Ansys CFX – NACA 0012 with Angle of Attack (AOA)

Written by cfd.ninja

March 11, 2020

In this tutorial you will learn to simulate a NACA Airfoil (0012) with Angle of Attack (AOA) using ANSYS CFX. First, we will import the points of the NACA profile and then we will generate the mesh using an unstructured mesh in Ansys Meshing. You can download the file in the following link.

"

We share the  tutorial NACA 4412 using ANSYS Fluent.

Related Articles

Ansys Meshing | Inflation

Ansys Meshing | Inflation

In this tutorial, you will learn to use the Inflation tool in Ansys Meshing to control the boundary layer mesh near walls for more accurate CFD simulations.

Stay Up to Date With The Latest News & Updates

Join Our Newsletter

Subscribe to receive emails with detailed information related to the CFD.

Follow Us

Subscribe to our social networks to receive notifications about our new tutorials