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dc.contributor.advisorGerakis, Alexandros
dc.contributor.advisorHara, Kentaro
dc.creatorMansour, Adnan
dc.date.accessioned2020-08-26T18:58:55Z
dc.date.available2020-08-26T18:58:55Z
dc.date.created2019-12
dc.date.issued2019-11-07
dc.date.submittedDecember 2019
dc.identifier.urihttps://hdl.handle.net/1969.1/188773
dc.description.abstractThe growth of plasma applications in industrial and scientific settings has led to the need for consistent computational plasma models. The multi-scale, highly nonlinear physics involved in plasma processes creates a challenging environment for computational modelling. Different combinations of assumptions and approximations are utilized to ease the computational burden associated with plasma fluid models. The goal of this research work is to document and describe in detail the theory, numerical modelling and results of two separate projects in plasma modelling. The first project is a multi-species one-dimensional model of ablating carbon arc discharge, namely for the synthesis of carbon nanotubes. It focuses on the development of chemical and physical models, as well as the derivation of multiple governing equations and boundary conditions used. Governing equations are solved for eleven species, and the chemical composition of the arc is dynamically updated. Multiple parameters are varied and benchmarked against each other. Numerical results are presented from published work and compared to experimental results, with which they have shown good agreement. The second project describes the development of numerical methods for a one-dimensional non-neutral drift-diffusion plasma model for Hall-effect thrusters. The overarching purpose of the project is to investigate the anomalous electron transport observed in experiments, yet to be captured by numerical models, by removing general assumptions one step at a time. The end goal is to have a simulation that does not rely on artificially introducing the empirical anomalous transport coefficient to achieve levels of electron mobility observed in experimental setups. This project removes the quasi-neutral assumption and solves for the electrons as a separate species, utilizing the drift-diffusion model. It focuses on the implementation of several numerical schemes that are developed to help alleviate the severe timestep size restrictions associated with non-neutral plasma models. Results are compared with results from neutral simulations as well as other non-neutral models in development.en
dc.format.mimetypeapplication/pdf
dc.language.isoen
dc.subjectPlasma modellingen
dc.subjectablating arc dischargeen
dc.subjectcarbon nanomaterial synthesisen
dc.subjectHall-effect thrusteren
dc.subjectplasma propulsionen
dc.subjectlow temperature plasmaen
dc.titleLow Temperature Plasma Modelling Techniques for Arc Discharge and Hall-Effect Thrustersen
dc.typeThesisen
thesis.degree.departmentAerospace Engineeringen
thesis.degree.disciplineAerospace Engineeringen
thesis.degree.grantorTexas A&M Universityen
thesis.degree.nameMaster of Scienceen
thesis.degree.levelMastersen
dc.contributor.committeeMemberStaack, David
dc.type.materialtexten
dc.date.updated2020-08-26T18:58:56Z
local.etdauthor.orcid0000-0002-6446-212X


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