X-43A Flight Research Program: Lessons Learned on the Road to Mach 10
X-33 Computational Aeroheating/Aerodynamic Predictions and Comparisons With Experimental Data
X-15: Extending the Frontiers of Flight
Wind Tunnel Measurements of Shuttle Orbiter Global Heating with Comparisons to Flight
Waveform Transition of Sonic Boom Generated from a Sphere at Hypersonic Speed
Variable Transpiration Cooling Effectiveness in Laminar and Turbulent Flows for Hypersonic Vehicles
Use of fusible temperature indicators for obtaining quantitative aerodynamic heat-transfer data
Unique Research Challenges for High-Speed Civil Transports
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
Two-Dimensional Approach to the Maximum Lift- TO-Drag Ratio of a Slender, Flat-Top, Hypersonic Wing
Turbojet Potential for Hypersonic Flight