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 2006-0993 Effects of Continuum Breakdown on Hypersonic Aerothermodynamics
AIAA 2006-0920 Boundary Layer Stability Analysis of Mars Science Laboratory Aeroshell
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
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
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