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  3. I am simulating flow past an airfoil, and I want to evaluate how the drag and the lift are affected by the angle of attack. I was able to get results for 0, 2, 4 and 6 degree angle of attack. However, once I went to 8, 10 and 12 the model did not converge. I am wondering if I am doing something wrong?

I am simulating flow past an airfoil, and I want to evaluate how the drag and the lift are affected by the angle of attack. I was able to get results for 0, 2, 4 and 6 degree angle of attack. However, once I went to 8, 10 and 12 the model did not converge. I am wondering if I am doing something wrong?

Tagged: 18, fluent, fluid-dynamics, General - FLUENT
    • August 25, 2023 at 12:16 pm
      SolutionSolution
      Participant

      Please see attached document for solution. Keywords: angle of attack, airfoil, converge, transient

      Attachments:
      1. 2049274.pdf

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