Research on flow and dilution characteristics of single and multiple jets in high-temperature and strong swirling crossflow
-
摘要:
为提高先进航空发动机燃烧室出口温度分布品质,需要探明在强旋流燃气中非等温横向射流的流动与掺混特性。针对强旋流中的高温差单股与多股横向射流,基于双色法甲基萘激光诱导荧光技术测量了横向射流掺混过程的温度场,同时采用大涡模拟获取其三维温度场与速度场,进而揭示横向射流的流动与掺混机制。结果表明:在高温强旋流中横向射流会跟随旋流倾斜,在下游形成二次低温区,旋流的脉动也会加强横向射流掺混的非定常特征。孤立的单股射流在流向截面中表现出近似直线的倾斜,穿透深度更大;而多股射流则出现背风侧弯曲现象,其掺混效果弱于单股射流。大涡模拟结果显示了多股射流对旋流切向速度有明显的阻挡作用,导致多股横向射流的切向作用力与切向剪切层减弱,这是多股射流掺混较弱的关键原因。
-
关键词:
- 燃烧室 /
- 掺混射流 /
- 平面激光诱导荧光(PLIF) /
- 大涡模拟(LES) /
- 旋流主流下横向射流
Abstract:To enhance the quality of the exit temperature distribution from advanced combustors, it is necessary to investigate the flow and dilution characteristics of non-isothermal jets in strong swirling crossflow. In this study, two-color 1-methylnaphthalene planar laser-induced fluorescence (1-MN PLIF) thermometer technology was used to investigate the temperature distributions of single and multiple jets in strong swirling crossflow with high temperature difference. Meanwhile, large eddy simulation (LES) was employed to obtain the three-dimensional temperature and velocity fields, thereby revealing the flow and dilution mechanisms of jet in swirling crossflow. The results indicated that the low temperature jet inclined in swirling crossflow and generated a secondary low temperature zone downstream of the mainstream; the fluctuations of the swirling mainstream also intensified the jet's unsteady characteristics with distinct mode due to the jet/mainstream velocity ratio and the hole diameter. A single jet showed a nearly straight inclination in the streamwise cross-sections, whereas the multiple jets tended to be twisted to the swirl leeward side of the jets, with a lower degree of dilution than the single jet. The LES results showed that the multiple jets significantly impeded the tangential velocity of the swirling mainstream, leading to a reduction in the tangential force and tangential shear layer of the multiple transverse jets. This phenomenon was mainly attributed to the weaker dilution performance of multiple jets.
-
表 1 试验与模拟工况
Table 1. Operating conditions and case setup
工况 Mj/(kg/h) d/m Re Vr Jr N 1 8.8 0.0074 23508 3.0 16.5 1 2 13.2 0.0074 35262 4.4 35.5 1 3 18.4 0.0107 33994 3.0 16.5 1 4 27.5 0.0107 50807 4.4 35.5 1 5 32.1 0.014 45903 3.0 16.5 1 6 47.1 0.014 67324 4.4 35.5 1 7 26.4 0.0074 23508 3.0 16.5 3 8 39.6 0.0074 35262 4.4 35.5 3 -
[1] Lefebvre A H, Ballal D R. Gas turbine combustion[M]. Boca Raton: Taylor & Francis, 2010. [2] 林宇震, 林阳, 张弛, 等. 先进燃烧室分级燃烧空气流量分配的探讨[J]. 航空动力学报, 2010, 25(9): 1923-1930. Lin Yuzhen, Lin Yang, Zhang Chi, et al. Discussion on combustion airflow distribution of advanced staged combustor[J]. Journal of Aerospace Power, 2010, 25(9): 1923-1930. (in ChineseLin Yuzhen, Lin Yang, Zhang Chi, et al. Discussion on combustion airflow distribution of advanced staged combustor[J]. Journal of Aerospace Power, 2010, 25(9): 1923-1930. (in Chinese) [3] Karagozian A R. The jet in crossflow[J]. Physics of Fluids, 2014, 26(10): 101303. doi: 10.1063/1.4895900 [4] Broadwell J E, Breidenthal R E. Structure and mixing of a transverse jet in incompressible flow[J]. Journal of Fluid Mechanics, 1984, 148: 405-412. doi: 10.1017/S0022112084002408 [5] Smith S H, Mungal M G. Mixing, structure and scaling of the jet in crossflow[J]. Journal of Fluid Mechanics, 1998, 357: 83-122. [6] Esmaeili M, Afshari A, Jaberi F A. Turbulent mixing in non-isothermal jet in crossflow[J]. International Journal of Heat and Mass Transfer, 2015, 89: 1239-1257. doi: 10.1016/j.ijheatmasstransfer.2015.05.055 [7] Straußwald M, Abram C, Sander T, et al. Time-resolved temperature and velocity field measurements in gas turbine film cooling flows with mainstream turbulence[J]. Experiments in Fluids, 2020, 62(1): 3. doi: 10.1007/s00348-020-03087-2 [8] Lind S, Retzer U, Will S, et al. Investigation of mixture formation in a diesel spray by tracer-based laser-induced fluorescence using 1-methylnaphthalene[J]. Proceedings of the Combustion Institute, 2017, 36(3): 4497-4504. doi: 10.1016/j.proci.2016.07.034 [9] Trost J, Zigan L, Leipertz A, et al. Characterization of four potential laser-induced fluorescence tracers for diesel engine applications[J]. Applied Optics, 2013, 52(33): 8001-8007. doi: 10.1364/AO.52.008001 [10] 芦绮玲, 陈刚. 多孔紊动射流的数值模拟与实验研究进展[J]. 水科学进展, 2008, 19(1): 137-146. Lu Qiling, Chen Gang. Development in numerical and experimental study of the multiple jets[J]. Advances in Water Science, 2008, 19(1): 137-146. (in ChineseLu Qiling, Chen Gang. Development in numerical and experimental study of the multiple jets[J]. Advances in Water Science, 2008, 19(1): 137-146. (in Chinese) [11] 高猛, 槐文信, 曾玉红. 横流中垂直出流式多孔射流稀释特性研究[J]. 华中科技大学学报(自然科学版), 2018, 46(6): 94-98. Gao Meng, Huai Wenxin, Zeng Yuhong. Dilution characteristics of vertical multiple jets in crossflow[J]. Journal of Huazhong University of Science and Technology (Nature Science Edition), 2018, 46(6): 94-98. (in Chinese doi: 10.13245/j.hust.180617Gao Meng, Huai Wenxin, Zeng Yuhong. Dilution characteristics of vertical multiple jets in crossflow[J]. Journal of Huazhong University of Science and Technology (Nature Science Edition), 2018, 46(6): 94-98. (in Chinese) doi: 10.13245/j.hust.180617 [12] Dai W, Zhang Y, Lin Y Z, et al. Influence of the arrangement of dilution holes for dilution mixing in a three-injector reverse flow combustor[R]. Düsseldorf, Germany: ASME Turbo Expo 2014: Turbine Technical Conference and Exposition, 2014. [13] 杨思恒, 王建臣, 张弛, 等. 三头部中心分级燃烧室出口温度分布研究[J]. 工程热物理学报, 2021, 42(10): 2737-2748. Yang Siheng, Wang Jianchen, Zhang Chi, et al. Investigation on outlet temperature distribution of a three-sector centrally staged combustor[J]. Journal of Engineering Thermophysics, 2021, 42(10): 2737-2748. (in ChineseYang Siheng, Wang Jianchen, Zhang Chi, et al. Investigation on outlet temperature distribution of a three-sector centrally staged combustor[J]. Journal of Engineering Thermophysics, 2021, 42(10): 2737-2748. (in Chinese) [14] Chao Y C, Ho W C. Heterogeneous and nonisothermal mixing of a lateral jet with a swirling crossflow[J]. Journal of Thermophysics and Heat Transfer, 1991, 5(3): 394-400. doi: 10.2514/3.276 [15] Tsao J M, Lin C A. Reynolds stress modelling of jet and swirl interaction inside a gas turbine combustor[J]. International Journal for Numerical Methods in Fluids, 1999, 29(4): 451-464. doi: 10.1002/(SICI)1097-0363(19990228)29:4<451::AID-FLD796>3.0.CO;2-X [16] Panda P P, Roa M, Slabaugh C D, et al. High-repetition-rate planar measurements in the wake of a reacting jet injected into a swirling vitiated crossflow[J]. Combustion and Flame, 2016, 163: 241-257. doi: 10.1016/j.combustflame.2015.10.001 [17] Fang Zhengzhe, Zhang Chi, Liu Yushuai, et al. Thermal mixing and structure of the jet in swirling crossflow[J]. Physics of Fluids, 2024, 36(9): 095123. doi: 10.1063/5.0222782 [18] Cai J, Jeng S M, Tacina R. Multi-swirler aerodynamics - experimental measurements[C]//37th Joint Propulsion Conference and Exhibit. Salt Lake City: AIAA, 2001: 3574. [19] Yao Kanghong, He Xiaomin, Jin Yi, et al. Investigations of the effect of the primary hole on ignition performance of a three-dome model combustor with RP-3 liquid aviation fuel[J]. Aerospace Science and Technology, 2023, 139: 108403. doi: 10.1016/j.ast.2023.108403 [20] Coletti F, Benson M J, Ling J, et al. Turbulent transport in an inclined jet in crossflow[J]. International Journal of Heat and Fluid Flow, 2013, 43: 149-160. doi: 10.1016/j.ijheatfluidflow.2013.06.001 -

下载: