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Standsicherheit
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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
Xb-70 Aerodynamic, Geometric, Mass, and Symmetric Structural Mode Data
Xb-70 Aerodynamic, Geometric, Mass, and Symmetric Structural Mode Data
X-48B Flight Research - Test Progress and Instrumentation Needs for the Future
X-38 Application of Dynamic Inversion Flight Control
X-33 Attitude Control Using the XRS-2200 Linear Aerospike Engine
X-33 Attitude Control System Design for Ascent, Transition, and Entry Flight Regimes
X-33 Ascent Flight Controller Design by Trajectory Linearization: A Singular Perturbational Approach
X-33 Ascent Flight Controller Design by Trajectory Linearization: A Singular Perturbational Approach
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
X-29A flight control system performance during flight test
Wing/store flutter with nonlinear pylon stiffness
Wing modification for increased spin resistance
Wing flap-type control effectiveness and effects of control hinge gap seals for a supercritical wing
Wind Tunnel Tests on a Tail-Less Swept Wing Span-Distributed Cargo Aircraft Configuration
Wind-Tunnel Tests of Hinge-Moment Characteristics of Spring-Tab Ailerons
Wind-Tunnel Tests of a Series of Parachutes Designed for Controllable Gliding Flight
WIND-TUNNEL TESTS OF A SERIES OF 18-FOOT-DIAMETER PARACHUTES WITH EXTENDABLE FLAPS
Wind-Tunnel Tests of a Portion of a PV-2 Helicopter Rotor Blade
Wind-tunnel Tests of a Piston-type Control Booster on an Airfoil and Aileron Model