X-31A flight flutter test excitation by control surfaces
Velocity tracking control of a four-rotor mini helicopter
V-22 low-speed/high rate of descent (HROD) test results
Time-Accurate Simulation of Longitudinal Flight Mechanics with Control by CFD/RBD Coupling
The implementation of an autonomous helicopter testbed
The Dolphin 6075: an helicopter dedicated to flight test research
TEDAS II - High speed data acquisition, storage and distribution
System concept for a rotorcraft vision system to improve cargo handling operations
Status of a digital integrated propulsion/flight control system for the YF-12 airplane
Stability prediction of sling load dynamics using wind tunnel models
Stability of hingeless rotor blades in hover with pitch-link flexibility
Stability characteristics of a conical aerospace plane concept
Stability augmentation of helicopter rotor blades using passive damping of shape memory alloys
Propulsion/aircraft integration and dynamic performance of hypersonic TSTO-vehicles
Preliminary Design of a Mach 6 Configuration Using MDO
Prediction of rotor aeroacustic in forward flight by a lifting surface method
Performance improvement with variable rotor span and RPM
Parallel computing of helicopter response to turbulence toward real-time implementation
Optimization of asymmetric oblique flying wing configurations under variable constraints
Oppertunities in flight/propulsion control coupling (FPCC)
Nutzung des A340-Simulators für Flugeigenschaftsanalysen
Numerical methods for the aeromechanical design of flapping wing hovering MAV
Modern wind tunnel techniques for unsteady testing - development of dynamic test rigs
Modelling the aerodynamics of coaxial helicopters - from an isolated rotor to a complete aircraft
Modeling lead-lag dynamics for rotorcraft-pilot-couplings investigation
Micro-rotorcraft performance improvement using trailing-edge gurney flaps
Incorporation of aircraft performance considerations in inverse airfoil design
Improving helicopter flight mechanics models with laser measurements of blade flapping
Higher order staggered coupling schemes to predict the aeroelastic behavior of helicopter rotors
From the test benches to the first prototype of the muFly micro helicopter
Flutter and gust response analysis of flexible aircraft with active control
Flow control for aircraft performance enhancements - Overview of airbus - University cooperation
Extended energy management methods for flight performance optimization
Experimental and numerical aspects of simulating unsteady flows around the X-31 configuration
Experimental aerodynamic and aeroacoustic investigation of a scaled tilt rotor in hover