Volume 25 Issue 8
Aug.  2010
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GUAN Fa-ming, SHEN Qing, WANG Qiang. Numerical analysis of multi-mode mixed disturbance wave in a supersonic plane shear layer[J]. Journal of Aerospace Power, 2010, 25(8): 1768-1775.
Citation: GUAN Fa-ming, SHEN Qing, WANG Qiang. Numerical analysis of multi-mode mixed disturbance wave in a supersonic plane shear layer[J]. Journal of Aerospace Power, 2010, 25(8): 1768-1775.

Numerical analysis of multi-mode mixed disturbance wave in a supersonic plane shear layer

  • Received Date: 2009-06-22
  • Rev Recd Date: 2010-06-29
  • Publish Date: 2010-08-28
  • Disturbance modes and flow structures were numerically analyzed for a two-dimensional spatial evolving supersonic plane free shear layer at Mac = 1.2.The disturbance modes and the disturbances parameters of streamwise stations were analyzed with linear stability theory(LST) method and disturbance form direct numerical simulation(DNS) method.The disturbance wave evolving of specially designed disturbance frequency was simulated with disturbance form DNS method.It is found that the multi-mode disturbance without phase difference is produced by the specially designed disturbance frequency in the shear layer.

     

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