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Multi-GPU PIC solver for modeling of ion thruster plasma plume
Revathi Jambunathan
,
Deborah A. Levin
Aerospace Engineering
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Dive into the research topics of 'Multi-GPU PIC solver for modeling of ion thruster plasma plume'. Together they form a unique fingerprint.
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Keyphrases
Multi-GPU
100%
Electron Source
100%
Ion Thruster
100%
Plasma Plume
100%
Plume Dynamics
75%
Plume
50%
Dirichlet Boundary Condition
50%
Ion Source
25%
Electron Velocity
25%
Xenon
25%
Electrostatic Trapping
25%
Source Location
25%
Electron Population
25%
Dynamic Kinetics
25%
Neutral State
25%
Neumann Boundary Condition
25%
Xenon Ions
25%
Three-dimensional Particle-in-cell
25%
Particle-in-cell Simulation
25%
Quasi-neutral
25%
Electron Kinetics
25%
Mesothermal
25%
Neutralizer
25%
Engineering
Graphics Processing Unit
100%
Dirichlet Boundary Condition
100%
Thruster
100%
Plasma Plume
100%
Ion Source
50%
Electron Velocity
50%
Neumann Boundary Condition
50%
Boundary Condition
50%
Physics
Boundary Condition
100%
Electron Source
100%
Blood Plasma
100%
Electrostatics
50%
Ion Source
25%
Earth and Planetary Sciences
Boundary Condition
100%
Electron Source
75%
Xenon
50%
Neutralizers
25%
Material Science
Xenon
100%