You will learn about the aerodynamic flows CFD using Ansys ICEMCFD and Ansys Fluent
What you'll learn:
What you'll learn:
- You will be able to create airfoil data file from coordinates for ICEMCFD
- You will be to create high quality hexa mesh with boundary layer and Y+ considerations
- How to create three meshes for mesh-independence study
In this course you will learn about the CFDof external aerodynamics. In this course first we will create geometry of airfoil in ICEMCFD and then we will create high quality hexa mesh. After that we will solve this case in Fluent.
You will run case at angle of attack zero and angle of attack 10 and compare results with NASA data for Cp, lift coefficient and drag coefficient.
In future we will introduce more complex problems. Hope to see you soon on course.
