Volume 24 Issue 5
May  2009
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HAN Ji-ang, ZHONG Jing-jun, YAN Hong-ming, SUN Peng, YU Yang. Numerical research of three dimensional flow-path in a ram-rotor[J]. Journal of Aerospace Power, 2009, 24(5): 1079-1088.
Citation: HAN Ji-ang, ZHONG Jing-jun, YAN Hong-ming, SUN Peng, YU Yang. Numerical research of three dimensional flow-path in a ram-rotor[J]. Journal of Aerospace Power, 2009, 24(5): 1079-1088.

Numerical research of three dimensional flow-path in a ram-rotor

  • Received Date: 2008-05-09
  • Rev Recd Date: 2008-09-16
  • Publish Date: 2009-05-28
  • According to the design method of a typical three dimensional supersonic intake,a kind of three dimensional flow-path of a ram-rotor was designed.The three dimensional Reynolds-averaged Navier-Stokes equations and the Spalart-Allmaras turbulent model were adopted to simulate numerically the flow field of the designed three dimensional flow-path of the ram-rotor.It has been found that,unlike the linear shock wave system in three dimensional supersonic intake,the shock wave in the three dimensional flow-path is curved shock wave.As compared to the two dimensional flow-path,the shock wave system in the three dimensional flow-path is more vaguer and complex.The back pressure and the rotational speed have great influence on the performance of the three dimensional flow-path.

     

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