| Citation: | Deng Guangzhou, Yang Shunhua, Wang Yanhua, et al. Review of droplet deformation and breakup in supersonic flow induced by shock waves[J]. Journal of Aerospace Power, 2026, 42（X）：20250512 doi: 10.13224/j.cnki.jasp.20250512
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Recent research progress on shock-induced droplet deformation and breakup in supersonic flows was reviewed from the perspectives of droplet breakup dynamics and two-phase physical property effects, near-field shock structures around droplets, turbulence evolution, internal droplet flow, and numerical simulation methods. Existing relevant studies mainly focused on the influences of two-phase physical parameters on breakup modes, the complex shock-wave systems formed during shock–droplet interactions and their characteristics, and the regulatory effects of turbulence evolution on interfacial instability and droplet breakup processes. It is generally recognized that shock-induced droplet breakup is a complex multiscale process jointly governed by aerodynamic forces, interfacial instabilities, and turbulence. However, current studies on the effects of shock waves, turbulence, and related factors on droplet breakup remain largely at a qualitative stage. Future research should be based on cross-scale high-fidelity numerical methods to further strengthen the quantitative characterization of the effects of shock waves and turbulence on droplet breakup and to achieve the decoupling analysis of their respective influences on the breakup process.
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