City Research Online

Numerical Investigation of the Aerodynamic Droplet Breakup at Mach Numbers Greater Than 1

Stefanitsis, D., Koukouvinis, F. ORCID: 0000-0002-3945-3707, Nikolopoulos, N. and Gavaises, M. ORCID: 0000-0003-0874-8534 (2020). Numerical Investigation of the Aerodynamic Droplet Breakup at Mach Numbers Greater Than 1. Journal of Energy Engineering, 147(1), doi: 10.1061/(ASCE)EY.1943-7897.0000720

Abstract

The present work examines numerically the breakup of water droplets exposed to gas flows at Mach numbers Ma>1, which resemble the ambient conditions encountered in the injection systems of scramjet (supersonic combustion ramjet) engines. A CFD model is utilized which solves the compressible Navier-Stokes equations, the energy equation, the mass conservation in volume fraction form (volume of fluid method) along with two equations of state to model the density variations of the two phases. In addition, a coupled VOF/Lagrange model is employed to capture the appearance of micro-droplets, which are smaller than the smallest grid cell. As a first step, a 2-dimensional planar simulation (water column) is performed at conditions of Ma=1.47 in order to validate the numerical model; its results are compared against published experimental and numerical data. Good agreement is observed for the temporal evolution of droplet shape, the streamwise deformation, the leading-edge displacement as well as the shock wave reflection. Subsequently, the validated model is utilized to perform a 3-D simulation at Ma=1.23, which corresponds to the conditions of previous experimental studies, and its results are compared against the experimental data as well as the results from previous numerical studies, showing good agreement. Furthermore, surface instabilities are observed at the droplet surface initiated by interfacial instabilities due to the shearing effect and the interaction with the shock-wave, pertaining to Kelvin-Helmholtz and Rayleigh-Taylor instabilities, despite the stabilising contribution of surface tension; viscosity effects are found to play an insignificant role.

Publication Type: Article
Additional Information: This material may be downloaded for personal use only. Any other use requires prior permission of the American Society of Civil Engineers. This material may be found at https://ascelibrary.org/journal/jleed9.
Publisher Keywords: Droplet breakup; shock wave; high Mach number; CFD; surface instabilities;
Subjects: Q Science > QC Physics
T Technology > TL Motor vehicles. Aeronautics. Astronautics
Departments: School of Mathematics, Computer Science & Engineering > Engineering > Mechanical Engineering & Aeronautics
Date Deposited: 20 Jul 2020 12:00
URI: https://openaccess.city.ac.uk/id/eprint/24574
[img]
Preview
Text - Accepted Version
Download (1MB) | Preview

Export

Downloads

Downloads per month over past year

View more statistics

Actions (login required)

Admin Login Admin Login