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Yaw Axis Stability Augmentation System Flight Test Report
Yaw Axis Control as a Means of Improving V/STOL Aircraft Performance
YAV-8B Simulation and Modeling. Volume 2: Program Listing
YAV-8B Simulation and Modeling. Volume 1: Aircraft Description and Program Summary
Xc-142A V/STOL Transport Tri-Service Limited Category I Evaluation
Xb-70 Aerodynamic, Geometric, Mass, and Symmetric Structural Mode Data
Xb-70 Aerodynamic, Geometric, Mass, and Symmetric Structural Mode Data
X-43A Flight-Test-Determined Aerodynamic Force and Moment Characteristics at Mach 7.0
X-33 Ascent Flight Controller Design by Trajectory Linearization: A Singular Perturbational Approach
X-31 Quasi-Tailless Flight Demonstration
X-31A Quasi-Tailless Flight Test Results
X-31 Aerodynamic Characteristics Determined from Flight Data
X-29 Flight Control System: Lessons Learned
X-29A Technology Demonstrator Flight Test Program Overview
X-29A Longitudinal and Directional Force and Moment Supplemental Transonic Wind Tunnel Test Results
Working with Allies and Partners: A Cost-Based Analysis of U.S. Air Forces in Europe
Wing Rock Prediction Method for a High Performance Fighter Aircraft
Wing Planform Effects at Supersonic Speeds for an Advanced Fighter Configuration
Wind-Tunnel Tests to Determine Aerodynamic Forces and Moments on Ships at Zero Heel
Wind Tunnel Tests on the Static Aerodynamics of a Spinning 105 mm Artillery Shell Model
Wind Tunnel Tests on a Tail-Less Swept Wing Span-Distributed Cargo Aircraft Configuration
Wind-Tunnel Tests of a Series of Parachutes Designed for Controllable Gliding Flight
Wind-Tunnel Tests of a Portion of a PV-2 Helicopter Rotor Blade
Wind Tunnel Tests of an F-8 Airplane Model Equipped with an Oblique Wing
Wind-Tunnel Tests of a 1/78-Scale Model XZWG-1 Airship with Car and Lifting Outrigger
Wind Tunnel Test on a 1/4.622 Froude Scale, Hingeless Rotor, Tilt Rotor Model, Volume 4
Wind Tunnel Test on a 1/4.622 Froude Scale, Hingeless Rotor, Tilt Rotor Model, Volume 3