Estimation of aircraft inertia characteristics from bifilar pendulum test data
Experimental aerodynamic and aeroacoustic investigation of a scaled tilt rotor in hover
Experimental and numerical aspects of simulating unsteady flows around the X-31 configuration
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
Experimentelle und numerische Bestimmung der dynamischen Derivative
Extended energy management methods for flight performance optimization
First steps in the development of handling qualities criteria for a civil tilt rotor
Flexible aircraft modelling for flight loads analysis of wake vortex encounters
Flight test identification of SH-2G flapped-rotor helicopter flight mechanics models
Flow control for aircraft performance enhancements - Overview of airbus - University cooperation
Flugregelung und aktive Schwingungsdämpfung für flexible Großraumflugzeuge
Flutter and gust response analysis of flexible aircraft with active control
Friedliche Drohne. Flugversuchsträger mit Embedded-PC-Steuerung
From the test benches to the first prototype of the muFly micro helicopter
Genetic optimizations of EC-135 noise abatement flight procedures using an aeroacoustic database
Guidance and control of a spacecraft to rendezvous and dock with a non-cooperative target
Helicopter vibration reduction using fixed-system auxiliary moments
Higher order staggered coupling schemes to predict the aeroelastic behavior of helicopter rotors
Hingeless rotor aeroelastic stability analysis with refined aerodynamic modeling
Hybridmodellierung und Systemidentifizierung der nichtlinearen Hubschrauber-Flugdynamik
Impact of aerodynamics and structures technology on heavy lift tiltrotors
Improvement of aerospace plane performance by overfueled ramjet combustion
Improving helicopter flight mechanics models with laser measurements of blade flapping
Incorporation of aircraft performance considerations in inverse airfoil design
Influence of rotor wakes on helicopter aerodynamic behaviour
Innovative Rotorsysteme (INROS). Abschlussbericht. Berichtszeitraum: 01.01.2007 - 31.03.2010