Print Email Facebook Twitter Deformation measurement in the wind tunnel for an UAV leading edge with a morphing mechanism Title Deformation measurement in the wind tunnel for an UAV leading edge with a morphing mechanism Author Radestock, M. (Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR)) Riemenschneider, J. (Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR)) Monner, H.P. (Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR)) Huxdorf, O. (Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR)) Werter, N.P.M. (TU Delft Aerospace Structures & Computational Mechanics) De Breuker, R. (TU Delft Aerospace Structures & Computational Mechanics) Date 2016 Abstract In a wind tunnel experiment a morphing wing with span extension and camber morphing was investigated. The considered aircraft is an unmanned aerial vehicle (UAV) with a span of 4 m. During the investigations a half wing model was analysed with pressure and structural measurement. The half wing model has three different morphing mechanisms. The focus is on the morphing leading edge concept, which will be shortly described with the main objectives. First of all the morphing leading edge will be described. Afterwards the results of the wind tunnel measurement for pressure distribution, balance and deformation measurement will be presented and discussed. To reference this document use: http://resolver.tudelft.nl/uuid:69b47a1d-0b0c-4279-ac71-f70a1b513a8f Source 30th Congress of International Council of the Aeronautical Sciences: Daejeon, Korea, Republic of Event 30th Congress of International Council of the Aeronautical Sciences, 2016-09-25 → 2016-09-30, Daejeon, Korea, Republic of Part of collection Institutional Repository Document type conference paper Rights © 2016 M. Radestock, J. Riemenschneider, H.P. Monner, O. Huxdorf, N.P.M. Werter, R. De Breuker Files PDF 2016_0166_paper.pdf 498.24 KB Close viewer /islandora/object/uuid:69b47a1d-0b0c-4279-ac71-f70a1b513a8f/datastream/OBJ/view