate and equivalent ratio. According to the calculated extinction strain rate, near lean extinction limit (e.g., equivalence ratio equaling to 0.65), the flame was much sensitive to middle acoustic frequency owing to low extinction strain rate, generally presenting flame lift-off.
KW - Acoustics perturbation
KW - Flame structure
KW - Swirl combustion
KW - Thermoacoustic oscillation
KW - Tubular flame
UR - http://www.scopus.com/inward/record.url?scp=85092420949&partnerID=8YFLogxK
U2 - 10.13224/j.cnki.jasp.2020.08.010
DO - 10.13224/j.cnki.jasp.2020.08.010
M3 - 文章
AN - SCOPUS:85092420949
SN - 1000-8055
VL - 35
SP - 1655
EP - 1663
JO - Hangkong Dongli Xuebao/Journal of Aerospace Power
JF - Hangkong Dongli Xuebao/Journal of Aerospace Power
IS - 8
ER -