Numerical simulation and modeling of a liquid jet in supersonic crossflow

In this study, we simulated liquid jets in supersonic crossflow (LJSC) under various inflow Mach numbers using the diffuse interface method. The results show that as the Mach number increases, the liquid jet exhibits reduced penetration and faster fragmentation, accompanied by different breakup modes. A theoretical model was developed to predict the near-field trajectory, which shows good agreement with experimental and numerical data. The proposed primary breakup model can be incorporated into Lagrangian methods to enhance computational accuracy.