ANSYS CFX – NACA Airfoil 0012 with Angle of Attack


This is another tutorial on a profile (NACA 0012), however here we change the angle of attack in a very simple way. You can try with other angles and observe the separation of the boundary layer.



Download: NACA 0012













Readers Comments (18)

  1. What about drag and lift coefficients versus reynolds number in a constant angle of attack? It would be a nice tutorial …

    Reply
  2. Greate pieces. Keep writing such kind of information on your blog.
    Im really impressed by it.
    Hi there, You’ve performed a fantastic job. I’ll certainly digg it
    and for my part recommend to my friends. I’m sure they will be benefited from this web site.

    Reply
  3. I respect your work.

    Reply
  4. Interesting thank you for sharing

    Reply
  5. jeffrey turford May 1, 2017 @ 7:06 am

    cool post buddy, thank you for posting

    Reply
  6. Dennis Antoniou May 22, 2017 @ 5:41 am

    Hey body, please help i cant find the txt file to simulate the airfoil.Where can i find! Thanks and congrats for your great work!

    Reply
  7. Where the text file with coordinates bro ? i can’t find it !!!
    please send it to me on

    Reply
  8. Hi,
    Really great tutorials so helpful. Would you have a tutorial of a rotating airfoil so with multiple domains?
    Thank you.
    Regards

    Reply
    • Hi my friend; Thanks
      In this moment I haven’t it, but I hope to do a tutorial about that soon.
      Regards

      Reply

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