Volume 12 Issue 4
Oct.  1997
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Article Navigation >  Journal of Aerospace Power  > 1997  >  12(4): 350-352
Xu Hang, Huang Yang. NUMERICAL SIMULATION OF COMBUSTOR FLOWS[J]. Journal of Aerospace Power, 1997, 12(4): 350-352.
Citation: Xu Hang, Huang Yang. NUMERICAL SIMULATION OF COMBUSTOR FLOWS[J]. Journal of Aerospace Power, 1997, 12(4): 350-352.
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NUMERICAL SIMULATION OF COMBUSTOR FLOWS

  • 1.

    4th Dept.Beijing University of Aeronautics and Astronautics,Beijing 100083

  • 2.

    4th Dept.Beijing University of Aeronautics and Astronautics,Beijing 100083

  • Received Date: 1996-10-01
  • Rev Recd Date: 1997-01-01
  • Publish Date: 1997-10-28
    Abstract
  • A method has been developed for calculation of three-dimensional flows in aeroengine combustor including diffuser and flametube,inner and outer annuluses.The 3D body-fitting grid has been generated to deal with the complex geometry of the combustor.The non-staged grid scheme and k-ε turbulence model has been adopted.The mass flowing thought primary holes,dilution holes and film cooling holes has been calculated.The calculated results are consistent reasonably with the experimental measurements.

     

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      沈阳化工大学材料科学与工程学院 沈阳 110142

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