Discover how you can unlock the future of aerospace engineering in this webinar, which is designed to help you advance comprehensive flow modeling in your aerospace designs.
ABOUT THIS WEBINAR:
In this webinar, we will take a look at the advancements in Ansys Fluent solver capabilities for compressible flows with improved overlap between pressure-based and density-based solvers, defining the use-cases and solver comparison for a transonic free-jet.
We will also provide an introduction to the Mach-Hessian cell adaption technique for resolving shock waves and sonic regions with improved accuracy, without over-refining the entire domain.
DATE: April 29th, 2025
TIME: 2-3 PM EST
LOCATION: Virtual
WHAT YOU WILL LEARN:
- The advancements in Ansys Fluent solver capabilities for compressible flows.
- The improved overlap between pressure-based and density-based solvers.
- An introduction to the Mach-Hessian cell adaption technique for resolving shock waves and sonic regions.
SPEAKER:
