- A CFD code specifically developed for turbomachinery applications. The pre-processor allows for very rapid mesh generation and boundary condition definition. Problem can be set up and ready to run within 5 minutes.
- Specific turbomachinery post processor allows for rapid visualisation as well as summary information on efficiency, head, flow rate, cavitation performance in pumps and broadband noise in fans.
- Fast and accurate solver allowing accurate solutions to be obtained in about 30 min on P4 PC for 350,000 nodes mesh.
- Well validated CFD solver originally developed at Florence University and NASA Lewis with more than 70 peer-reviewed papers.
Design of High Performance Pump Stage
Hydraulic Design Optimisation of a Torque Converter
Design of a 3 Stage Axial LP Turbine for Aeroengine Applications