Volume 32 Issue 11
Nov.  2017
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Experiment on static characteristics of plasma synthetic jet actuator with oblique orifice[J]. Journal of Aerospace Power, 2017, 32(11): 2784-2790. doi: 10.13224/j.cnki.jasp.2017.11.028
Citation: Experiment on static characteristics of plasma synthetic jet actuator with oblique orifice[J]. Journal of Aerospace Power, 2017, 32(11): 2784-2790. doi: 10.13224/j.cnki.jasp.2017.11.028

Experiment on static characteristics of plasma synthetic jet actuator with oblique orifice

doi: 10.13224/j.cnki.jasp.2017.11.028
  • Received Date: 2016-04-22
  • Publish Date: 2017-11-28
  • A plasma synthetic jet actuator with oblique orifice was designed. The discharge characteristics and flow field characteristics were researched by electric parameter measurement system and highspeed Schlieren technology. Results showed that compared with the actuator with normal orifice, the injection flow induced by the jet actuator with oblique orifice tended to attach the wall and behave with significant asymmetry, enhancing the jet flow control capability. Moreover, the effect of buoyancy on the evolution of high temperature plasma jet flow was observed, the normal velocity induced by the buoyancy effect altered the flow direction, and this effect got stronger at the end of the evolution.

     

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