This chapter contains information relating to turbomachinery modeling implemented as beta features in Ansys Fluent 2024 R2.
- 22.1. Using Mixing-Plane Interface with Influence Coefficient Method (ICM) in Aerodynamic Damping Analysis
- 22.2. Periodic Motion Fast Mesh Smoothing
- 22.3. Efficiency Calculations
- 22.4. Blade Film Cooling Additional Hole Shapes
- 22.5. Particle Tracking Across General Turbo Interfaces
- 22.6. Turbo Create Zone/Interfaces Highlighting
- 22.7. Blade Flutter Analysis - CFX Profile Support
- 22.8. General Turbo Interface with Lip Feature
- 22.9. Point Surfaces that Move with the Mesh
- 22.10. References