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ANSYS CFX – NACA Airfoil 4412 – Unstructured Mesh


The simulation of a NACA Airfoil is one of the most common however here we teach you something different: how to import points from your own airfoil and how to create an unstructured mesh easily (does not require high computational cost). You will also learn the steps to follow to develop any simulation.
Do you prefer FLUENT? We also have a tutorial in FLUENT click here.




Download: NACA 4412

PART 1

PART 2




PART 3

PART 4




Readers Comments (10)

  1. Hello! Cool post, amazing!!!

    Reply
  2. Im really like your video thank you.

    Reply
  3. Hello, thanks for this great tutorial. However, I can’t find the text file. Where can I find it?

    Reply
  4. Hey, Thanks for the tutorial! But I have a question, why are you using sweep method for meshing? Thanks!

    Reply
  5. Hi autor,
    first of all thanks for all your afforts.
    I dowloaded naca4412.txt file. but it’s coordinates data are not same as you drawed it on DesignModeler. the points does not seems like airfoil.

    did you make some updaqtes on text file before importing to DesignModeller ?

    Thanks a lot

    Reply

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