Journal of Shanghai Jiaotong University ›› 2018, Vol. 52 ›› Issue (8): 924-929.doi: 10.16183/j.cnki.jsjtu.2018.08.007

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Experimental Study on the Anti-Icing Performance of Plasma Jet I. Parametric Analysis of DBD-PA and Verification on the Anti-Icing Performance

ZHAO Binbin,DONG Wei,LIU Juan,ZHANG Yi   

  1. 1. School of Mechanical Engineering, Shanghai Jiao Tong University, Shanghai 200240, China; 2. CFTC, Commercial Aircraft Corporation of China, Ltd., Shanghai 200232, China; 3. SACSC, Commercial Aircraft Corporation of China, Ltd., Shanghai 200240, China
  • Received:2017-04-06

Abstract: The anti-icing performance of plasma jet fixed on NACA0012 wing model is studied in icing wind tunnel. A plasma jet actuator is designed and installed on the wing model surface, and thermocouples are cleverly embedded beneath the actuator to detect the anti-icing effect. A parametric analysis is performed to investigate the relationship of the anti-icing performance with voltage and frequency, respectively, and the anti-icing effect of plasma jet above insulated electrode is verified.

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

CLC Number: