X-31A flight flutter test excitation by control surfaces
Vorticity equation solutions for slender wings at high incidence
Vibration analysis of composite turbopropellers using a nonlinear beam-type finite-element approach
Velocity tracking control of a four-rotor mini helicopter
Validation of mathematical simulations of helicopter vertical response characteristics in hover
V-22 low-speed/high rate of descent (HROD) test results
Unmanned aerial vehicle aerodynamic model identification from a racetrack manoeuvre
Time and frequency-domain identification and verification of BO 105 dynamic models
Time-Accurate Simulation of Longitudinal Flight Mechanics with Control by CFD/RBD Coupling
The Wright Brothers: First aeronautical engineers and test pilots
The T-Wing tail-sitter unmanned air vehicle: From design concept to research flight vehicle
The effect of simulator motion on pilot control behaviour for agile and inert helicopter dynamics
The effect of airframe aerodynamics on V-22 rotor loads
The Dolphin 6075: an helicopter dedicated to flight test research
System identification modeling of a small-scale unmanned rotorcraft for flight control design
Survey of TIGER main rotor loads from design to flight test
Studies of trims, stability, controllability, and some flying qualities of a tandem rotor helicopter
State-space representation of vortex wakes by the method of lines
Stability prediction of sling load dynamics using wind tunnel models
Stability characteristics of a conical aerospace plane concept
Stability augmentation of helicopter rotor blades using passive damping of shape memory alloys
Stability and control analysis of the slowed-rotor compound helicopter configuration
Some aeromechanical aspects of insect-like flapping wings in hover
Simulating moth wing aerodynamics: Towards the development of flapping-wing technology
Rotor power reduction using multiple spanwise-segmented, optimally-actuated trailing-edge flaps
Rotor design optimization using a multidisciplinary approach
Rotorcraft handling qualities engineering: Managing the tension between safety and performance
Rotor aerodyanmic in ground effect at low advance ratios
Robust gust alleviation and stabilization of very flexible aircraft