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Flight dynamics
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dynamics
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X-33 Experimental Aeroheating at Mach 6 Using Phosphor Thermography
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 Quasi-Tailless Flight Demonstration
X-31 post-stall envelope expansion and tactical utility testing
X-31 High Angle of Attack Control System Performance
X-31A System Identification Applied to Post-Stall Flight: Aerodynamics and Thrust Vectoring
X-31A Quasi-Tailless Flight Test Results
X-31A High Angle of Attack and Initial Post Stall Flight Testing
X-31 Aerodynamic Characteristics Determined from Flight Data
X-29A Aircraft Structural Loads Flight Testing