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Embry Riddle Aeronautical University

Liquid Slosh Analysis Using Smoothed Particle Hydrodynamics

Abstract

dc:description.abstract

<p>The purpose of the research described here is to study the implementation of Smoothed Particle Hydrodynamics (SPH) algorithms as an adequate means for propellant slosh simulations in 1g and 0g environments. The dualSPHysics solver has been adapted for propellant slosh simulations. Simulated sloshing liquid frequency and damping ratio data for 1g cases has been compared to existing experiments for both spherical and prismatic container geometries. The 0g case has been studied to determine what further modifications would be required to obtain realistic simulations results. The findings in this research will be used to create a sloshing simulation to determine torques applied to a Cubesat during operations.</p>

Degree

thesis:*
Name thesis:degree_name
Master of Aerospace Engineering
Level thesis:degree_level
Thesis - Open Access
Discipline thesis:degree_discipline
Aerospace Engineering
Year
2014

Author and committee

dc:creator, dc:contributor.*
Author dc:creator
  • Field, Kristopher S.

Subjects

dc:subject × 5

Identifiers

dc:identifier.*
Repository record dc:identifier
https://commons.erau.edu/edt/159
OAI identifier oai:identifier
oai:commons.erau.edu:edt-1158

Chain of custody

source
Harvested from
Embry Riddle Aeronautical University
Base URL
commons.erau.edu/do/oai/
Last updated
2026-07-27
Source record
OAI-PMH GetRecord
citation

Field, Kristopher S.. Liquid Slosh Analysis Using Smoothed Particle Hydrodynamics. Thesis - Open Access thesis, 2014. https://commons.erau.edu/edt/159