Morphogenetic modelling of in-flight icing

Measuring and testing – Meteorology – Icing condition

Reexamination Certificate

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C244S13400A

Reexamination Certificate

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06868721

ABSTRACT:
The accretion of ice on an aerodynamic surface is predicted by identifying predetermined atmospheric parameters relevant to ice formation in a particular fluid environment. Then the behaviour of individual fluid elements is simulated based on the identified parameters to create a model of the ice accretion.

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“Simulation of airfoil icing with a novel morphogenetic model”, Krzysztof Szilder, pp. 1-8.
“Development of a shallow-water icing model in Fensap-Ice”, Y. Bourgault, Journal Of Aircraft, vol. 37, No. 4, Jul.-Aug. 2000, pp. 640-646.
“Experimental and computational simulation of in-flight icing phenomena”, R.J. Kind et al., Progress in Aerospace Sciences, 34, 1998, pp. 257-345.

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