Cannot get definitive solution

    • bilal ojaily

      Hi !

      I am tring to calculate lift and drag coefficients for drawn wing in chord=0.102m and length=0.203m at 10m/s velocity in sea level standart, but I cant get a definitive solution, continuously the iteration values change untile 5000 iteratios like this photo.
      How can I solve this problem?

    • Rob
      Ansys Employee

      Why do you think you've not got the right answer after 5000 iterations? 

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