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HELICOPTERS
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keywords:(HELICOPTERS)
40th European Rotorcraft Forum 2014 : 2-5 September 2014, Southampton, UK
Analytical Estimate of Rotor Controls Required for a Straight Vortex Disturbance Rejection
Iterative learning control experimental results in twin-rotor device
Reduced In-Plane, Low-Frequency Noise of an Active Flap Rotor
Analysis and Control of a Magnetorheological Landing Gear System for a Helicopter
Open-Loop Control of Performance and Vibratory Loads Using Leading-Edge Slats
Development of Control Strategies for a Twin-Cyclocopter in Forward Flight
Modeling and Simulation of Cure Kinetics and Flow in Cavity-Molded Composites
Application of Strand Grid Framework to Complex Rotorcraft Simulations
Simulation of Coupled Helicopter–Slung Load–Pilot Dynamics
Quieting a Rib-Framed Honeycomb Core Sandwich Panel for a Rotorcraft Roof
Minimum Loss Load, Twist, and Chord Distributions for Coaxial Helicopters in Hover
High-Fidelity Linear Time-Invariant Models for Higher Harmonic Closed-Loop Rotor Control Studies
PKW-ähnliche Steuerungskonzepte für den Einsatz im Hubschrauber
Linear Time Invariant Approximations of Linear Time Periodic Systems
Using Model-Scale Tandem-Rotor Measurements in Ground Effect to Understand Full-Scale CH-47D Outwash
Aeroacoustic Simulation of a Complete H145 Helicopter in Descent Flight
The effects of rectangular riblets on rectangular micro air vehicles for drag reduction
Civil and parapublic helicopter : the concise global industry guide ; annual handbook ; 12.2013
Investigation of Rotor Vibratory Loads of a UH-60A Individual Blade Control System
A Review of 60 Years of Rotor Hub Drag and Wake Physics: 1954–2014
Photogrammetric Measurements of an EH-60L Brownout Cloud
Optimum Actuator-Disk Performance in Hover and Axial Flight by a Compact Momentum Theory with Swirl
Vehicle Modeling Additions for Off-Axis Improvements in a Real-Time Helicopter Model
Design and Development of the Atlas Human-Powered Helicopter
Design and Development of the Atlas Human-Powered Helicopter
A System Identification Strategy for Nonlinear Model of Small-Scale Unmanned Helicopters
Multibody Dynamics Simulation and Experimental Investigation of a Model-Scale Tiltrotor
Dynamic Stall Model with Circulation Pulse and Static Hysteresis for NACA 0012 and VR-12 Airfoils
Concurrent Aerodynamic Optimization of Rotor Blades Using a Nash Game Method
Obstacle Avoidance and Targeted Flight for Rotary Wing MAVs in GPS-Denied Environments
Robustness and Limits of Vortex Generator Effectiveness in Helicopter Drag Reduction
A Third Approximation to Glauert's Momentum Theory
Development of a Helicopter Operations Management System for Disaster Relief Missions