Keywords
CFD, reaction control system thrusters, multiphase flow, Eulerian-Lagrangian, Lagrangian multiphase, reacting flow
Abstract
In the current age of space exploration, the push to reach further to deep space presents a greater need for analysis and verification and validation of rocketry components in the space environment. Due to the nature of space, firings of rocket thrusters in space is a multi-regime problem. With the low density, pressure, and temperature of the environment, the resultant plume structure, seeded with unburnt fuel droplets, extends up to multiple orders of magnitude in distance as compared to a plume structure in the Earth’s atmosphere. The frozen droplets, or particles, create concerns including surface contamination and erosion, calling a cause for study and model development to understand particle behavior in this multi-regime environment. This work intends to develop a model to analyze and understand multiphase flow and particle behavior in this environment utilizing the lower fidelity, but more computationally efficient, RANS turbulence modeling. Particle properties are compared against a regime-defining parameter to understand the trends in behavior. Finally, the work closes out on a preliminary look into implementing fully reacting flow chemistry for the multiphase flow. These results and progress are promising in developing an efficient model that may be integrated into a hybrid model to better predict particle behavior and dispersion in this multi-regime environment.
Completion Date
2024
Semester
Summer
Committee Chair
Kinzel, Michael
Degree
Master of Science in Mechanical Engineering (M.S.M.E.)
College
College of Engineering and Computer Science
Department
Mechanical and Aerospace Engineering
Degree Program
Mechanical Engineering - Thermofluids
Format
application/pdf
Identifier
DP0028481
URL
https://purls.library.ucf.edu/go/DP0028481
Language
English
Release Date
8-15-2024
Length of Campus-only Access
None
Access Status
Masters Thesis (Open Access)
Campus Location
Orlando (Main) Campus
STARS Citation
Zou, Janice, "A Near Field Lagrangian Particle Modeling for the Multiphase Flow of Reaction Control System Thrusters in Space Environments" (2024). Graduate Thesis and Dissertation 2023-2024. 276.
https://stars.library.ucf.edu/etd2023/276
Accessibility Status
Meets minimum standards for ETDs/HUTs