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Jian Chen,Jianzhong Li,Qingqing Dong,Jiutian Xue,Ge Hu 한국항공우주학회 2023 International Journal of Aeronautical and Space Sc Vol.24 No.3
To meet the qualification of temperature rise and reduce emissions, a high temperature rise combustor which is based on RQL (rich-burn/quick-quench/lean-burn) under different primary holes structure had been used to investigate the flow characteristic and combustion performance. The flow field was measured by PIV (particle imaging velocimetry) under different primary holes structure at normal temperature and pressure, and the combustion and emissions performances were simulated under the same conditions in this paper. The results show that the flow field, the airflow mixing effectiveness in the quench zone airflow, the distribution of temperature, the emission and the combustion efficiency change obviously with the primary holes structure. The maximum central recirculation zone height with staggered structure (Case-II) is about 23% higher than that with symmetrical structure. The central recirculation zone length is reduced by 36% and the velocity gradient in the rich zone is increased when the primary holes structure is symmetrical with three holes (Case-I). The insufficient penetration of primary jets has a negative impact to the efficient mixing of the quench zone airflow. Therefore, the symmetrical structure of primary holes is used, increasing the number of holes while reducing the area of single-hole will have a negative impact on the efficient mixing of the quench zone airflow. In addition, when the primary holes structure is symmetrical with four holes (Case-III), the combustion efficiency was reduced by 0.07% and 0.03%, and the maximum emission index of NO was increased by 14% and 19%, respectively, compared with the Case-I and Case-II. On the contrary, the maximum emission index of CO and soot were reduced in rich zone.