AIAA-2019-3260: Simulation of the Schiaparelli Entry and Comparison to Aerothermal Flight Data
Computational Aerothermodynamic Environments for the Mars 2020 Entry Capsule (AIAA 2018-3116)
Impact of Non-Tangent-Slab Radiative Transport on Flowfield-Radiation Coupling (AIAA 2017-1371)
Development of a Radiative Heating Margin Policy for Lunar Return Missions (AIAA 2017-1370)
Backshell Radiative Heating on Human-Scale Mars Entry Vehicles (AIAA 2017-4532)
On the Development of a New Nonequilibrium Chemistry Model for Mars Entry (AIAA 2017-1372)
State-to-State Modeling of CO for Mars Entry Applications (AIAA 2015-0476)