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Linear buckling of shells with general boundary conditions

1Linear buckling of cylindrical shells under compression and torsion

Under pure compression, the shell buckles into an axisymmetric or diamond-shaped pattern (Yoshimura pattern), whereas under pure torsion, the shell deforms into a diagonal-shaped pattern with spiral wrinkles. Castro et al. Castro et al., 2014 and Lu et al. Lu et al., 2025 explores how these modes interact under combined loads, such as compression with pre-torsion or torsion with pre-compression. The interaction of axial and torsional loads creates a rich variety of behaviors:

Table 1:Post-Buckling Characteristics for Various Loading Conditions

Loading TypePost-Buckling PatternStability/Behavior
Pure CompressionDiamond-shapedHighly unstable; snapping occurs with decreasing NN.
Pure TorsionDiagonal-shapedSmooth path; load carrying capacity usually decreases.
Torsion + Pre-tensionDiagonal-shapedPre-tension increases the critical load and stabilizes the path.
Torsion + Pre-compressionTwisted DiamondLarge pre-compression triggers snapping and complex pattern transitions.

The next sections will discuss different implementations of this shell buckling problem.

References
  1. Castro, S. G. P., Mittelstedt, C., Monteiro, F. A. C., Arbelo, M. A., Ziegmann, G., & Degenhardt, R. (2014). Linear buckling predictions of unstiffened laminated composite cylinders and cones under various loading and boundary conditions using semi-analytical models. Composite Structures, 118, 303–315. 10.1016/j.compstruct.2014.07.037
  2. Lu, L., Leanza, S., Liu, Y., & Zhao, R. R. (2025). Buckling and post-buckling of cylindrical shells under combined torsional and axial loads. European Journal of Mechanics - A/Solids, 112, 105653. 10.1016/j.euromechsol.2025.105653