Mixing in nearwall regions downstream of a sonic jet in a supersonic crossflow at Mach 2.7

被引:46
|
作者
Sun, Ming-bo [1 ]
Hu, Zhi-wei [2 ]
机构
[1] Natl Univ Def Technol, Sci & Technol Scramjet Lab, Changsha 410073, Hunan, Peoples R China
[2] Univ Southampton, Fac Engn & Environm, Aerodynam & Flight Mech, Southampton SO17 1BJ, Hants, England
基金
英国工程与自然科学研究理事会; 美国国家科学基金会;
关键词
LARGE-EDDY SIMULATION; TRANSVERSE JET; NUMERICAL-SIMULATION; CAVITY FLAMEHOLDER; COMBUSTOR; INJECTION; ETHYLENE; GENERATION; HYDROGEN;
D O I
10.1063/1.5045752
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
The mixing status downstream of a transverse sonic jet in a supersonic crossflow at a Mach number of 2.7 was studied. Direct numerical simulations were performed to investigate the transport of a passive scalar of jet fluid for jet-to-cross-flow momentum flux ratios (denoted as J) of 1.85 and 5.5. Results showed that a counter-rotating vortex pair (CVP) with two branches generates in the jet nearfield, grows, and breaks into small eddies in the farfield, which enhances the local mixing. A nearwall region in the jet lee between the CVP branches is identified to have a low mass fraction of the jet fluid and this region expands as J increases. Analysis of the streamlines originating from the jet orifice and the crossflow suggests that the jet fluid in the downstream nearwall region is entrained by the lateral crossflow upstream of the jet, which travels around the jet and mixes with the injectants downstream of the jet. Higher J leads to a lower mass fraction of the jet fluid in the nearwall region of the jet nearfield, but produces a higher mass fraction in the nearwall region of the farfield. Athree-dimensional schematic of the jet wakes is presented and explains the formation of the nearwall low mass fraction zone in the jet nearfield. Published by AIP Publishing.
引用
收藏
页数:18
相关论文
共 50 条
  • [1] Numerical investigation on mixing process of a sonic fuel jet into a supersonic crossflow
    Li, Chaolong
    Ma, Likun
    Xia, Zhixun
    Chen, Binbin
    Feng, Yunchao
    Duan, Yifan
    INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2022, 47 (87) : 37025 - 37039
  • [2] Numerical study of flow structures and mixing characteristics of a sonic jet in supersonic crossflow
    Liang, Chang-hai
    Sun, Ming-bo
    Liu, Yuan
    Li, Guang-xin
    Yu, Jiang-fei
    ACTA ASTRONAUTICA, 2020, 166 : 78 - 88
  • [3] Dynamics of sonic jet injection into supersonic crossflow
    Genin, Franklin
    Menon, Suresh
    JOURNAL OF TURBULENCE, 2010, 11 (04): : 1 - 30
  • [4] Effects of the jet-to-crossflow momentum ratio on a sonic jet into a supersonic crossflow
    Guo-Lei Wang~(a)) and Xi-Yun Lu~(b)) Department of Modern Mechanics
    Theoretical & Applied Mechanics Letters, 2011, 1 (01) : 53 - 57
  • [5] Effects of the jet-to-crossflow momentum ratio on a sonic jet into a supersonic crossflow
    Wang, Guo-Lei
    Lu, Xi-Yun
    THEORETICAL AND APPLIED MECHANICS LETTERS, 2011, 1 (01)
  • [6] Effect of boundary layer thickness on transverse sonic jet mixing in a supersonic turbulent crossflow
    Pizzaia, A.
    Rossmann, T.
    PHYSICS OF FLUIDS, 2018, 30 (11)
  • [7] Effects of the injector geometry on a sonic jet into a supersonic crossflow
    WANG GuoLei
    CHEN LiWei
    LU XiYun
    Science China(Physics,Mechanics & Astronomy), 2013, Mechanics & Astronomy)2013 (02) : 366 - 377
  • [8] Effects of the injector geometry on a sonic jet into a supersonic crossflow
    Wang GuoLei
    Chen LiWei
    Lu XiYun
    SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2013, 56 (02) : 366 - 377
  • [9] Effects of the injector geometry on a sonic jet into a supersonic crossflow
    GuoLei Wang
    LiWei Chen
    XiYun Lu
    Science China Physics, Mechanics and Astronomy, 2013, 56 : 366 - 377
  • [10] LES of an inclined sonic jet into a turbulent crossflow at Mach 3.6
    Ferrante, Antonino
    Matheou, Georgios
    Dimotakis, Paul E.
    JOURNAL OF TURBULENCE, 2011, 12 (02): : 1 - 32