Abstract

One-dimensional numerical simulations based on hybrid Eulerian-Lagrangian method are performed to study the interactions between propagating shocks and dispersed evaporating water droplets. Two-way coupling for exchanges of mass, momentum, energy and vapour species is adopted for the dilute two-phase gas-droplet flows. Interphase interactions and droplet breakup dynamics are investigated with initial droplet diameters of 30, 50, 70 and 90 {\mu}m under an incident shock wave Mach number of 1.3. Novel two-phase flow phenomena are observed when droplet breakup occurs. First, droplets near the two-phase contact surface show obvious dispersed distribution because of the reflected pressure wave that propagates in the reverse direction of the leading shock. The reflected pressure wave grows stronger for larger droplets. Second, spatial oscillations of the gas phase pressure, droplet quantities (e.g., diameter and net force) and two-phase interactions (e.g., mass, momentum, and energy exchange), are observed in the post-shock region when droplet breakup occurs, which are caused by shock / droplet interactions. Third, the spatial distribution of droplets (i.e., number density, volume fraction) also shows strong oscillation in the post-shock region when droplet breakup occurs, which is caused by the oscillating force exerted on the droplets.

Highlights

  • Shock / droplet interactions are frequently encountered in engineering practice

  • Numerical simulations are performed with hybrid Eulerian-Lagrangian approach to investigate the two-phase interactions between propagating shock waves and evaporating water droplets proceed with breakup

  • One-dimensional numerical simulations are conducted to study the intersections between the propagating shocks and dilute evaporating water droplets

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Summary

Introduction

Shock / droplet interactions are frequently encountered in engineering practice. Examples are the high-speed vehicle flying through the cloud (droplet diameters of dd,0 = 1-100 μm) or rain (dd,0 = 100-10,000 μm) [1] and the liquid jet of hydrocarbon fuels (dd,0 = 10-200 μm) in scramjet engines [2]. Numerical simulations are performed with hybrid Eulerian-Lagrangian approach to investigate the two-phase interactions between propagating shock waves and evaporating water droplets proceed with breakup.

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