Transonic / supersonic flows

A new feature still under development allows the kinetic solver to model unsteady transonic and supersonic flows at arbitrary Mach numbers. The solver is able to capture shock waves and model fully compressible flow.

Advanced modeling

Advanced modeling involving moving parts allows the simulation of varying conditions such as aircraft maneuverability, weapon deployment or flow around rotor blades.

High lift configurations

The solver is robust even for the analysis of high lift configurations and stall angle.

XFlow's tolerance of complex geometries allows the analysis of the full aircraft geometry.