Strongly Coupled Computation of Material Response and Nonequilibrium Flow for Hypersonic Ablation
Strongly Coupled Computation of Material Response and Nonequilibrium Flow for Hypersonic Ablation
Axisymmetric Fully 2D Hybrid-PIC Model for Hall Thrusters (AIAA 2018-4811)
Effectiveness of Thermionic Emission for Cooling Hypersonic Vehicle Surfaces (AIAA 2018-1714)
Reduced Reaction Mechanism for Rocket Nozzle Ablation Simulations (AIAA 2017-3682)
Unsteady Simulations of Rocket Plume Expansions in Geostationary Earth Orbit
Unsteady Simulations of Rocket Plume Expansions in Geostationary Earth Orbit