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HELICOPTERS
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keywords:(HELICOPTERS)
New Methods to Subjectively and Objectively Evaluate Adverse Pilot Couplings
Aeroelastic Analysis of Avian-Based Flexible Flapping Wings for Micro Air Vehicles
Experimental Analysis of the Aerodynamics of Long-Shrouded Contrarotating Rotor in Hover
U.S. ARMY COMBAT CAPABILITIES DEVELOPMENT COMMAND - AVIATION & MISSILE CENTER: THE FUTURE OF ADS-33
AHS Rotorcraft Handling Qualities Technical Meeting : Huntsville, Alabama, USA, 18-19 February 2020
Helicopter Slung Load Control Using Lagged Cable Angle Feedback
Prediction of Rotorcraft Design Impacts on Maneuverability Characteristics
A Real-Time Expert Control System For Helicopter Autorotation
Characterization of CH-47D Rotor System Fault Signatures Using a Comprehensive Model
Development of a Quad Cycloidal-Rotor Unmanned Aerial Vehicle
Advanced Composite Materials Technology for Rotorcraft through the Use of Nanoadditives
Optimum Loading and Induced Swirl Effects in Hover
Modular Multisolver Approach for Efficient High-Fidelity Simulation of the HART II Rotor
Eigenstructure Control: A Rotorcraft Handling Qualities Engineering Tool
Performance Enhancement in Dynamic Stall Condition Using Active Camber Deformation
Dynamic Stall Life Cycle on a Rotating Blade in Steady Forward Flight
Rotorcraft Flight Envelope Protection by Model Predictive Control
Simulation of Airfoil Interaction in Co-Rotating Coaxial Rotors with Uncertainty Quantification
Quadcopter Rotor Phasing for Minimization of Aircraft Vibratory Loads
Vortex Particle Method Whirl-Flutter Predictions of a Tiltrotor with Wing Extensions
A Computational Framework for Helicopter Fuselage Drag Reduction Using Vortex Generators
Collaborative Investigation of the Aerodynamic Behavior of Airfoils in Reverse Flow
Stability of Nonlinear, Time-Dependent Rotorcraft Systems Using Lyapunov Characteristic Exponents
Fluid Dynamics of the Helicoidal Wake Sheets Trailed from a Hovering Rotor
The Influence of Laminar-Turbulent Transition on Rotor Performance at Low Reynolds Numbers