Answers are grounded in this paper and cite their sources.
This Note presents closed-farm solutions for axisymmetrical and axially unsymmetrical buckling of angle-ply laminated circular cylindrical shells under axial compression. The axisymmetrical and axially unsymmetrical buckling stress are found to be different from each other, and the best lamination angles which give the highest buckling stress are obtained.
No takes yet. Share an insight, caveat, or question.
Yoshiyuki Hirano (1979) studied this question.
Synapse has enriched 5 related papers. Consider them for comparative context: