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Abstract

The buckling of laminated composite spherical shell cap with and without a cutout subjected to transverse load is investigated. The geometrical non-linear analysis is carried out using the finite element method based on the first-order shear deformation theory. An eight noded degenerated isoparametric shell element with five degrees of freedom at each node is considered. The geometric non-linear behaviour and the collapse pressures with the associated mode shapes are presented for simply supported and clamped symmetrically and anti-symmetrically laminated cross-ply spherical shell cap without a cutout subjected to uniform normal pressure. The dependence of collapse pressure on the size of a central circular cutout is also studied.

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How to Cite
Sai Ram, K. (2023). Buckling of Laminated Composite Spherical Shell Cap. Journal of Aerospace Sciences and Technologies, 57(2), 259–269. https://doi.org/10.61653/joast.v57i2.2005.763

References

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