Volume 35 Issue 11
Nov.  2020
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YANG Shengke, GUO Qiling, LUO Zhenbing. Experiment on airfoil runback ice protection based on synthetic jet,[J]. Journal of Aerospace Power, 2020, 35(11): 2364-2370. doi: 10.13224/j.cnki.jasp.2020.11.013
Citation: YANG Shengke, GUO Qiling, LUO Zhenbing. Experiment on airfoil runback ice protection based on synthetic jet,[J]. Journal of Aerospace Power, 2020, 35(11): 2364-2370. doi: 10.13224/j.cnki.jasp.2020.11.013
shu

Experiment on airfoil runback ice protection based on synthetic jet,

doi: 10.13224/j.cnki.jasp.2020.11.013
  • 1.

    Key Laboratory of Icing and Anti/De-Icing,China Aerodynamics Research and Development Center,Mianyang Sichuan 621000,China

  • 2.

    College of Aerospace Science and Engineering,National University of Defense Technology,Changsha 410073,China

  • Received Date: 2020-05-11
  • Publish Date: 2020-11-28
    Abstract
  • A hybrid ice protection method combining thermoelectric systems and synthetic jet actuators was designed to solve the problem of runback ice. In this method, the thermoelectric system was arranged on the leading edge of the wing to prevent the supercooled water droplets from freezing. The synthetic jet slot was located downstream the thermoelectric system to change the trajectory of runback water. The effects of the liquid water content, the incoming flow and the velocity of synthetic jet on the anti-icing performance of the hybrid ice protection system were studied in the icing wind tunnel. The results showed that the hybrid ice protection method could keep both the leading-edge and downstream regions free from icing.

     

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