Keywords
Shock tube, water droplet, droplet deformation, displacement, drag coefficient, acoustic levitation, droplet injection
Abstract
Water droplet breakup in high-speed flow is a relatively popular experimental study to analyze breakup mechanisms. There is a plethora of experiments performed at low Mach number and low Weber number, but studies with higher speed flows and higher Weber numbers are less common. In this study, water droplet breakup is assessed using high-speed shock waves (Mach 2.3-above Mach 5) in a shock tube. Multiple methods are used to introduce droplets, and multiple different water purity levels are considered. An assessment was made into whether cavitation played a role in the breakup process physically, as this has been a budding area of research to describe the underlying mechanisms behind droplet breakup. Additionally, a novel method of droplet introduction in a shock tube was attempted utilizing an acoustic levitation device in the shock tube at pressures below atmospheric. Statistical analysis is also performed to determine droplet predictability and the reliability of the data. Droplets are recorded using a high-speed camera recording at framerates from approximately 750,000 to 5 million frames per second. Conclusions are made as to breakup mechanisms at play, which droplet introduction method works best for producing high quality data, and how accurately models used predict breakup and other characteristics of the droplets.
Completion Date
2025
Semester
Summer
Committee Chair
Vasu, Subith
Degree
Doctor of Philosophy (Ph.D.)
College
College of Engineering and Computer Science
Department
Department of Mechanical and Aerospace Engineering
Format
Language
English
Release Date
2-15-2026
Document Type
Dissertation
Campus Location
Orlando (Main) Campus
Subjects
Fluid dynamics--Research; Shock waves--Experiments; Hydrodynamics--Research; Cavitation--Research; Photography, High-speed--Scientific applications
STARS Citation
Briggs, Sydney M., "On High-Speed Breakup of Water Droplets Behind High Mach Number Shocks" (2025). Graduate Thesis and Dissertation post-2024. 552.
https://stars.library.ucf.edu/etd2024/552
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