Hartwich, Tobias S.Tobias S.HartwichPanek, StefanStefanPanekWilckens, DirkDirkWilckensWille, TobiasTobiasWilleKrause, DieterDieterKrause2024-06-132024-06-132024-08-01Composite Structures 341: 118216 (2024)https://hdl.handle.net/11420/47839Thin-walled cylindrical shells under axial compression load are prone to buckling. The influencing factors leading to a reduction of the buckling load are a major design challenge. The sensitivity to imperfection increases with rising slenderness. In literature, cylinders with the same parameters and different slenderness are rarely tested in a larger number of samples. In this contribution, seven cylindrical shells, six of them nominally identical, are tested on two different test rigs and compared with twelve specimens with a smaller radius and same wall thickness from a previous series of tests. It is shown how the imperfection sensitivity is dependent on the R/t-ratio. Additionally, it is demonstrated how the quality of the test set ups corresponds with the achieved buckling load. Finally, the suitability of selected design approaches is determined based on the test results. Based on that, recommendations for the choice of a suitable approach are given.en0263-82232024Elsevierhttps://creativecommons.org/licenses/by/4.0/BucklingComposite shellsImperfectionsTest rigTechnology::620: Engineering::620.1: Engineering Mechanics and Materials ScienceTechnology::624: Civil Engineering, Environmental Engineering::624.1: Structural Engineering::624.17: Structural Analysis and DesignJournal Article10.15480/882.967110.1016/j.compstruct.2024.11821610.15480/882.9671Journal Article