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Flugmechanik
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keywords:("Flugmechanik")
A hybrid multilevel approach for aeroelastic optimization of composite wing-box
Aircraft operating environments around high-speed ships
A mathematical model of a twin ducted-fan vertical takeoff and landing jetpack
A multi-body approach for modelling manoeuvring aeroelastic aircraft during preliminary design
Analysis of helicopter blade-vortex interaction noise with flight path or attitude modification
Analysis of partial wing damage on flying-wing unmanned air vehicle
A parametric design study for a swashplateless helicopter rotor with trailing-edge flaps
Application of sliding-mode control to air-air interception problem
Application of time-domain unsteady aerodynamics to rotary-wing aeroelasticity
A quasilinear analysis and design technique for nonlinear flight control system
A rational approach to comparing the performance of coaxial and conventional rotors
A severity analysis for rotorcraft encounters with vortex wakes
A theoretical technique for analyzing aeroelastic stability of bearingless rotors
A variable stability projectile using an internal moving mass
A virtual cockpit for a distributed interactive simulation
Blade response calcultaions using three-dimensional aerodynamic modeling
Cell-vertex, multigrid Euler scheme for use with multiblock grids
Computational aerodynamics analysis of a Martian rotorcraft
Conceptual design of a medium-sized joined-wing aircraft
Control mechanism strategies for spin-stabilized projectiles
Cost/performance benefits of large-scale ground vibration test systems
Design and investigation of a bio-inspired ventilated flapping wing
Design and testing of an autorotative payload delivery system
Design, development, and open-loop flight-testing of a twin-rotor cyclocopter micro air vehicle
Development of an attitude guidance and control system for the Thunderstar suborbital spacecraft
Dynamic behavior of the vortex ring formed on a butterfly wing
Dynamic blade shape for improved helicopter rotor performance
Dynamic modeling and fuzzy control for a small tiltrotor unmanned aerial vehicle
Estimation of aircraft inertia characteristics from bifilar pendulum test data
Experimental investigation of hypersonic buzz on a delta configuration
Experimental investigations of the functional morphology of dragonfly wings
Experimental method for studying gust effects on micro rotorcraft
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
Friedliche Drohne. Flugversuchsträger mit Embedded-PC-Steuerung
Helicopter vibration reduction using fixed-system auxiliary moments