Design of high-power synthetic jet actuator and its flowfield investigation

Yan Ming Liu*, Bao Guo Wang, Shu Yan Liu

*Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

2 Citations (Scopus)

Abstract

The flowfields surrounding a high-power synthetic jet actuator was simulated numerically in detail. To seek for the novel active-flow-control method, optimization design was also carried out to improve the controlling ability and efficiency. With the invariable model and concerned parameters, the actuator becomes more desirable as the rotating speed increases. Average velocity and maximal velocity at the actuator exit increase as the piston displacement enlarges, which show that the actuator is more efficient. The length of exit section needs optimization. The actuator does not always exhibit good performance with the narrower exit. In the actual design, the various factors need to be considered.

Original languageEnglish
Pages (from-to)552-556
Number of pages5
JournalTuijin Jishu/Journal of Propulsion Technology
Volume29
Issue number5
Publication statusPublished - Oct 2008

Keywords

  • Exit velocity
  • High-power actuator
  • Optimum design
  • Vortex pair

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