Experimental study of an anti-icing method over an airfoil based on pulsed dielectric barrier discharge plasma-Reference-Cited by-同舟云学术

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Experimental study of an anti-icing method over an airfoil based on pulsed dielectric barrier discharge plasma

Published:2018-07 Issue:7 Volume:31 Page:1449-1460
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

TIAN Yongqiang,ZHANG Zhengke,CAI Jinsheng,YANG Leilei,KANG Lei

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference33 articles.

1. Aircraft anti-icing and de-icing techniques and modeling;Thomas;J Aircr,1996

2. Aircraft icing handbook;Civil Aviation Authority,2000

3. Griffiths R, Korkan K. Study of theoretical and wind tunnel results on flight performance degradation due to leading edge rime ice accretion. Reston: AIAA; 1992. Report No.: AIAA-1992-0038.

4. Yi X. Numerical computation of aircraft icing and study on icing test scaling law [dissertation]. Mianyang: Chinese Aerodynamic Research and Development Center; 2007 [Chinese].

5. Airfoil aerodynamics in icing conditions;Bragg;J Aircr,1985

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