Effects of Chemistry in Nonequilibrium Hypersonic Flow Around Blunt Bodies
High-Speed Schlieren Analysis of Retropropulsion Jet in Mach 10 Flow
Numerical Simulation of Stagnation Line Nonequilibrium Airflows for Reentry Applications
Modeling Heat-Shield Erosion due to Dust Particle Impacts for Martian Entries
Study on Heating Strategies of Nose Cone Electrothermal Anti-Icing
Investigation of Martian-Dust Drag and Heat Transfer for Mars Sample Return Mission
Investigations of Base Thermal Environment on Four-Nozzle Liquid Launch Vehicle at High Altitude
Tool for Rapid Transient Transpiration-Cooled Reentry Simulation
Assessment of Limiting Processes of Numerical Schemes on Hypersonic Aeroheating Predictions
Molecular-Dynamics-Derived Gas–Surface Models for Use in Direct-Simulation Monte Carlo
Study of the Liquid Breakup Process in Solid Rocket Motor
Influence of Single Roughness Element on Hypersonic Boundary-Layer Transition of Cone
Radiative Heating During Mars Science Laboratory Entry: Simulation, Ground Test, and Flight
Study of Laminar Forced Convection Heat Transfer for Dimpled Heat Sinks
Aeroelastic Analysis of Pinched Panels in Supersonic Flow Changing with Altitude
Experimental and Numerical Study of Cooling Gas Injection in Laminar Supersonic Flow
Prediction of Nonequilibrium Air Plasma Radiation Behind a Shock Wave
Characterization of Structural Response to Hypersonic Boundary-Layer Transition