Aeroheating Analysis for the Afterbody of a Titan Probe
AIAA 2006-0382 A Code Calibration Study for Huygens Entry Aeroheating
AIAA 2006-0386 Viking Afterbody Heating Computations and Comparisons to Flight Data
AIAA 2006-0388 Uncertainty Analysis of Aeroheating Predictions for Titan Entries
AIAA 2006-0920 Boundary Layer Stability Analysis of Mars Science Laboratory Aeroshell
AIAA 2006-0993 Effects of Continuum Breakdown on Hypersonic Aerothermodynamics
CFD Simulations in Support of Shuttle Orbiter Contingency Abort Aerodynamic Database Enhancement
Computational Fluid Dynamics for Winged Re-entry Vehicles at Hypersonic Conditions
Development of the Mars Science Laboratory Heatshield Thermal Protection System
Modeling and Experimental Validation of CN Radiation Behind a Strong Shock Wave
Modeling of Stardust Entry at High Altitude, Part 1: Flowfield Analysis
Shuttle orbiter contingency abort aerodynamics, II: Real-gas effects and high angles of attack
Sizing and Margins Assessment of Mars Science Laboratory Aeroshell Thermal Protection System
THE IMPACT OF FLOWFIELD-RADIATION COUPLING ON AEROHEATING FOR TITAN AEROCAPTURE