Measuring and testing – Meteorology – Icing condition
Reexamination Certificate
2005-03-22
2005-03-22
Swiatek, Robert P. (Department: 3643)
Measuring and testing
Meteorology
Icing condition
C244S13400A
Reexamination Certificate
active
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.
REFERENCES:
patent: 4210021 (1980-07-01), Vykhodtsev et al.
patent: 4732351 (1988-03-01), Bird
patent: 5195046 (1993-03-01), Gerardi et al.
patent: 5585551 (1996-12-01), Johansson et al.
patent: 6347767 (2002-02-01), Holmen
patent: WO 9420819 (1994-09-01), None
“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.
(Marks & Clerk)
Mitchell Richard J.
National Research Council Canada
Swiatek Robert P.
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