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HUBSCHRAUBER
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keywords:(HUBSCHRAUBER)
Reduced In-Plane, Low-Frequency Noise of an Active Flap Rotor
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
Towards consistent hybrid overset mesh methods for rotorcraft CFD
Helicopter noise prediction: The current status and future direction
Parallel universal approach to mesh motion and application to rotors in forward flight
Wing–vortex interaction: unraveling the flowfield of a hovering rotor
Surface micro-grooves for near-wall exergy and flow control: application to aircraft intake de-icing
The Aerodynamics Investigation of Vortex Trap on Helicopter Blade
Dynamics of a pneumatic artificial muscle actuation system driving a trailing edge flap
An unsteady aerodynamic formulation for efficient rotor tonal noise prediction