Synonyme wurden verwendet für:
Flugmechanik
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keywords:("Flugmechanik")
ZERO-ODP REFRIGERANTS FOR LOW TONNAGE CENTRIFUGAL CHILLER SYSTEMS
Yaw Stability Control and Emergency Roll Control for Vehicle Rollover Mitigation
Yaw Effects on the Narrowband Spectra Above a Delta Wing in Turbulent Flow
XB-70A Mach 3 Design and Operating Experience
X-29 Flight Test Program Including Wind Tunnel and Computational Support
World's First VTOL Airplane Convair/Navy XFY-1 Pogo
Winglet Design and Analysis for Cessna 152 - A Numerical Study
Wing Airfoil Simplified Design and Analysis
Wind Tunnel-to-Road Aerodynamic Drag Correlation
Wind-Tunnel Tests of Vehicle Cooling System Performance at High Blockage
Wind Tunnel Testing of Micro Air Vehicles at Low Reynolds Numbers
Wind-Tunnel Modelling off Commercial Vehicle Drag-Reducing Devices: Three Case Studies
Wind-Tunnel Measurements of Wing-Canard Interference and a Comparison with Various Theories
Wind Tunnel Investigations of a High Speed Stowed Rotor Aircraft
Wind-Tunnel Investigation of the Low-Speed Aerodynamics of Slender Accelerator-Type Configurations
Wind Tunnel Investigation of an Inflatable Aerodynamic Boattail for Tractor-Trailers
Wind Tunnel Investigation of an Improved Upper Surface Blown-Flap Transport Semi-Span Model
Windows Opening Influence on the Drag Coefficient of a Hatchback Vehicle
Wind Noise and Aerodynamic Drag Optimization of Outside Rear View Mirrors
Wind-Averaged Drag Determination for Heavy-Duty Vehicles Using On-Road Constant-Speed Torque Tests
Western Michigan University Research Vehicle Gamma
“Web-ACSYNT”: Conceptual-Level Aircraft Systems Analysis on the Internet
Wave Drag and High-Speed Performance of Supersonic STOVL Fighter Configurations
Wake and Unsteady Surface-Pressure Measurements on an SUV with Rear-End Extensions
Vortical Sources of Aerodynamic Force and Moment
Vortex Method Simulation of Ground Vehicle Aerodynamics
VORTEX CONTROL FOR TAIL BUFFET ALLEVIATION ON A TWIN-TAIL FIGHTER CONFIGURATION
Virtual Development and Application of Chassis Components and Chassis Controls at GM Europe
VIBRATION CHARACTERISTICS of Three- and Four-Blade Propellers for HIGH-OUTPUT Engines
Vibrational Sensor Based on Fluid Damping Mechanisms
Velocity Dependence of High Angle of Attack Longitudinal Flying Qualities Criteria
Vehicle Load Estimation Using Recursive Total Least Squares for Rollover Detection
Vehicle Kinematics-Based Image Augmentation against Motion Blur for Object Detectors