William L. Wells

• Measured and predicted aerodynamic coefficients and shock shapes for Aeroassist Flight Experiment (AFE) configuration
• Measured and predicted shock shapes for AFE configuration at mach 6 in air and in FDb□-s□b4b□-s□s
• Measured and predicted shock shapes for AFE configuration at mach 6 in air and in FD₄
• Surface flow and heating distributions on a cylinder in near wake of Aeroassist Flight Experiment (AFE) configuration at incidence in Mach 10 air