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title: Aircraft Aerodynamic Design
X-38 NASA/DLR/ESA-Dassault Aviation Integrated Aerodynamic and Aerothermodynamic Activities
X-37 Flight Demonstrator: Approach and Landing Test Vehicle Flight Test Approach
Variable Stiffness Spar Wind-Tunnel Model Development and Testing
Usability Evaluation of a Flight-Deck Airflow Hazard Visualization System
Transonic-Small-Disturbance and Linear Analyses for the Active Aeroelastic Wing Program
Thermal Management Design for the X-33 Lifting Body
Success Stories in Control: Nonlinear Dynamic Inversion Control
Post-Stall Aerodynamic Modeling and Gain-Scheduled Control Design
Measured Aerodynamic Interaction of Two Tiltrotors
Intelligent Control for the BEES Flyer
Flying wings / flying fuselages
Flight Test of the F/A-18 Active Aeroelastic Wing Airplane
Experiments in High-Lift for High-Speed Civil Transports
Evolution of a Mars Airplane Concept for the ARES Mars Scout Mission
Dynamics and Stability and Control Characteristics of the X-37
Dual-Spool Turbine Facility Design Overview