Volume 2 Issue 2
Apr.  1987
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Zhao Jianxing. NUMERICAL RESEARCH OF TURBULENT FLOWS IN A CYLINDRICAL COMBUSTOR[J]. Journal of Aerospace Power, 1987, 2(2): 179-181,192.
Citation: Zhao Jianxing. NUMERICAL RESEARCH OF TURBULENT FLOWS IN A CYLINDRICAL COMBUSTOR[J]. Journal of Aerospace Power, 1987, 2(2): 179-181,192.

NUMERICAL RESEARCH OF TURBULENT FLOWS IN A CYLINDRICAL COMBUSTOR

  • Received Date: 1986-11-01
  • Publish Date: 1987-04-28
  • A two-dimensional transient finite difference technique has developed to predict recirculation zones behind bluff body f lameholder in a cylindrical combustor. For turbulent flow simulation,the two-equation k-e turbulent model has been comprised in a simple computer program. The governing equations consist of continuityequation,momentum equation, turbulent kinetic energy equation and turbulentkinetic energy dissipation rate equation. The calculations show that the dimensionlesslength L/d of recirculation zones and the maximum mass flow rate Mr/Mo increase with the flameholder cone angle a. The results are infair agreement with experimental data. Therefore,the transient time-marching method employedin this paper is quite simple and reasonable.

     

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