Flow over an Airfoil NACA 2412

In this project, you will be creating the geometry and setting up the cases for different angle of attacks in Converge Studio. And then simulating to analyze the drag and lift force experienced by an Airfoil at different angle of attacks.

  • Duration : 1 Month
  • Domain : MECHANICAL ENGINEERING, AUTOMOTIVE ENGINEERING, MATERIALS ENGINEERING, AEROSPACE ENGINEERING, AERONAUTICAL ENGINEERING
  • Benefits : In this project, you will be creating the geometry and setting up the cases for different angle of attacks in Converge Studio. And then simulating to analyze the drag and lift force experienced by an Airfoil at different angle of attacks.
  • Price : 30000
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