U of M | CoE | Aerospace
Nonequilibrium Gas and Plasma Dynamics Group University of Michigan

• Research
  
  
• Electric Propulsion
• Spacecraft Propulsion
• Hypersonics
• Ablation
• Completed Projects
  
  
• Publications
• People

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Spacecraft Propulsion

• Electric Propulsion
  • Ion Thrusters
  • Hall Thruster Clusters
• Rocket Exhaust Particles

Hypersonics

• Hypersonic Interaction Flows
• Sharp Leading Edges

Transitional Flow

• Computational Analysis of TOMEX Flows

Nonequilibrium Plasma

• Unified Code for Nonequilibrium Plasma Systems

Materials Processing

• Physical Deposition of YBCO
• Physical Deposition of Titanium
• Supersonic Molecular Beams for Thin Film Deposition
• Plasma Etching of Semi-conductors

MEMS Flows

• Low-Speed Rarefied Flow Over Airfoils