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Flugmechanik
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X-33 Experimental Aeroheating at Mach 6 Using Phosphor Thermography
X-33 Computational Aeroheating/Aerodynamic Predictions and Comparisons With Experimental Data
X-33 Attitude Control System Design for Ascent, Transition, and Entry Flight Regimes
X-33 Aerodynamic and Aeroheating Computations for Wind Tunnel and Flight Conditions
X-31 Post-Stall Envelope Expansion and Tactical Utility Testing
X-31A System Identification Applied to Post-Stall Flight: Aerodynamics and Thrust Vectoring
X-31A High Angle of Attack and Initial Post Stall Flight Testing
Wright Laboratory Research and Development Facilities Handbook