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Critical Reynolds number and limit of the laminar model

    • Giorgio Casulli

      I'm studying the laminar flow on a NACA 4412 profile and I was wondering which is the critical reynolds number for this case, in particular i would like to know which is the max reynolds number at which the laminar model is able to give reliable results.

      Any ideas?

    • Rob
      Forum Moderator

      We can't really answer that. Flow separation, mesh, time step size, wing shape etc will all play a role, so it's not a case of giving a single value.

      If you run the laminar model at what point don't you get data that agree with publications? 

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