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HUBSCHRAUBER
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Development of integrated rotorcraft design and virtual manufacturing framework
The helicopter – efficiency or efficacy?
Correlation of helicopter rotor aeroelastic response with HART-II wind tunnel test data
Laser-based obstacle warning system for helicopters
Solution to rotor blade erosion in sandy environments
Elements of helicopter supermanoeuvrability at low flight velocities
Helicopter escape compartment and all-in-one control column
Real-time hardware simulation of a small-scale helicopter dynamics
Examination of indirect responses of helicopters using a refined inflow model
BAE systems seeks helicopter landing breakthrough
Terrain collision avoidance systems for turbine powered helicopters
Helicopter engine condition monitoring program growing rapidly in US
Neural network based feedback error controller for helicopter
QinetiQ developed antenna extends UAV reach
Improvement of dynamic response prediction of helicopters
30 year partnership with Westland Helicopters Ltd
On the effect of mass and stiffness unbalance on helicopter tail rotor system behavior
Formulation for flutter and vibration analysis of a hingeless helicopter blade in hover: Part I
Direct adaptive fuzzy control for a nonlinear helicopter system
Military helicopter sales will spur increase in turboshaft engine orders
State space identification and implementation of H∞ control design for small-scale helicopter
The safety of shipborne helicopter operation
A nonlinear inverse simulation technique applied to coaxial rotor helicopter maneuvers
Selected aerodynamic design issues for the single-rotor remotely piloted helicopter
Helicopter noise measurements data report
FAC roadshow highlights 'challenge and opportunity' at GKN-Westland
Configuration design and optimisation study of a compound gyroplane
Rotorcraft research in India: recent developments
Insight into the effects of rotor downwash on engine jet
Canadian helicopter verifies night vision system with Ascension's laserBIRD
Modeling the unsteady aerodynamic forces of a maneuvering rotor
Effect of free play in rotor blades hinges on the non-linear ground resonance of a helicopter