Radiative Heating During Mars Science Laboratory Entry: Simulation, Ground Test, and Flight
Thermal Analysis and Testing of Nonrotating Cone with Hot-Air Anti-Icing System
Characterization of Structural Response to Hypersonic Boundary-Layer Transition
Modeling Heat-Shield Erosion due to Dust Particle Impacts for Martian Entries
Numerical Simulation of Stagnation Line Nonequilibrium Airflows for Reentry Applications
High-Speed Schlieren Analysis of Retropropulsion Jet in Mach 10 Flow
Investigations of Base Thermal Environment on Four-Nozzle Liquid Launch Vehicle at High Altitude
Hypersonic Boundary-Layer Instability Characteristics on Sharp Cone with Porous Coating
Influence of Single Roughness Element on Hypersonic Boundary-Layer Transition of Cone
Study of the Liquid Breakup Process in Solid Rocket Motor
Tool for Rapid Transient Transpiration-Cooled Reentry Simulation
Hybrid Particle-Continuum Simulations of Hypersonic Flow Over a Hollow-Cylinder-Flare Geometry
Prediction of Nonequilibrium Air Plasma Radiation Behind a Shock Wave
Experimental and Numerical Study of Cooling Gas Injection in Laminar Supersonic Flow
Reverse Design of Ultrasonic Absorptive Coating for the Stabilization of Mack Modes
Assessment of Limiting Processes of Numerical Schemes on Hypersonic Aeroheating Predictions
Molecular-Dynamics-Derived Gas–Surface Models for Use in Direct-Simulation Monte Carlo
Surface Heating and Boundary-Layer Transition on a Hypersonic Inflatable Aerodynamic Decelerator