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Flugmechanik
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Robust gust alleviation and stabilization of very flexible aircraft
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
Time and frequency-domain identification and verification of BO 105 dynamic models
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
The T-Wing tail-sitter unmanned air vehicle: From design concept to research flight vehicle
Cost/performance benefits of large-scale ground vibration test systems
A parametric design study for a swashplateless helicopter rotor with trailing-edge flaps
Cell-vertex, multigrid Euler scheme for use with multiblock grids
Performance of a cycloidal rotor concept for micro air vehicle applications
Some aeromechanical aspects of insect-like flapping wings in hover
Survey of TIGER main rotor loads from design to flight test
Rotor design optimization using a multidisciplinary approach
Computational aerodynamics analysis of a Martian rotorcraft
Validation of mathematical simulations of helicopter vertical response characteristics in hover
A quasilinear analysis and design technique for nonlinear flight control system
Hingeless rotor aeroelastic stability analysis with refined aerodynamic modeling
The effect of airframe aerodynamics on V-22 rotor loads
Simulating moth wing aerodynamics: Towards the development of flapping-wing technology
Blade response calcultaions using three-dimensional aerodynamic modeling
Reduced-Order Aeroelastic Models for Dynamics of Maneuvering Flexible Air