Volume 24 Issue 9
Sep.  2009
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LIU You-hong, GUO Nan, LI Jiang-ning, CAI Juan, XU Xing-ping. Effect of cut angles at trailing edge on the performance of a lobed mixer[J]. Journal of Aerospace Power, 2009, 24(9): 1917-1922.
Citation: LIU You-hong, GUO Nan, LI Jiang-ning, CAI Juan, XU Xing-ping. Effect of cut angles at trailing edge on the performance of a lobed mixer[J]. Journal of Aerospace Power, 2009, 24(9): 1917-1922.

Effect of cut angles at trailing edge on the performance of a lobed mixer

  • Received Date: 2008-09-12
  • Rev Recd Date: 2008-12-11
  • Publish Date: 2009-09-28
  • The principle of effect of different cut angles at trailing edge of a practical lobed mixer on the thermal efficiency and the total-pressure recovery coefficient was studied by 3D-CFD(computational fluid dynamics)numerical simulation.The results show that,when the angles cut at trailing edge of the lobed mixer vary from 2.5° to 15°,the thermal efficiency augments and the total-pressure recovery coefficient decline as the angle increases,and when the cut angles vary from 15° to 60°,the thermal efficiency declines and the total-pressure recovery coefficient augments as the angle increases.

     

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