Modelling aeroelastic deformation of soft wing membrane kites
J.A.W. Poland (TU Delft - Aerospace Engineering)
R. Schmehl – Mentor (TU Delft - Wind Energy)
Carlos Simao Ferreira – Graduation committee member (TU Delft - Wind Energy)
J. Sodja – Graduation committee member (TU Delft - Aerospace Structures & Computational Mechanics)
More Info
expand_more
Other than for strictly personal use, it is not permitted to download, forward or distribute the text or part of it, without the consent of the author(s) and/or copyright holder(s), unless the work is under an open content license such as Creative Commons.
Abstract
Several structural models that could serve as building blocks for a next-generation FSI-based kite design tool have been developed. The models represent the leading-edge inflatable V3 soft wing membrane kite of Kitepower B.V., by using a wireframe multi-plate representation. Where the shape deformations are calculated using bridle line system models. Both by using a trilateration algorithm and a particle system model were accurate results found. Accurate in comparison to the experimentally obtained data from a photogrammetry analysis. The existence of slack and its non-dependence on empirical relations made the force-based particle system model best.