Experimental study on combustion characteristics of supersonic combustor based on alternating-wedge strut  

作　　者：Jie LI Wenyan SONG Yuhang WANG 

机构地区：[1]School of Power Energy,Northwestern Polytechnical University,Xi’an 710129,China

出　　处：《Chinese Journal of Aeronautics》2024年第5期214-227,共14页中国航空学报（英文版）

摘　　要：Acetone Planar Lase-Induced Fluorescence(PLIF)and OH-PLIF were employed to capture the fuel distribution and OH distribution downstream for the supersonic combustor based on the alternating-wedge strut.The combustion establishment process and combustion mode in the combustor under different fuel injection methods and different equivalence ratios were analyzed.Combined with the kerosene-PLIF and OH-PLIF results in the cavity combustor,a comparative analysis was conducted to understand the combustion characteristics and combustion modes between the alternating-wedge strut-based combustor and the cavity-based combustor.The results show that the combustor is in weak combustion mode in the case of low equivalence ratio,and the combustor is in intensive combustion mode in the case of high equivalence ratio.The lower limit of the equivalence ratio of the combustor to maintain the intensive combustion mode varies based on different fuel injection methods.The OH distribution under reacting condition has a strong correlation with the fuel distribution under non-reacting condition.The OH fluorescence signal near the injector is weaker when the fuel distribution is more concentrated.The injector position located at the base of the strut rear has better mixing performance,enabling the combustor to be in intensive combustion mode at a lower equivalence ratio.The combustion reaction in the alternating-wedge strut-based combustor is not necessarily dominated by mass transfer due to the mixing enhancement and premixed zone downstream of strut,while the combustion reaction process in the cavity-based combustor is mainly influenced by mass transfer.

关 键 词：Supersonic combustor Alternating-wedge strut CAVITY PLIF Fuel injection Fuel distribution Combustion characteristics Combustion mode 

分 类 号：V312[航空宇航科学与技术—航空宇航推进理论与工程]