Step geometry and countercurrent effects in dump combustor: Reacting flow

被引:2
|
作者
Sengupta, K. [1 ]
Russell, K. [1 ]
Mashayek, F. [1 ]
机构
[1] Univ Illinois, Dept Mech & Ind Engn, Chicago, IL 60607 USA
关键词
D O I
10.1080/10407780802289434
中图分类号
O414.1 [热力学];
学科分类号
摘要
In this article we report a numerical investigation of reacting flow in dump combustors with counterflow and modified step geometry. The flow is simulated by solving Reynolds-averaged Navier-Stokes equations in the framework of the realizable - turbulence model. A two-layer approach is used for the near-wall treatment, whereas a one-equation model is employed for the viscous sublayer. The closure for the reaction source term is based on the eddy dissipation concept. The article includes a study of the effect of reaction on the base flow, the effect of countercurrent on the flame, and finally, the role of step geometry. Application of countercurrent results in a thicker averaged flame surface, which leads to an overall increase in the heat release within the combustor. The effect of alteration of the step geometry is found to be much more complicated. At low levels of counterflow there is an increase in turbulence intensity with an increase of the step angle but little change in heat release.
引用
收藏
页码:569 / 580
页数:12
相关论文
共 50 条
  • [1] Step geometry and countercurrent effects in dump combustor, part 1: Cold flow
    Sengupta, K.
    Russell, K.
    Mashayek, F.
    AIAA JOURNAL, 2007, 45 (08) : 2033 - 2041
  • [2] Enhancing combustion in a dump combustor using countercurrent shear - Part 2: Heat release rate measurements and geometry effects
    Behrens, Alison A.
    Anderson, Matthew J.
    Strykowski, Paul J.
    Forliti, David J.
    Proceedings of the ASME Heat Transfer Division 2005, Vol 1, 2005, 376-1 : 347 - 354
  • [3] VELOCITY CHARACTERISTICS OF REACTING AND NONREACTING FLOWS IN A DUMP COMBUSTOR
    GABRUK, RS
    ROE, LA
    JOURNAL OF PROPULSION AND POWER, 1994, 10 (02) : 148 - 154
  • [4] EFFECTS OF AN S-INLET ON THE FLOW IN A DUMP COMBUSTOR
    SCHETZ, JA
    GURUSWAMY, J
    MARCHMAN, JF
    JOURNAL OF SPACECRAFT AND ROCKETS, 1985, 22 (02) : 221 - 224
  • [5] EFFECTS OF AN S-INLET ON THE FLOW IN A DUMP COMBUSTOR.
    Schetz, J.A.
    Guruswamy, J.
    Marchman III, J.F.
    1600, (22):
  • [6] THE EFFECTS OF COWLING GEOMETRY, AREA RATIO AND DUMP GAP ON A COMBUSTOR DIFFUSION SYSTEM
    Shen, Shanping
    He, Pei
    Shang, Mingtao
    Mao Ronghai
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2014, VOL 4B, 2014,
  • [7] Controlling volumetric heat release rates in a dump combustor using countercurrent shear
    Behrens, A. A.
    Strykowski, P. J.
    AIAA JOURNAL, 2007, 45 (06) : 1317 - 1323
  • [8] Enhancing combustion in a dump combustor using countercurrent shear - Part 1: Nonreacting flow control and preliminary combustion results
    Forliti, David J.
    Behrens, Alison A.
    Strykowski, Paul J.
    Tang, Brian A.
    PROCEEDINGS OF THE ASME HEAT TRANSFER DIVISION 2005, VOL 1, 2005, 376-1 : 339 - 346
  • [9] Simulation of turbulent reacting flow in a swirl combustor
    Zhang, Jian
    Chen, Chunming
    NUMERICAL HEAT TRANSFER PART A-APPLICATIONS, 2008, 53 (06) : 605 - 624
  • [10] Flow dynamics in low aspect ratio dump combustor
    Yadav, N. P.
    Kushari, Abhijit
    PROPULSION AND POWER RESEARCH, 2014, 3 (04) : 187 - 195