Volume 22 Issue 8
Aug.  2007
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WANG Suo-fang, ZHU Qiang-hua, ZHANG Yu, LUAN Hai-feng, HUANG Ai-xia. Numerical studies of heat transfer in a rotor-stator cavity with different radial positions of pre-swirl inlet[J]. Journal of Aerospace Power, 2007, 22(8): 1227-1232.
Citation: WANG Suo-fang, ZHU Qiang-hua, ZHANG Yu, LUAN Hai-feng, HUANG Ai-xia. Numerical studies of heat transfer in a rotor-stator cavity with different radial positions of pre-swirl inlet[J]. Journal of Aerospace Power, 2007, 22(8): 1227-1232.

Numerical studies of heat transfer in a rotor-stator cavity with different radial positions of pre-swirl inlet

  • Received Date: 2006-07-10
  • Rev Recd Date: 2007-01-31
  • Publish Date: 2007-08-28
  • The three-dimensional numerical simulations of heat transfer in a rotor-stator cavity with pre-swirl nozzles at different radial positions in the stator were conducted in this paper.The standard k-ε turbulence model and unstructured grid were applied with the purpose of investigating the heat transfer characteristics.Under the constant mass flow rate and the different radial position of the pre-swirl nozzles, the outflow temperature and the effect of heat transfer on the rotor are greatly affected by the different rotational Reynolds number, pre-swirl angle and rotor-stator gap.The results show that the heat transfer of the rotor is enhanced with the increase of the rotational Reynolds number or the decrease of the rotor-stator gap.When the pre-swirl nozzles were moved out along the radial direction, the temperature difference between the inlet and the outlet and the averaged Nusselt number take on up-down tendency, that is, exists a optimum radial position of the pre-swirl nozzles.

     

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