Abstract
In this work, a Coupled Level Set and Volume of Fluid (CLSVOF) solver using a geometric advection scheme is proposed and implemented. By improving droplet advection fidelity compared to existing methods, a reduction in the cost of characterising liquid breakup can be achieved, contributing to better fuel atomisation in propulsion systems. Validation of the solver is performed using a simple bubble advection case, where improved performance and field error compared to an algebraic CLSVOF implementation is noted. Verification is performed by replicating a planar airblast atomiser experiment. Here, good agreement with experimental results on breakup dynamics is observed along with clear improvement in droplet advection fidelity compared to algebraic methods. A comparison with a geometric VoF solver shows similar performance and accuracy due to the high Weber number flow. The isoCLSVOFFoam solver presented in this work presents a promising alternative to existing CLSVOF codes, particularly when good droplet resolution and surface tension modelling are required.
| Original language | English |
|---|---|
| Title of host publication | 59th 3AF International Conference on Applied Aerodynamics |
| Publisher | Association Aeronautique et Astronautique de France |
| Number of pages | 9 |
| DOIs | |
| State | Published - 24 Mar 2025 |
Keywords
- Level set method
- VOF
- atomization
- CFD (Computational Fluid Dynamics)
- multiphase flow
- combustion
- simulation
- Fuel injection
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