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Hubschrauber
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Aeroelastic response and blade loads ofa composite rotor in forward flight
Aeroelastic optimization of an advanced geometry helicopter rotor
Aeromechanical stability of a bearingless composite rotor in forward flight
Aeromechanical stability of rotorcraft with advanced geometry blades
Effect of modeling techniques in the coupled rotor-body vibration analysis
Dynamically tuned blade pitch links for vibration reduction
Multi-objective optimization of a composite helicopter rotor
Aeroelastic analysis of advanced geometry tiltrotor aircraft
Formulation of a rotor-system damage detection methodology
Helicopter vibration reduction with trailing edge flaps
Formulation of a comprehensive aeroelastic analysis for tiltrotor aircraft
Detection of helicopter rotor system simulated faults using neural networks
Helicopter rotor system health monitoring using numerical simulation and neural networks
Closed-loop hover test results with a neurocontroller on piezo-actuated smart rotor blades
Trailing edge flap control methodology for vibration reduction of helicopter with dissimilar blades
Aeroelastic stability of smart trailing-edge flap helicopter rotors
Wind Tunnel Testing for Performance and Vibratory Loads of a Variable-Speed Mach-Scale Rotor
Aeromechanics of a Variable-Speed Rotor
On the Role of Aerodynamic Nonlinearities in Sling Load Dynamics
Active Flaps and Slats for Rotor Performance Enhancement
Design, Development and Flight Testing of a Twin-Rotor Cyclocopter Micro Air Vehicle
Experimental Investigation of the Forward Flight Performance of a MAV-Scale Cycloidal Rotor
A Comparative Study of Different Weight Formulations Affecting Preliminary Sizing of Rotorcraft
Design and Testing of a Dual Tilt-Wing Micro Air Vehicle
Highly Accurate SLAM for Rotary Wing MAVs
Performance and Vibratory Load Measurements of a Slowed Rotor at High Advance Ratios
Aeromechanics of a Variable-Radius Rotor
Development of a Quad Shrouded Rotor Micro Air Vehicle and Performance Evaluation in Edgewise Flow
OBSTACLE AVOIDANCE AND TARGETED FLIGHT FOR ROTARYWING MAVS
INVESTIGATION OF THE UH-60A SLOWED ROTOR WIND TUNNEL TESTS USING UMARC
FLIGHT DYNAMICS IDENTIFICATION OF A CYCLOCOPTER MICRO AIR VEHICLE IN HOVER
HIGH-ADVANCE RATIO WIND TUNNEL TESTING OF TWO MACH-SCALE ROTOR GEOMETRIES
Performance and Flowfield Measurements of a MAV-Scale Helicopter Rotor in Hover
Development of Control Strategies and Flight Testing of a Twin-Cyclocopter in Forward Flight
Explorations of Novel Powerplant Architectures for Hybrid Electric Helicopters
Three-Dimensional CAD-Based Structural Modeling for Next Generation Rotor Dynamic Analysis