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HUBSCHRAUBER
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keywords:(HUBSCHRAUBER)
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
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
Extension of the Unstructured TAU-Code for Rotating Flows
Application of Feature-Based Grid Adaptation to Helicopter Rotor Flow
On-line scheduling and fault detection in NCS with communication constraints in Drone application
Neue Technologien für Durchsichtdisplays zur Verwendung im fliegenden Hubschraubersimulator FHS
A multi-body systems approach to simulate helicopter occupant protection systems
On Dynamic State-Space models for fatigue-induced structural degradation
Airfoil pressure measurements during a blade vortex interaction and a comparisonwith theory
Correlated turbulence modelling: An advancing Fourier series method
Surrogate based optimization of helicopter rotor blades for vibration reduction in forward flight
Parallel efficient mesh motion using radial basis functions with application to multi-bladed rotors
Detection of pre-crack fatigue damage in a U.S. army MH-47E Chinook aft rotor shaft
Active model based predictive control for unmanned helicopter in full flight envelope
Rotorcraft dispatching in large-scale emergencies using sequential linear assignment techniques
Computational fluid dynamics simulations of ship airwake
Modeling helicopter blade sailing: Dynamic formulation in the planar case
Assessment of maintenance need for condition-based maintenance development
Heute schon wie morgen fliegen. Mit dem Flugsimulator AVES Forschung auf Flight Level Zero
Compound Helicopter Optimum Design Based on Genetic Algorithm
Rotor power reduction using multiple spanwise-segmented, optimally-actuated trailing-edge flaps
Chimera simulation of a complete helicopter with rotors as actuator discs
Fatigue life reliability based on measured usage, flight loads, and fatigue strength variations
In-flight tuning: Wind tunnel test results and flight test preparation
A comparison of main rotor smoothing adjustments using linear and neural network algorithms
Modelling the aerodynamics of coaxial helicopters - from an isolated rotor to a complete aircraft
Optimization of inspection planning for probabilistic damage tolerance design
Recent applications of design optimization to rotorcraft - a survey
A new boundary integral formulation for the prediction of sound radiation
Influence of rotor wakes on helicopter aerodynamic behaviour