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Document type:
Konferenzbeitrag 
Contribution type:
Textbeitrag / Aufsatz 
Author(s):
Roessler, Christian; Stahl, Philipp; Sendner, Franz; Hermanutz, Andreas; Koeberle, Sebastian; Bartasevicius, Julius; Rozov, Vladyslav; Breitsamter, Christian; Hornung, Mirko; Meddaikar, Yasser M.; Dillinger, Johannes; Sodja, Jurij; De Breuker, Roeland; Koimtzoglou, Christos; Kotinis, Dimitrios; Georgopoulos, Panagiotis 
Title:
Aircraft Design and Testing of FLEXOP Unmanned Flying Demonstrator to Test Load Alleviation and Flutter Suppression of High Aspect Ratio Flexible Wings 
Abstract:
The idea of the EU funded FLEXOP project is to raise efficiency of a currently existing wing by derivative solution with higher aspect ratio at no excess structural weight. In order to enable such a resulting highly flexible wing the project goal is to develop methods for active suppression of flutter and passive load alleviation. The developed methods will be tested and validated with a UAV flutter demonstrator. The demonstrator is a 7m wingspan, 65kg MTOW UAV equipped with a jet engine. After...    »
 
Dewey Decimal Classification:
620 Ingenieurwissenschaften 
Horizon 2020:
636307 
Book / Congress title:
AIAA Scitech 2019 Forum 
Publisher:
American Institute of Aeronautics and Astronautics 
Date of publication:
06.01.2019 
Year:
2020 
Covered by:
Scopus 
Print-ISBN:
9781624105784 
Language:
en 
Fulltext / DOI:
TUM Institution:
Lehrstuhl für Aerodynamik und Strömungsmechanik