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Ansys Fluent-Airfoil – unexpected results

    • LindaC
      Subscriber

      Hi to everybody,


      I am new in Ansys. I wanted to ask two questions:



      • If I chose pressure-far-field for two horizontal sides (upper and lower boundaries of the domain, in Fluent they are called free2) I cannot put Mach Number equal to zero: "Error at Node 0: Mach number at Pressure Far-Field boundary should not be set to zero.";

        •    Why I cannot put a Mach number of 0?



      • If I put a very low number for Mach number I get the result in the picture attached, which is technically wrong;

        •    Do you know I get this kind of strange results?




       



       


      Thank you.


      Linda

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