Experimental Study on the Anti-Icing Performance of Plasma Jet
 II. Comparison of Anti-Icing Performance Using
 Streamwise and Spanwise DBD-PA

doi:10.16183/j.cnki.jsjtu.2018.11.016

Abstract

Abstract: The anti-icing performances of streamwise and spanwise plasma jet actuators fixed on NACA0012 are compared in the icing wind tunnel. Streamwise and spanwise actuators are designed and installed on the model surface, and thermocouples are specially embedded beneath the actuator to detect the anti-icing effects. Experiment results indicate that the spanwisely installed actuator cannot generate plasma jets due to the installation position being above the exposed electrode, leading to icing and thus a poor performance of anti-icing, while the streamwisely installed actuator realizes anti-icing by contrast.

Key words: anti-icing, plasma jet, icing wind tunnel, dielectric-barrier-discharge, actuator

CLC Number:

V 211.3

ZHAO Binbin,DONG Wei,ZHANG Yi. Experimental Study on the Anti-Icing Performance of Plasma Jet II. Comparison of Anti-Icing Performance Using Streamwise and Spanwise DBD-PA[J]. Journal of Shanghai Jiaotong University, 2018, 52(11): 1532-1536.

References

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Experimental Study on the Anti-Icing Performance of Plasma Jet II. Comparison of Anti-Icing Performance Using Streamwise and Spanwise DBD-PA

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