Corner Vortex Structures Within Recirculation Zones of Confined Bluff-Body Flows

被引:0
|
作者
Squeo, Joseph N. [1 ]
Sykes, Joshua P. [1 ]
Comer, Adam L. [1 ]
Gallagher, Timothy P. [2 ]
Rankin, Brent A. [3 ]
机构
[1] Innovat Sci Solut Inc, Dayton, OH 45459 USA
[2] AF Res Lab, Edwards AFB, CA 93524 USA
[3] AF Res Lab, Wright Patterson AFB, OH 45433 USA
关键词
Vortex Structure; Boundary Layer Separation; Non Reacting Flow; Computational Fluid Dynamics Simulation; Adverse Pressure Gradient; Combustion Chambers; Combustors; Lean Premixed Combustor; LARGE-EDDY-SIMULATION; LEAN BLOWOFF; COMBUSTION; MODEL;
D O I
10.2514/1.J063820
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The vortical structures of recirculation zones in turbulent nonreacting and premixed reacting flows around confined equilateral-triangle bluff bodies are investigated using large-eddy simulations. A three-dimensional flow structure is observed within the recirculation zones of reacting and nonreacting cases; the structure includes both the "spanwise" vortices that extend the length of the recirculation zone and "corner vortex structures" that are situated adjacent to the bluff-body trailing edge and spanwise walls. The corner vortex structures enhance the mixing and residence times of fluid inside the recirculation zone. Fluid is circulated between the spanwise vortices and corner vortex structures. Corner vortex structures always appear downstream (relative to the local flow) of the boundary-layer separation location on the spanwise walls within the recirculation zone, and they are absent when boundary-layer formation on the spanwise walls is prevented. Laminar boundary-layer theory predicts the boundary-layer separation locations within similar to 12% of the calculated values from the large-eddy simulations in all but one case. These results suggest that 1) boundary-layer separation on the spanwise walls is a necessary condition for the formation of corner vortex structures, and 2) boundary-layer separation on the spanwise walls is caused by an adverse pressure gradient in the recirculation zone.
引用
收藏
页码:2900 / 2911
页数:12
相关论文
共 50 条
  • [41] Vortex structure and temperature field in transitional diffusion flame stabilized on bluff-body
    Nishimura, T
    Kawahara, H
    Morio, K
    KAGAKU KOGAKU RONBUNSHU, 2000, 26 (05) : 711 - 719
  • [42] The influence of bluff-body structural parameters and incoming velocities on advanced vortex combustor
    Wang, Zhikai
    Zeng, Zhuoxiong
    Xu, Yihua
    ENERGY DEVELOPMENT, PTS 1-4, 2014, 860-863 : 1383 - 1387
  • [43] Experiments and large-eddy simulations of acoustically forced bluff-body flows
    Ayache, S.
    Dawson, J.
    Triantafyllidis, A.
    Balachandran, R.
    Mastorakos, E.
    TURBULENCE, HEAT AND MASS TRANSFER 6, 2009, : 147 - 150
  • [44] Experiments and Large-Eddy Simulations of acoustically forced bluff-body flows
    Ayache, S.
    Dawson, J. R.
    Triantafyllidis, A.
    Balachandran, R.
    Mastorakos, E.
    INTERNATIONAL JOURNAL OF HEAT AND FLUID FLOW, 2010, 31 (05) : 754 - 766
  • [45] VORTICAL STRUCTURES IN A 2-D VERTICAL BLUFF-BODY BURNER
    CHIN, LP
    TANKIN, RS
    COMBUSTION SCIENCE AND TECHNOLOGY, 1991, 80 (4-6) : 207 - 229
  • [46] Comparison of trapped vortex cavity with/without injection in annular central bluff-body trapped vortex combustor
    Han, Ji-Ang
    Li, Xiao-Dong
    Zhong, Jing-Jun
    Hangkong Dongli Xuebao/Journal of Aerospace Power, 2015, 30 (02): : 331 - 340
  • [48] MODELING OF TURBULENT REACTING FLOWS PAST A BLUFF-BODY - ASSESSMENT OF ACCURACY AND EFFICIENCY
    BAI, XS
    FUCHS, L
    COMPUTERS & FLUIDS, 1994, 23 (03) : 507 - 521
  • [49] Time-resolved particle image velocimetry in confined bluff-body burner flames
    D. Honoré
    B. Lecordier
    A. Susset
    D. Jaffré
    M. Perrin
    J. M. Most
    M. Trinité
    Experiments in Fluids, 2000, 29 : S248 - S254
  • [50] Numerical simulation of vortex structures in a two-dimensional vertical bluff-body burner for two different hydrocarbon fuels
    Kawahara, H
    Nishimura, T
    ADVANCED COMPUTATIONAL METHODS IN HEAT TRANSFER VIII, 2004, 5 : 87 - 96