Aircraft Icing Analysis

I have a case where I need to proving icing conditions is not a concern.  I can do a portion of the analysis in house to show that my product freezes and develops ice or does not develop ice when sitting stationary at below freezing temperatures.  What I can't do is show how the aerodynamics of a moving aircraft affect the ability for the product to keep from icing over.  I am curious is there a way to achieve this analysis in Solidworks, and if so would it require Simulation Flow?

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