SURVEY PAPERS - Computational Aerothermodynamic Design Issues for Hypersonic Vehicles
Multiblock Analysis for Shuttle Orbiter Re-entry Heating from Mach 24 to Mach 12
FLUID DYNAMICS - Analytical and Computational Study of Wall Temperature Jumps in Supersonic Flow
Influence of Ablation on Radiative Heating for Earth Entry
Solution Strategy for Three-Dimensional Configurations at Hypersonic Speeds
Aerodynamic Analysis of Commercial Experiment Transporter Re-Entry Capsule
Navier-Stokes Simulations of Orbiter Aerodynamic Characteristics Including Pitch Trim and Bodyflap
SPECIAL SECTION: X-34 - Computational Aeroheating Predictions for X-34
FLUID DYNAMICS - Comparison of Experimental and Numerical Studies of Ionizing Flow over a Cylinder
Mars Pathfinder Six-Degree-of-Freedom Entry Analysis
Hypersonic Aerodynamic Characteristics of a Proposed Single-Stage-to-Orbit Vehicle