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The intern has developed a 3D microscopic model to simulate water bead behavior on
hydrophobic and superhydrophobic coatings. The microscopic model developed at Concordia
University which simulates one bead cannot be directly integrated into an aircraft icing panel
code such as CANICE-2D. CANICE-2D approved by Transport Canada has been widely
used at Bombardier Aerospace to simulate aircraft in-flight icing. This is a panel code solving
the flow, the droplet trajectories, ice thermodynamic and the geometry. CANICE-2D can run
cases in few minutes which reduces the time to find the critical icing shape. CANICE-2D
calculates the ice shape by solving the heat and mass transfer equations and the water film
at the surface when glaze ice is formed.
Ali Dolatabadi
Bombardier Aeronautic Inc (Saint-Laurent, QC)
Engineering
Manufacturing; Transportation and warehousing
Concordia University
Accelerate
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