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Flugmechanik
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Dynamic behavior of the vortex ring formed on a butterfly wing
Experimental method for studying gust effects on micro rotorcraft
Experimental investigation of hypersonic buzz on a delta configuration
Mathematical modelling of a helicopter rotor track and balance: Theory
A theoretical technique for analyzing aeroelastic stability of bearingless rotors
Rotorcraft handling qualities engineering: Managing the tension between safety and performance
Optimal approach minimizing aircraft noise and fuel consumption
Mathematical modelling of a helicopter rotor track and balance: Results
A rational approach to comparing the performance of coaxial and conventional rotors
A mathematical model of a twin ducted-fan vertical takeoff and landing jetpack
Helicopter vibration reduction using fixed-system auxiliary moments
Studies of trims, stability, controllability, and some flying qualities of a tandem rotor helicopter
Experimental investigations of the functional morphology of dragonfly wings
Vibration analysis of composite turbopropellers using a nonlinear beam-type finite-element approach
Aircraft operating environments around high-speed ships
Conceptual design of a medium-sized joined-wing aircraft
Method for identification of non-linear multi-degree-of-freedom systems
The Wright Brothers: First aeronautical engineers and test pilots
A multi-body approach for modelling manoeuvring aeroelastic aircraft during preliminary design
Performance analysis of the slowed-rotor compound helicopter configuration
Control mechanism strategies for spin-stabilized projectiles
A severity analysis for rotorcraft encounters with vortex wakes
Stability and control analysis of the slowed-rotor compound helicopter configuration
System identification modeling of a small-scale unmanned rotorcraft for flight control design
Dynamic blade shape for improved helicopter rotor performance
First steps in the development of handling qualities criteria for a civil tilt rotor
Flight test identification of SH-2G flapped-rotor helicopter flight mechanics models
Design and testing of an autorotative payload delivery system
State-space representation of vortex wakes by the method of lines
Optimization of rotorcraft flight following engine failure
Robust gust alleviation and stabilization of very flexible aircraft
Impact of aerodynamics and structures technology on heavy lift tiltrotors
A variable stability projectile using an internal moving mass
Design and investigation of a bio-inspired ventilated flapping wing
Estimation of aircraft inertia characteristics from bifilar pendulum test data
Optimization of critical trajectories for rotorcraft vehicles
Main rotor-tail rotor interaction and its implications for helicopter directional control
Analysis of helicopter blade-vortex interaction noise with flight path or attitude modification