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Title:CHAOS: A multi-GPU PIC-DSMC solver for modeling gas and plasma flows
Author(s):Jambunathan, Revathi
Director of Research:Levin, Deborah A.
Doctoral Committee Chair(s):Levin, Deborah A.
Doctoral Committee Member(s):Hwu, Wen-Mei; Chew, Huck Beng; Stephani, Kelly A.
Department / Program:Aerospace Engineering
Discipline:Aerospace Engineering
Degree Granting Institution:University of Illinois at Urbana-Champaign
Degree:Ph.D.
Genre:Dissertation
Subject(s):PIC
DSMC
Forest of Octree
GPU
CUDA
MPI
Morton encoding
linearization
permeability
porous media
plasma plume
neutralization
electron kinetics
charge-exchange collisions
ion backflow
Abstract:Numerical modeling of gas and plasma-surface interactions is critical to understanding the complex kinetic processes that dominate the extreme environments of planetary entry and in-space propulsion. However, simulations of these systems that evolve over multiple length- and time-scales is computationally expensive. Until recently, approximations were used to keep computational costs tenable, which in turn, increased the uncertainty in predictions and offered limited insights into the micro-scale flow properties and electron kinetics that dominate the macroscale processes. The need to perform high-fidelity physics-based gas and plasma simulations has led to the development of a three-dimensional, multi-GPU, Particle-in-cell (PIC)-direct simulation Monte Carlo (DSMC) solver called Cuda-based Hybrid Approach for Octree Simulations (CHAOS) that is presented in this work. This computational tool has been applied to candidate PICA-like TPS materials that consist of an irregular porous network of fibers to allow high-temperature boundary layer gases as well as pyrolysis by-products to penetrate in and flow out of the material. Quantifying bulk transport properties of these materials is essential for accurate prediction of the macroscopic ablation rate. The second application that CHAOS is being used with is the modeling of ion thruster plumes that consist of fast beam ions and slow neutrals that undergo charge-exchange (CEX) reactions to produce slow ions and fast neutrals. These slow CEX ions are strongly influenced by the electric field induced between the ion plume and the thruster surface, resulting in a backflow of ions towards the critical solar panel and thruster surfaces. Three backflow quantities, namely, ion flux, incidence angle, and incidence energy affect the macroscopic sputtering rate of the solar panel surfaces over extended operational times and are predicted from the PIC-DSMC simulations.
Issue Date:2019-01-23
Type:Text
URI:http://hdl.handle.net/2142/104740
Rights Information:Copyright 2019 Revathi Jambunathan
Date Available in IDEALS:2019-08-23
Date Deposited:2019-05


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