@inproceedings{JunkGawronSchroeder2019,
  author    = {Stefan Junk and Philipp Gawron and Werner Schr{\"o}der},
  title     = {Development of an Additively Manufactured Adaptive Wing Using Digital Materials},
  series = {Sustainable Design and Manufacturing 2019 : Proceedings of the 6th International Conference on Sustainable Design and Manufacturing (KES-SDM 19)},
  volume    = {SIST 155},
  editor    = {Peter Ball and Luisa Huaccho Huatuco and Robert J. Howlett and Rossi Setchi},
  edition   = {1.},
  publisher = {Springer},
  address   = {Singapore},
  isbn      = {978-981-13-9270-2 (Hardcover)},
  doi       = {10.1007/978-981-13-9271-9\_5},
  pages     = {49 -- 59},
  year      = {2019},
  abstract  = {The ability to change aerodynamic parameters of airfoils during flying can potentially save energy as well as reducing the noise made by the unmanned aerial vehicles (UAV) because of sharp edges of the airfoil and its rudders. In this paper, an approach for the design of an adaptive wing using a multi-material 3D printer is shown. In multi-material 3D printing, up to six different materials can be combined in one component. Thus, the user can determine the mixture and the spatial arrangement of this “digital material” in advance in the pre-processing software. First, the theoretical benefits of adaptive wings are shown, and already existing adaptive wings and concepts are explicated within a literature review. Then the additive manufacturing process using photopolymer jetting and its capabilities to print multiple materials in one part are demonstrated. Within the scope of a case study, an adaptive wing is developed and the necessary steps for the product development and their implementation in CAD are presented. This contribution covers the requirements for different components and sections of an adaptive wing designed for additive manufacturing using multiple materials as well as the single steps of development with its different approaches until the final design of the adaptive wing. The developed wing section is simulated, and qualitative tests in a wind tunnel are carried out with the wing segment. Finally, the additively manufactured wing segment is evaluated under technical and economic aspects.},
  language  = {en}
}