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De-icing of wing

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Hi,
I'm doing simulation of deicing of wing due to heating up sections of the leading edge of the wing. However, when I go through all the boundary set up and run the solution. I get an error:

Undefined value found.
- Detail: NaN or Inf found when solving linear system using SOR.

I've attached my file to this, please help me eliminate this if possible. Few possibilities of error might be at how my velocity is set up: i want it in -y direction but I'm not sure if that will cause any problems or not.

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