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Standsicherheit
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US-UAE Relations: A Partnership Threatened by Differences Regarding Human Rights
Use of Higher Fidelity Slosh Models to Reduce Conservatism in Launch Vehicle Flight Control Designs
USAF Limited Flying Qualities Evaluation of an F-4E with Fixed Leading Edge Slats
Update on Risk Reduction Activities for a Liquid Advanced Booster for NASA's Space Launch System
Unsteady Separation Experiments on 2-D Airfoils, 3-D Wings, and Model Helicopter Rotors
Unsteady Gas Dynamics Problems Related to Flight Vehicles
Unsteady Aerodynamics and Aeroelastic Research at AFWAL (Air Force Wright Aeronautical Laboratories)
Unsteady Aerodynamic Analysis of Space Shuttle Vehicles. Part 3: Booster Interference Effects
Uncoupled Longitudinal Stability and Control of Circulation Controlled Rotor VTOL Aircraft in Hover
UH-2 Jet-Augmented High-Speed Research Helicopter Maneuverability and Dynamic Stability Evaluation
Uh-2 Helicopter High-Speed Flight Research with Lift and Thrust Augmentation