X-43A Flight Research Program: Lessons Learned on the Road to Mach 10
Wind Tunnel Measurements of Shuttle Orbiter Global Heating with Comparisons to Flight
Use of fusible temperature indicators for obtaining quantitative aerodynamic heat-transfer data
Two-dimensional, hypersonic wings of maximum lift-to-drag ratio.
Two-dimensional approach to the maximum lift- to-drag ratio of a slender, flat-top, hypersonic wing
Turbojet Potential for Hypersonic Flight
Transonic Aerodynamic Characteristics of Two Hypersonic Cruise Configurations
Thrust Augmentation Options for the beta 2 Two-Stage-to-Orbit Vehicle
Supersonic Transport/Hypersonic Transport (SST/HST) Development
Supersonic Reacting Internal Flow Fields
Supersonic Investigation of Two Dimensional Hypersonic Exhaust Nozzles
Studies Relating to the Attainment of High Lift-Drag Ratios at Hypersonic Speeds