Blade Displacement Measurements of a Rotor in Forward Flight in the Langley 14- by 22-Ft Wind Tunnel
Modelling Helicopter Flight Dynamics: Building a Simulation Model
Rotor in Vertical Flight: Blade Element Theory
An active flap deployment system for blade-disturbance interaction alleviation
Heat-transfer measurements on the rotor blade of a rotor entry vehicle model
Experimental observations of two-dimensional blade-vortex interaction
Propeller-rotor whirl flutter - A state-of- the-art review
Numerical simulation of helicopter aeromechanics in slow descent flight
Accurate and Efficient Vortex-Capturing for Rotor Blade Vortex Interaction
Aerodynamic Damping Blade Vibrations in Turbo-Machines
An experimental and theoretical study of blade-vortex interaction noise
Alleviation of Retreating Side Stall Using Active Gurney Flaps
Novel boundary integral formulation of blade-vortex interaction aerodynamics of helicopter rotors
Linearized Aerodynamic Theory of Rotor Blades. II- Lifting-Line Theory
Analysis of helicopter blade-vortex interaction noise with flight path or attitude modification
Hovering performance of a rotor with slotted blade tips
Rotorcraft vibration reduction and noise prediction using a unified aeroelastic response simulation
Low cycle fatigue behaviour of alternative steels for highly stressed rail components
9x7 Wind Tunnel Sonic Boom Measurements and Computational-Experimental Comparisons
Stall Margin Enhancement of Aeroengine Compressor with a Novel Type of Alternately Swept Blades
Propeller Noise at Subsonic Blade Tip Speeds, Torque and Thrust Force
Studies of the Dynamic Stall or Airfoil Profiles for Helicopter Rotors
Flight Acoustic Testing and Data Acquisition For the Rotor Noise Model (RNM)
Rotor Mechanisms for Forward Flight
Experimental/numerical evaluation of integral trailing edge flaps for helicopter rotor applications
Loads and Stability Analysis of an Unmanned Tilt Rotor
A Wind-Tunnel Investigation of a 7-Foot- Diameter Ducted Propeller
Modeling Helicopter Near-Horizon Harmonic Noise Due to Transient Maneuvers
Calculation of the Aerodynamic Flow Field in the Vicinity of a Sea King Helicopter
Quasi-three-dimensional flow of gas in turbomachine blade row
Weibull distributions applied to cost and risk analysis for aero engines