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Flugmechanik
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Dynamic behavior of the vortex ring formed on a butterfly wing
Energy reference guidance for drag-modulated aerocapture
Application of time-domain unsteady aerodynamics to rotary-wing aeroelasticity
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
Simulations- und Flugversuche über Flugeigenschaften von Hyperschall-Flugzeugen
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
Studies of trims, stability, controllability, and some flying qualities of a tandem rotor helicopter
Helicopter vibration reduction using fixed-system auxiliary moments
Experimental investigations of the functional morphology of dragonfly wings
High downforce race car vertical dynamics: aerodynamic index
Aircraft operating environments around high-speed ships
Conceptual design of a medium-sized joined-wing aircraft
Unmanned aerial vehicle aerodynamic model identification from a racetrack manoeuvre
Vibration analysis of composite turbopropellers using a nonlinear beam-type finite-element approach
The Wright Brothers: First aeronautical engineers and test pilots
Method for identification of non-linear multi-degree-of-freedom systems
Development of an attitude guidance and control system for the Thunderstar suborbital spacecraft
Design, development, and open-loop flight-testing of a twin-rotor cyclocopter micro air vehicle
Dynamic modeling and fuzzy control for a small tiltrotor unmanned aerial vehicle
A multi-body approach for modelling manoeuvring aeroelastic aircraft during preliminary design
Generic Modeling and Parametric Study of Flapping Wing Micro-Air-Vehicle
Vorticity equation solutions for slender wings at high incidence
Vortraege des DFVLR-Kolloquiums am 8. Mai 1973 im Forschungszentrum Porz-Wahn
Performance analysis of the slowed-rotor compound helicopter configuration
Stability and control analysis of the slowed-rotor compound helicopter configuration
System identification modeling of a small-scale unmanned rotorcraft for flight control design
A severity analysis for rotorcraft encounters with vortex wakes
Dynamic blade shape for improved helicopter rotor performance
Control mechanism strategies for spin-stabilized projectiles
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
Effect of ionospheric drag on atmospheric density estimation and orbit prediction