Hybrid modeling approach for the tether of an airborne wind energy system
UNICADO: multidisciplinary analysis in conceptual aircraft design
SystemXF: a novel approach for holistic system modeling in aircraft conceptual design
Acoustic pre-design studies of ducted fans for small aircraft
DC supply structure and protection concept for (hybrid) electric CS-25 aircraft
Ducted fans for hybrid electric propulsion of small aircraft
Model-based safety assessment for conceptual aircraft systems design
Determining infrastructure requirements for an air taxi service at Cologne Bonn Airport
Experimental investigation of a rotor blade tip vortex pair
Stabilization of the vertical take-off of a rigid flying wing for an airborne wind energy system
Conceptual design and comparison of hybrid electric propulsion systems for small aircraft
Technology selection for holistic analysis of hybrid-electric commuter aircraft