Study on the flow characteristics and oscillating mechanism of a swirl flame

被引:9
作者
Di, Dong [1 ]
Yan, Yingwen [1 ]
Liu, Yunpeng [1 ]
机构
[1] Nanjing Univ Aeronaut & Astronaut, Coll Energy & Power Engn, Nanjing 210016, Peoples R China
基金
中国国家自然科学基金;
关键词
Large-eddy simulation; Oscillating combustion; Partially premixed combustion; Inner recirculation zone; PVC; POD; COMBUSTION; STABILIZATION;
D O I
10.1016/j.fuel.2021.121657
中图分类号
TE [石油、天然气工业]; TK [能源与动力工程];
学科分类号
0807 ; 0820 ;
摘要
The larger eddy simulation (LES) method was used to simulate the combustion oscillation using a partially premixed combustion model and coupling with a user-defined function. The simulated results were post processed by proper orthogonal decomposition (POD) and compared with the experimental results. The results showed that the asymmetry of the upper and lower vortex structures in the inner recirculation zone represented the destruction of the vortex structures and reflected the occurrence of a processing vortex core (PVC). The PVC structure produced by the swirler was more complex than a cyclone. The inner shear layer (ISL) and the outer shear layer (OSL) appeared in the inner and outer recirculation zones respectively, which represented the region with the strongest velocity pulsation; the velocity pulsation of axial centerline could be used to characterize the pulsation energy when the combustion oscillation occurred. First, necking occurred in the inner recirculation zone, and then it adhered to the center of the swirler outlet. The ISL and OSL had strong shearing actions that generating pulsating energy, then they gradually developed downstream and merged into the inner recirculation zone. The different rotation directions of the inner and outer recirculation zones increased the instability of the boundary of the inner recirculation zone. It could also increase the breakdown of the asymmetric vortex structures and exacerbated the occurrence of the PVC. In addition, the phase difference between the heat release rate and pressure pulsation in different regions was different, which leaded to inconsistent driving characteristics of the flame oscillation.
引用
收藏
页数:15
相关论文
共 26 条
[1]   Extinction of laminar partially premixed flames [J].
Aggarwal, Suresh K. .
PROGRESS IN ENERGY AND COMBUSTION SCIENCE, 2009, 35 (06) :528-570
[2]  
Chuangqi, 2017, GUANGDONG CHEM IND, V44, P41
[3]   CONTROL REQUIREMENTS FOR THE RB-211 LOW-EMISSION COMBUSTION SYSTEM [J].
CORBETT, NC ;
LINES, NP .
JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 1994, 116 (03) :527-533
[4]   Impact of Precessing Vortex Core Dynamics on Shear Layer Response in a Swirling Jet [J].
Frederick, Mark ;
Manoharan, Kiran ;
Dudash, Joshua ;
Brubaker, Brian ;
Hemchandra, Santosh ;
O'Connor, Jacqueline .
JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 2018, 140 (06)
[5]   Mixing and stabilization study of a partially premixed swirling flame using laser induced fluorescence [J].
Galley, D. ;
Ducruix, S. ;
Lacas, F. ;
Veynante, D. .
COMBUSTION AND FLAME, 2011, 158 (01) :155-171
[6]   Dynamics and stability of lean-premixed swirl-stabilized combustion [J].
Huang, Ying ;
Yang, Vigor .
PROGRESS IN ENERGY AND COMBUSTION SCIENCE, 2009, 35 (04) :293-364
[7]  
Lai A, 2020, COMBUST SCI TECHNOL, V26, P10
[8]   Modeling premixed combustion-acoustic wave interactions: A review [J].
Lieuwen, T .
JOURNAL OF PROPULSION AND POWER, 2003, 19 (05) :765-781
[9]  
Liu Y., 2018, AIAA J, V57, P1, DOI DOI 10.1016/J.ORGEL.2018.02.029
[10]   Vortex breakdown: a review [J].
Lucca-Negro, O ;
O'Doherty, T .
PROGRESS IN ENERGY AND COMBUSTION SCIENCE, 2001, 27 (04) :431-481