Atomisation & Spray combustion
High-fidelity prediction of liquid jet breakup, droplet formation, and spray dynamics under complex multiphase, turbulent, and reactive flow conditions across engineering applications
Technical capabilities in MPflow
MPflow provides a unified framework for modelling atomisation and spray processes across regimes, from dense liquid cores to fully dispersed sprays:
- Dedicated multiphase CFD solvers for primary and secondary atomisation
- Interface-resolving methods capturing Rayleigh–Taylor and Kelvin–Helmholtz instabilities
- Natural transition from Eulerian interface tracking & Lagrangian spray modelling
- Fully coupled LES and RANS turbulence modelling for high-fidelity transient flows
- Advanced treatment of:
- Droplet breakup and coalescence
- Evaporation and heat transfer
- Two-way coupling between droplets and carrier phase
- Compatible with OpenFOAM libraries and extended with proprietary MPflow capabilities



Our CFD approach
- High-resolution simulation of liquid jet instability growth and breakup
- Direct modelling of interface deformation under turbulence and shear
- LES-based resolution of transient structures in near-nozzle regions
- Coupled modelling of:
- Primary atomisation (jet breakup)
- Secondary atomisation (droplet fragmentation)
- Accurate prediction of:
- Droplet size distribution (SMD)
- Velocity and temperature fields
- Spray penetration and dispersion
Physics-based ML acceleration
- ML models trained on high-fidelity CFD and experimental datasets
- Surrogate modelling of:
- Breakup regimes
- Droplet size distributions
- Spray evolution dynamics
- Embedded into solver for:
- On-the-fly acceleration of LES/RANS closures
- Rapid prediction of spray characteristics without resolving all scales
- Hybrid CFD–ML framework preserving physical consistency and conservation laws
- Generalisation across:
- Fuels (including cryogenic and reactive fluids)
- Injector geometries
- Operating conditions
Why ML-CFD matters for Atomisation & Spray Combustion
- Simulation time reduced from 8 hours to <1 minute: rapid evaluation of injector and combustion system designs
- 7–10× acceleration with ML-enhanced turbulence modelling (RANS & LES)
- High accuracy (<5–7% deviation) in droplet size, spray angle, and penetration
- Instant exploration of operating conditions, including pressure, temperature, and injection strategies
- Scalable across fuels and geometries, including complex injector configurations
- Reduces experimental campaigns and accelerates development cycles in combustion systems


