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HELICOPTERS
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keywords:(HELICOPTERS)
Variable rotor speed control for an integrated helicopter/engine system
Nonlinear Analysis of a Coaxial Microhelicopter with a Bell Stabilizer Bar
Helicopter Rotor Sailing by Non-Smooth Dynamics Co-Simulation
Towards consistent hybrid overset mesh methods for rotorcraft CFD
Parallel universal approach to mesh motion and application to rotors in forward flight
Design and implementation of H-inf controller for micro-monocopter
Simulation calculation of mooring tension of the ship-based helicopter
CFD based shape optimization of a helicopter main rotor
CFD based shape optimization of a helicopter main rotor
The Aerodynamics Investigation of Vortex Trap on Helicopter Blade
Attitude control of a quadrotor aircraft subject to a class of time-varying disturbances
Extension of the Unstructured TAU-Code for Rotating Flows
On-line scheduling and fault detection in NCS with communication constraints in Drone application
Application of Feature-Based Grid Adaptation to Helicopter Rotor Flow
A multi-body systems approach to simulate helicopter occupant protection systems
Neue Technologien für Durchsichtdisplays zur Verwendung im fliegenden Hubschraubersimulator FHS
On Dynamic State-Space models for fatigue-induced structural degradation
Correlated turbulence modelling: An advancing Fourier series method
Airfoil pressure measurements during a blade vortex interaction and a comparisonwith theory
Surrogate based optimization of helicopter rotor blades for vibration reduction in forward flight
Detection of pre-crack fatigue damage in a U.S. army MH-47E Chinook aft rotor shaft
Parallel efficient mesh motion using radial basis functions with application to multi-bladed rotors
Active model based predictive control for unmanned helicopter in full flight envelope
Modeling helicopter blade sailing: Dynamic formulation in the planar case
Compound Helicopter Optimum Design Based on Genetic Algorithm
Computational fluid dynamics simulations of ship airwake
Rotorcraft dispatching in large-scale emergencies using sequential linear assignment techniques
Fatigue life reliability based on measured usage, flight loads, and fatigue strength variations
Chimera simulation of a complete helicopter with rotors as actuator discs
Heute schon wie morgen fliegen. Mit dem Flugsimulator AVES Forschung auf Flight Level Zero
Assessment of maintenance need for condition-based maintenance development
Rotor power reduction using multiple spanwise-segmented, optimally-actuated trailing-edge flaps