Структурные характеристики мезофаз и мезоморфных стекол металалканоатов
Анализ движения наноспутника SamSat-218Д по траекторным измерениям
Zonal Detached-Eddy Simulation of Separated Flow Around a Finite-Span Wing
Zonal Detached-Eddy Simulation of an Airfoil in Poststall Condition
Yawsonde Technology for the Jet Propulsion Laboratory (JPL) Free Flying Magnetometer (FFM) Program
Yaw Rate and Sideslip Angle Control through Single Input Single Output Direct Yaw Moment Control
Yaw Departure and Recovery of a Tailless Aircraft Configuration
Yaw-Control Spoiler Design Using Design of Experiments Based Wind Tunnel Testing
Yaw Angle Effect on Flow Structure over the Nonslender Diamond Wing
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
Worst-Case Disturbances for Time-Varying Systems with Application to Flexible Aircraft
Wireless Protocol Design for a Cooperative Pedestrian Protection System
Wing Rock Prediction Method for a High Performance Fighter Aircraft
Wing Rock Motion of an Aircraft Model at Fixed Angle of Attack
Wing Rock Induced by a Hemisphere–Cylinder Forebody
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
Wind Tunnel Tests of Elevon Gap Heating on the Space Shuttle Orbiter (OH-107)
Wind-Tunnel Tests of a Series of Parachutes Designed for Controllable Gliding Flight
Wind Tunnel Tests of a Scale Model Railroad Automobile Rack Car
Wind Tunnel Tests of 16 Percent Thick Airfoil Section with Spoilers at Different Chordwise Positions
Wind Tunnel Test of Ring-Wing Canard Configurations for Air-to-Surface Antitank Missiles