X-43A Flight-Test-Determined Aerodynamic Force and Moment Characteristics at Mach 7.0
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-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
X-31 Aerodynamic Characteristics Determined from Flight Data
Wing Rock Prediction Method for a High Performance Fighter Aircraft
Wing Pressure Distributions from Subsonic Tests of a High-Wing Transport Model
Wing Planform Effects at Supersonic Speeds for an Advanced Fighter Configuration
Wing-Alone Aerodynamic Characteristics for High Angles of Attack of Supersonic Speeds