Consistent Atomic Oxygen Model for Direct Simulation Monte Carlo Below 1000 Kelvin
Study of the Liquid Breakup Process in Solid Rocket Motor
Radiative Heating During Mars Science Laboratory Entry: Simulation, Ground Test, and Flight
Characterization of Structural Response to Hypersonic Boundary-Layer Transition
Heat Transfer Evaluation on Ice-Roughened Cylinders
Numerical Modeling of Earth Reentry Flow with Surface Ablation
Experimental Study on Pressure Drop of Aluminum-Oxide/Water Nanofluids
Influence of Cooling-Gas Properties on Film-Cooling Effectiveness in Supersonic Flow
Development of a Nonequilibrium Finite-Rate Ablation Model for Radiating Earth Reentry Flows
Vacuum Ultraviolet Spectral Measurements for Superorbital Earth Entry in X2 Expansion Tube
Thermal Analysis and Testing of Nonrotating Cone with Hot-Air Anti-Icing System
Approach for Modeling Rocket Plume Impingement and Dust Dispersal on the Moon
Assessment of Limiting Processes of Numerical Schemes on Hypersonic Aeroheating Predictions
Prediction of Nonequilibrium Air Plasma Radiation Behind a Shock Wave
Acoustic Interferometry and the Calibration Integral Equation Method for Inverse Heat Conduction
Uncertainty Analysis of Radiative Heating Predictions for Titan Entry
Fluidic Control Method for Improving the Self-Starting Ability of Hypersonic Inlets