| 摘要 |
A skin (1) for a morphing structure of an aircraft is disclosed, said skin comprising one or more corrugations (2). A corresponding method of manufacturing a skin for a morphing structure of an aircraft is also disclosed comprising shaping the skin (1) to a desired form including one or more corrugations (2). In one embodiment, Aluminium forming bars (5) are sequentially introduced between folds (7, 8) in the material of the skin. |
