24th Congress of International Council of the Aeronautical Sciences, 29 August-3, September 2004, Yokohama, Japan
Paper ICAS 2004-7.5.R.2

DEVELOPMENT OF ICE ACCRETION AND ANTI-ICING SYSTEM SIMULATION CODE

S. Nishio, S. Kato
Kawasaki Heavy Industries, Ltd., Japan

Keywords: ice accretion, anti-icing, simulation code

This simulation code calculates flow field, collection efficiency, surface temperature, water mass flow rate, and ice shapes of a two dimensional airfoil, based on a flight condition and meteorological condition. In this paper, the overview and validation results of this code are presented.

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