Survey of TIGER main rotor loads from design to flight test
Optimal control : workshop, Universität Greifswald, 1.-3. Oktober 2002
The Wright Brothers: First aeronautical engineers and test pilots
Mechanisms underlying chasing behaviour of male blowflies
Dynamic analysis of flexible supercavitating vehicles using modal based elements
Complex configuration meshing - an industrial view and approach
Optimization of asymmetric oblique flying wing configurations under variable constraints
Incorporation of aircraft performance considerations in inverse airfoil design
Higher order staggered coupling schemes to predict the aeroelastic behavior of helicopter rotors
Helicopter vibration reduction using fixed-system auxiliary moments
A severity analysis for rotorcraft encounters with vortex wakes
Optimization of rotorcraft flight following engine failure
Stability augmentation of helicopter rotor blades using passive damping of shape memory alloys
The T-Wing tail-sitter unmanned air vehicle: From design concept to research flight vehicle
V-22 low-speed/high rate of descent (HROD) test results
A parametric design study for a swashplateless helicopter rotor with trailing-edge flaps
Some aeromechanical aspects of insect-like flapping wings in hover
Computational aerodynamics analysis of a Martian rotorcraft
Micro-rotorcraft performance improvement using trailing-edge gurney flaps
A neural approach for fast simulation of flight mechanics
First steps in the development of handling qualities criteria for a civil tilt rotor
State-space representation of vortex wakes by the method of lines
Optimization of critical trajectories for rotorcraft vehicles
Analysis of helicopter blade-vortex interaction noise with flight path or attitude modification
A framework for integration of IVHM technologies for intelligent integration for vehicle management
Integrated flight loads modelling and analysis for flexible transport aircraft
Integrated flight loads modelling and analysis for flexible transport aircraft