03.2 - Experimental Aerodynamics
ANALYSIS OF AN ELECTRICAL-POWERED-DUCTED-THRUST VECTORING-FLAP
V. Gollnick¹, J. Luehrmann¹, F. Danquah¹, A. Semke¹, T. Mueller¹, J. Thoeben¹; ¹Hamburg University of Technology, Germany
The Lilium-Jet is fascinating aviation community. However only a few technical information is available, the research question is about a better understanding of the design concept. An experimental study about the behaviour of the Ducted Fan Flap wing concept is presented. The experimental approach and achieved results are presented. A summary and perspective of the next steps is given.