Finished Projects

 
Title Short Description
AGILE Aircraft 3rd Generation MDO for Innovative Collaboration of Heterogeneous Teams of Experts
ATEFA Acoustic modelling of different air taxi concepts and description of new communal noise situation in urban areas of German conurbations based on realistic traffic scenarios
AVACON Evaluation of hybrid laminar flow control in combination with a high bypass ratio engine mounted on the wing
BIMOD Investigation of oscillating high-lift flaps for increasing maximum lift
CeRAS Central Reference Aircraft data System
Dachwirbel Experimental and numerical investigation of the interaction of wake vortices with gable roofs
E-DARIT In-flight measurement of electric propulsion systems in propulsion and recovery mode and concluding construction and design recommendations: Psychoacoustic investigation of propellers
FLEXOP Derivation of methods for the design and consideration of flutter-free wings by active load control
FORMIC Estimation of the climate impact of formation flight under consideration of realistic modelling of technological influences and operational processes on system level as well as in the formation
GNOSIS Holistic evaluation of electric flying taking into account a life cycle analysis
MVDC Design and evaluation of system architectures for electrically powered aircraft
Near-Wake of Bluff Bodies Experimental investigations of the flow of bluff bodies and its change due to slip angles
HYFLY System investigation of distributed hybrid propulsion systems for aircraft consisting of a reluctance generator coupled with a high-speed gas turbine, battery and electric motors with high power density
PAKO Psychoacoustic Optimization of Airplanes
RINGO Identification of research infrastructure needs, gaps and overlaps for the aviation sector in Europe with respect to fulfilment of the goals specified in the strategy document Flightpath 2050
TeDiMo Establishing a technology diffusion model in the context of the Technology Evaluator that facilitates the investigation of the propagation of new technologies developed in Clean Sky 2
Twin-Helix Dynamics and instabilities of helical vortex pairs
Vortex Design by Wingtip Shaping Experimental and numerical investigation of the influence of wing tip geometry on the velocity components of wake vortices in the near field