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Flugmechanik
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WORKLOAD MONITORING THROUGH SPEECH ANALYSIS: TOWARDS A SYSTEM FOR AIR TRAFFIC CONTROL
Women in Flight Research at NASA Dryden Flight Research Center from 1946 to 1995, Number 6
Wing X-7A (Tv-14) - Determination of Deformation Due to Flight Loads
Wing/Wall Aerodynamic Interactions in Free Flying, Maneuvering MAVs
Wing–Wake Interaction of Three-Dimensional Flapping Wings
Wing-Wake Interaction and its Proper Orthogonal Decomposition
Wings with minimum drag due to lift in supersonic flow
Wing Surface Pressure Data from Large-Scale Wind-Tunnel Tests of a Propeller-Driven STOL Model
Wings of the Nation. Volume 19, Number 12, 1968 (Selected Articles)
Wings of the Minimum Induced Drag: Spanload Implications for Aircraft and Birds
Wing Shape Optimization of a Near-Sonic Passenger Plane
Wing Selection and Dynamic Derivative Estimation of a Tailless UAV
Wing Rock Suppression Using Forebody Vortex Control
Wing Rock Suppression in the F-15 Aircraft
Wing Rock Prediction Method for a High Performance Fighter Aircraft
Wing pressure distributions from subsonic tests of a high-wing transport model
Wing Pressure Distributions from Subsonic Tests of a High-Wing Transport Model
Wing pressure-distribution measurements up to 0,866 Mach number in flight on jet-propelled airplane
Wing planform effects at supersonic speeds for an advanced fighter configuration
Wing Planform Effects at Supersonic Speeds for an Advanced Fighter Configuration
Wing Panel Design with Novel Skin-Buckling Containment Features
Wing Lifting Line Representation - Application to the Two Wings in Tandem Interaction
Winglets. 1972-July, 1983 (Citations from the International Aerospace Abstracts Data Base)
Winglet Forward Thrust Quantified and the Mechanism of Induced Drag Reduction
Winglet effectiveness on low aspect ratio wings at supersonic Mach numbers
Winglet Effectiveness on Low Aspect Ratio Wings at Supersonic Mach Numbers
Winglet Design and Optimization for UAVs
Winglet Design and Analysis for Cessna 152 - A Numerical Study
Winglet and long duct nacelle aerodynamic development for DC-10 derivatives
Wing Leading Edge Concepts for Noise Reduction
WING LEADING EDGE CONCEPTS FOR NOISE REDUCTION
Wing laminar boundary layer in the presence of a propeller slipstream