25th Congress of International Council of the Aeronautical Sciences, 3 - 8 September 2006, Hamburg, Germany
Paper ICAS 2006-P6.4

THE DESIGN OF A SERIES OF ELECTROTHERMAL ICE PROTECTION SYSTEMS

Y. Wang, G. L. Luo, G. P. Lin*
Beihang Univ.& BATRC, China; *Beihang Univ., China

Keywords: aircraft, anti-icing, numerical simulation, multiphase flow

A series of electrothermal ice protection systems, which is adapted to composite radome, have been designed mainly based on computational simulation method. The computational accuracies of 3D droplets impingement and the demands of conjugate heatflux are verified by the experimentations and authoritative reports. Review and prospect are also included.

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