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Flugmechanik
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About the Use of Vortex Generators to Improve Aircraft Aerodynamics
Actively translating a rear diffuser device for the aerodynamic drag reduction of a passenger car
Adaptive vortex generators based on active hybrid composites: from idea to flight test
Aeroacoustic Characteristics of a Quadcopter Impeller in Vertical Take-Off and Landing Mode
Aerodynamic Analysis of a Box Winglet: Viscous and Compressible Flow Predictions
Aerodynamic Design and Performance Research of Racing Cars with Adaptive Control of Attitude
Aerodynamic design optimization of a helicopter rotor blade-sleeve fairing
Aerodynamic design optimization of rear body shapes of a sedan for drag reduction
Aerodynamic study of a generic car model with wheels and underbody diffuser
Aeroelastic tailoring of an NLF forward swept wing
Analysis of trimmable conditions for a civil aircraft with active high-lift system
An improved high-lift aerodynamic prediction method for transport aircraft
A two-element high-lift airfoil in disturbed flow conditions
Automobile aerodynamics influenced by airfoil-shaped rear wing
Comparative Analysis of Turbulence Models for Automotive Aerodynamic Simulation and Design
Composite model of a research flight simulator for a helicopter with the hingeless main rotor
Computationally effective mathematical model of airplane flight
Conceptual design analysis of a variable swept half-span wing of a supersonic business jet
Drag Reduction of a Passenger Car Using Flow Control Techniques
Effect of an active high-lift system failure during landing approaches
Effect of Crosswinds on the Aerodynamics of Two Passenger Cars Crossing Each Other
Effects of Wheel Configuration on the Flow Field and the Drag Coefficient of a Passenger Vehicle
Engine integration based on multi-disciplinary optimisation technique
Experimental investigation of generic ice block trajectories under freestream conditions
Flap efficiency analysis for the SAGITTA diamond wing demonstrator configuration
Flow Features and Aerodynamic Analysis of the Canard Missiles
High-lift design for a forward swept natural laminar flow wing
Improvement of the Control System for the Wing Performance of an Unmanned Aerial Vehicle
Influence of Inter-Vehicle Distance on the Aerodynamics of a Two-Truck Platoon
Investigation of helicopter maneuverability by the power balance method