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