Computation of Hypersonic Flows Using the Direct Simulation Monte Carlo Method
State-resolved Characterization of Nitric Oxide Formation in Shock Flows (AIAA 2018-1233)
A PARAMETRIC COMPUTATIONAL STUDY OF BORON TRANSPORT IN HALL THRUSTERS (AIAA 2016-4843)
State-resolved O~2--N~2 Kinetic Model at Hypersonic Temperatures (AIAA 2017-0659)
Simulation of O~2-N Collisions on ab-initio Potential Energy Surfaces (AIAA 2016-1249)
High Fidelity Modeling of Thermal Relaxation and Dissociation of Oxygen (AIAA 2016-0736)
Axisymmetric Fully 2D Hybrid-PIC Model for Hall Thrusters (AIAA 2018-4811)
Effectiveness of Thermionic Emission for Cooling Hypersonic Vehicle Surfaces (AIAA 2018-1714)
Conjugate Analysis of Rocket Nozzle Ablation (AIAA 2017-3351)
Reduced Reaction Mechanism for Rocket Nozzle Ablation Simulations (AIAA 2017-3682)
Computational Analysis of Electron Transpiration Cooling for Hypersonic Vehicles (AIAA 2017-0900)
Limits for Thermionic Emission from Leading Edges of Hypersonic Vehicles (AIAA 2016-0507)