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HUBSCHRAUBER
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Effect of free play in rotor blades hinges on the non-linear ground resonance of a helicopter
A low-vulnerability helicopter rotor blade
Studies of helicopter dynamic stability and control laws
Rotor unsteady aerodynamics model using an efficient free-vortex method
Optimal location of centre of gravity for swashplateless helicopter UAV and MAV
Mathematical modeling of helicopter aerobatic maneuvers
Westland Helicopters choose FLIR
Contract to prove future Lynx is right choice
Research on dynamics of a supercritical propulsion shaft equipped with a dry friction damper
Meggitt Avionics selected for helicopter upgrade programmes
High-speed machining revolutionises production at Boeing Helicopters
Equivalent linear damping model of nonlinear hydraulic damper for helicopter rotor
Helicopter stability and control in the presence of windshear
Production contract signed for Tiger's MTR390 engine
Portable electroluminescent helicopter landing pad
Obstacle detection systems for the rotorcraft
First high-velocity machining application in commercial helicopters
Viper CNC fibre placement system for tiltrotor aircraft
Brookhouse technology behind the scenes in USAF helicopter simulators
Helicopter safety relies on Mettler Toledo
GKN Westland - exploiting powerful CAE software to gain competitive advantage
Racal secures £5 million orders for Nimrod and EHIO1
Sikorsky S-92 anti-icing completes wind tunnel test requirements
Commitment to CAE environment for GKN Westland Helicopters
IMI Marston wins prestigious military helicopter contract
BT46 simulator for the German antitank helicopter PAH-1 AI
A new method for predicting rotor wake geometries and downwash velocity field
Crashworthiness of helicopter subfloor structural components
Optimization software helps design low-noise rotorcraft flight procedures
1 million investment in document handling
Boeing joins Team Cormorant for maritime patrol project
BARCO's avionics displays selected by Boeing
NH90's RTM322 surpasses maximum operational power rating
Red Box introduces lightweight start power for light helicopters
Lightweight start power for light helicopters
The potential of rotorcraft to increase airport capacity
Stability analysis of aeroelastic systems based on aeroelastic FRF and condition number
ESDU data item simulates fatigue of helicopter rotor systems
H∞ robust controller for autonomous helicopter hovering control