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

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Search Completed | Title | Experimental study of an anti-icing method over an airfoil based on pulsed dielectric barrier discharge plasma
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Y. TIAN et al.
1. Thomas SK, Cassoni RP. Aircraft anti-icing and de-icing tech- niques and modeling. J Aircr 1996;33(5):841–54.
2. Civil Aviation Authority. Aircraft icing handbook. 1st ed. New Zealand: Safety Education and Publishing Unit; 2000. p. 1–4.
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. Bragg MB, Gregorek GM, Lee JD. Airfoil aerodynamics in icing
conditions. J Aircr 1985;23(1):76–81.
6. Bragg MB, Broeren AP, Blumenthal LA. Iced-airfoil aerodynam-
ics. Prog Aerosp Sci 2005;41(5):323–62.
7. Jr Coffman HJ. Review of helicopter icing protection systems.
Reston: AIAA; 1983. Report No.: AIAA-1983-2529.
8. Browm AP. The aerodynamic effects of engine power on lift and drag of a turbo-propeller transport aeroplane in light rime icing
accretion. Reston: AIAA; 2004. Report No.: AIAA-2004-4874.
9. Veres JP, Jorgenson Philip CE. Modeling commercial turbofan engine icing risk with ice crystal ingestion. Reston: AIAA; 2013.
Report No.: AIAA-2013-2679.
10. Venkataramani KS, Plybon RC, Holm RG, Krup BR. Aircraft
engine icing model. Reston: AIAA; 2008. Report No.: AIAA-
11. Ross R. Analysis of an airplane windshield anti-icing system.
Reston: AIAA; 1982. Report No.: AIAA-1982-1372.
12. Gates EM, Thompson WC. Simulated atmospheric rime icing of some wind speed sensors. J Atmos Oceanic Technol 1986;3
13. Louchez PR, Bernardin S, Laforte JL. Physical properties of
aircraft de-icing and anti-Icing fluids. Reston: AIAA; 1998. Report
No.: AIAA-1998-0575.
14. Rosenthal HA, Nelepovitz DO, Rockholt HM. De-icing of
aircraft turbine engine inlets. Atlantic: FAA Technical Center;
1988. Report No.: DOT/FAA/CT-87/37.
15. Li B. Brief survey of deicing/anti-icing fluid and techniques for
aircraft. Cleaning Word 2008;28(1):26–31 [Chinese].
16. Pourbagian M, Habashi WG. Surrogate-based optimization of electrothermal wing anti-icing systems. J Aircr 2013;50
17. Mohseni M, Amirfazli A. A novel electro-thermal anti-icing
system for fiber-reinforced polymer composite airfoils. Cold Reg Sci Technol 2013;87(3):47–58.
18. 19.
21. 22.
23. 24. 25.
30. 31.
Martin CA, Putt JC. Advanced pneumatic impulse ice protection system (PIIP) for aircraft. J Aircr 1992;29(4):714–6. Sommerwerk H, Horst P, Bansmer S. Studies on electro impulse de-icing of a leading edge structure in an icing wind tunnel. Reston: AIAA; 2016. Report No.: AIAA-2016-3441.
Yeong YH, Loth Eric, Sokhey J, Lambourne A. Ice adhesion strength on hydrophobic and superhydrophobic coatings. Reston: AIAA; 2014. Report No.: AIAA-2014-2063.
Cao L, Jones AK, Sikka VK. Anti-icing superhydrophobic coatings. Langmuir ACS J Surf Colloids 2009;25(21):12244–8. Kulinich SA, Fsrhadi S, Nose K, Du XW. Superhydrophobic surface: are they really ice-repellent? Langmuir ACS J Surf Colloids 2011;27(1):25–9.
Farhadi S, Farzaneh M, Kulinich SA. Anti-icing performance of superhydrophobic surfaces. Appl Surf Sci 2011;257(14):6264–9. Wang JJ, Choi KS, Feng LH. Recent developments in DBD plasma flow control. Prog Aerosp Sci 2013;62(4):52–78.
Corke TC, Enloe CL, Wilkingson SP. Dielectric barrier discharge plasma actuators for flow control. Annu Rev Fluid Mech 2009;42 (1):505–29.
Joussot R, Hong D, Rabat H. Thermal characterization of a DBD plasma actuator: dielectric temperature measurements using infrared thermography. Reston: AIAA; 2010. Report No.: AIAA-2010-5102.
Stanfield SA, Menart J, Jr Dejuseoh C. Rotational and vibrational temperatures for a dielectric barrier discharge in air using emission spectroscopy. AIAA Journal 2009;47(5):1107–15.
Dong B, Bauchire JM, Pouvesle JM. Experimental study of a DBD surface discharge for the active flow control of subsonic airflow. J Phys D Appl Phys 2008;41(15):1525–8.
Erfani R, Zare-Behtash H, Kontis K. Plasma actuators: influence of dielectric surface temperature. Exp Therm Fluid Sci 2012;42 (5):258–64.
Qiu XG, Han FH. Anti-icing system of aircraft. Beijing: National Defense Industry Press; 2004 [Chinese].
Kriegseis J, Mo ̈ ller B, Grundmann S. Capacitance and power consumption quantification of dielectric barrier discharge (DBD) plasma actuators. J Electrostat 2011;69(4):302–12.
Ma H, Zhang DL, Meng FX. Experiment of electro-thermal anti- icing on a composite assembly. Acta Aeronaut Astronaut Sin 2013;34(8):1846–53 [Chinese].
Fortin G, Adomou M, Perron J. Experimental study of hybrid anti-icing system combining thermalelectric and hyperpholic coatings. SAE Int J Aerosp 2011;38(3):281–3.

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