Simulation of Reduction of Shock-Induced Boundary Layer Separation (Workshop)

This workshop will demonstrate how to set up and simulate problems of boundary layer aspiration arising in internal and external high speed supersonic aerodynamics.

Learning Outcomes:

Following completion of this course, you will be able to:

• Simulate the baseline case i.e., without any bleed. 
• Use source terms to model the boundary layer bleed.

Prerequisites:

• Ansys Fluent Beyond the Basics

Please note: These training materials were developed and tested in the 2023R2 release.