中国科学院机构知识库网格
Chinese Academy of Sciences Institutional Repositories Grid
Numerical research on the mixing mechanism of lobed mixer with inlet swirl in linear radial distribution

文献类型:期刊论文

作者Lei, Zhijun; Zhang, Yanfeng; Zhu, Zihao; Zhu, Junqiang
刊名PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY
出版日期2015-05-01
卷号229期号:3页码:280-297
关键词Lobed mixer inlet swirl streamwise vortices normal vortices jet mixing mixing nozzle
英文摘要A detailed numerical simulation is presented to investigate the effects of inlet swirl and its radial distribution on the mixing mechanisms of a turbofan mixer with 12 lobes, by using the commercial ANSYS CFX solver and k- SST model. The core-to-bypass temperature ratio and pressure ratio were set to 2.59 and 0.97, respectively, giving the Mach number of 0.66 and bypass ratio of 2.65 at mixing nozzle outlet. In the core inlet, the swirl angle was raised from 0 degrees to 30 degrees in a uniform or linear radial distribution manner. The inlet swirl and its radial gradient did enhance the development, interaction, and dissipation of the vortices downstream of lobed mixer, resulting in accelerating the lobed jet mixing. When the inlet swirl was less than 20 degrees, the total pressure and thrust loss increments of lobed jet were acceptable and no more than 0.26% and 1.57%, respectively, compared with the baseline case. The results also showed that the three-dimensional separation bubble on center-body and the backflows along jet axis at the rail of center-body, resulting from the swirling flow between lobes' trough and center-body, were the dominant sources of total pressure and thrust losses for all cases with inlet swirl. And, reasonable radial distribution of inlet swirl could inhibit the aforementioned 3D separation and backflow, and thus limited the increment of jet mixing loss favorably.
WOS标题词Science & Technology ; Technology
类目[WOS]Engineering, Mechanical
研究领域[WOS]Engineering
关键词[WOS]PROPER ORTHOGONAL DECOMPOSITION ; TURBOFAN EXHAUST DUCT ; FORCED MIXER ; NOZZLES ; FLOW ; DOWNSTREAM
收录类别SCI
语种英语
WOS记录号WOS:000353037600004
公开日期2015-12-22
源URL[http://ir.etp.ac.cn/handle/311046/98949]  
专题工程热物理研究所_中国科学院工程热物理所(论文库)_期刊论文(SCI)
作者单位Chinese Acad Sci, Inst Engn Thermophys, Key Lab Light Duty Gas Turbine, Beijing 100190, Peoples R China
推荐引用方式
GB/T 7714
Lei, Zhijun,Zhang, Yanfeng,Zhu, Zihao,et al. Numerical research on the mixing mechanism of lobed mixer with inlet swirl in linear radial distribution[J]. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY,2015,229(3):280-297.
APA Lei, Zhijun,Zhang, Yanfeng,Zhu, Zihao,&Zhu, Junqiang.(2015).Numerical research on the mixing mechanism of lobed mixer with inlet swirl in linear radial distribution.PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY,229(3),280-297.
MLA Lei, Zhijun,et al."Numerical research on the mixing mechanism of lobed mixer with inlet swirl in linear radial distribution".PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY 229.3(2015):280-297.

入库方式: OAI收割

来源:工程热物理研究所

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