A research project is underway at NASA Lewis to produce a computer code which can accurately predict ice growth under any meteorological conditions for any aircraft surface. The most recent release of this code is LEWICE 1.6. This paper will demonstrate some of the newer capabilities of this code as well as describe each of these advancements in full and make comparisons with the experimental data available. Further refinement of these features and inclusion of additional features continue to be performed on this model.
The Icing Technology Branch at NASA Lewis has been involved in an effort to validate two thermal ice protection codes developed at the NASA Lewis Rese...
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