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 (eg
equivalence ratio equaling to 065)
the flame was much sensitive to middle acoustic frequency owing to low extinction strain rate
Oxyfuel combustion of propane based on rapidly mixed tubular flame technology
Experimental research progress in combustion of metal under microgravity
Flame structure in supersonic combustion chamber based on 500 Hz OH-PLIF technology,
Experiment on structure of premixed flame in annular combustor using OH-PLIF
Full status two phase turbulent combustion model
Related Author
王宁飞
李军伟
石保禄
初庆钊
赵晓尧
彭维康
Jianzhong LIU
Peihui XU
Related Institution
北京理工大学 宇航学院
Institute for Thermal Power Engineering, Zhejiang University
重庆大学 能源与动力工程学院 低品位能源利用技术及系统教育部重点实验室
National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics,School of Jet Propulsion, Beijing University of Aeronautics and Astronautics
School of Mechanical Engineering,Southwest Jiaotong University