Volume 22 Issue 9
Sep.  2007
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Article Navigation >  Journal of Aerospace Power  > 2007  >  22(9): 1439-1443
WANG Fei, LEI Yong, YANG Hua. Numerical simulation of 3-D flow field in an aeroengine combustor nozzle-loop[J]. Journal of Aerospace Power, 2007, 22(9): 1439-1443.
Citation: WANG Fei, LEI Yong, YANG Hua. Numerical simulation of 3-D flow field in an aeroengine combustor nozzle-loop[J]. Journal of Aerospace Power, 2007, 22(9): 1439-1443.
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Numerical simulation of 3-D flow field in an aeroengine combustor nozzle-loop

  • School of Power and Enery, Northwestern Polytechnical University, Xi'an 710072, China

  • Received Date: 2006-09-11
  • Rev Recd Date: 2007-01-12
  • Publish Date: 2007-09-28
    Abstract
  • According to the structural characteristic of the nozzle-loop,a grid calculation model of nozzle-loop was generated by using tetrahedral unstructured grid and thin & thick grid meshing method.And,numerical simulation was performed for the 3-D flow field of nozzle-loop,providing in detail the interior flow characteristic of single nozzle and the outflow flux of nozzle-loop.The results lay a firm basis for further research of nozzle-loop's flux distribution trait.

     

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