KENTUCKY RE-ENTRY UNIVERSAL PAYLOAD SYSTEM (KRUPS): DESIGN AND TESTING FOR ORBITAL FLIGHT
HINGE METHOD FOR CFD AND FLUID-ABLATION INTERACTION MODELING
FULLY COUPLED INTERNAL RADIATIVE HEAT TRANSFER FOR THE 3D MATERIAL RESPONSE OF HEAT SHIELD
A NOVEL ENGINEERING METHODOLOGY FOR DECOUPLED AEROTHERMAL ANALYSIS OF HYPERSONIC ATMOSPHERIC ENTRY
SPALLATION PARTICLE SIZE ANALYSIS RESULTING FROM ARC-JET EXPERIMENTS
RADIATIVE TRANSMISSION AND ABSORPTION WITHIN THE ABLATIVE HEAT SHIELD OF HYPERSONIC VEHICLES
MICRO-SCALE THERMAL-STRUCTURAL MODELING FOR CARBON FIBERS