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HUBSCHRAUBER
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keywords:(HUBSCHRAUBER)
Reduced In-Plane, Low-Frequency Noise of an Active Flap Rotor
Variable rotor speed control for an integrated helicopter/engine system
Nonlinear Analysis of a Coaxial Microhelicopter with a Bell Stabilizer Bar
Higher harmonic pitch link loads reduction using fluidlastic isolators
Helicopter Fuselage Wake Prediction Using Detached-Eddy Simulation
Helicopter fuselage aerodynamic data fitting using multivariate smoothing thin plate splines
Oscillating aerofoil and perpendicular vortex interaction
Airflow hazard prediction for helicopter flight in icing condition
Helicopter Rotor Sailing by Non-Smooth Dynamics Co-Simulation
New Technology for Field Survey of Traditional Settlements
Towards consistent hybrid overset mesh methods for rotorcraft CFD
Helicopter noise prediction: The current status and future direction
Wing–vortex interaction: unraveling the flowfield of a hovering rotor
Parallel universal approach to mesh motion and application to rotors in forward flight
Surface micro-grooves for near-wall exergy and flow control: application to aircraft intake de-icing
Simulation calculation of mooring tension of the ship-based helicopter
Design and implementation of H-inf controller for micro-monocopter
The Aerodynamics Investigation of Vortex Trap on Helicopter Blade
Attitude control of a quadrotor aircraft subject to a class of time-varying disturbances
Dynamics of a pneumatic artificial muscle actuation system driving a trailing edge flap
An unsteady aerodynamic formulation for efficient rotor tonal noise prediction
Study on Equivalent Damping in Nonlinear Fluidlastic Damper of Helicopter Rotor
Air coupled acoustic thermography (ACAT) inspection technique
Judging the urgency of non-verbal auditory alarms: A case study
Unsteady Euler and Navier-Stokes Simulations of Propellers with the Unstructured DLR TAU-Code
Application of Feature-Based Grid Adaptation to Helicopter Rotor Flow
Recent developments in rotary-wing aerodynamic theory
Extension of the Unstructured TAU-Code for Rotating Flows
Vom Buckelwal lernen heißt besser fliegen lernen. Wie Hubschrauber noch wendiger werden können
Condition monitoring of helicopter gearboxes using automatic vibration analysis techniques
Holistic approach for structural integrity evaluation of composite main rotor blades
On-line scheduling and fault detection in NCS with communication constraints in Drone application
Design of a helicopter structural member using friction stir welding
Potential and limitation of UAV for monitoring subsidence in municipal landfills
Neue Technologien für Durchsichtdisplays zur Verwendung im fliegenden Hubschraubersimulator FHS
Emergency landing dynamic conditions: a comparison with accident impact conditions
Vibration Analysis of the Load on Helicopter Swashplate Rod
On Dynamic State-Space models for fatigue-induced structural degradation
A multi-body systems approach to simulate helicopter occupant protection systems
Applications des alliages d'aluminium forges et matrices dans l'aeronautique
Welche strukturmechanischen Aspekte sind zu beachten? Kleben im Hubschrauberbau