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The effect of different geometrical imperfection of buckling of composite cylindrical shells subjected to axial loading

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Figure

Table 1 Mechanical properties of the CFRP
Fig. 2 Buckling modes and loads obtained through static analysis ofmodels without imperfections
Fig. 4 Variation of initial imperfection (−2 mm, 2 mm) of the outer surface of the cylindrical shell (Priyadarsini et al
Fig. 6 Curve number 2 in Figure of 4 instead of Comparison of effects of different value of imperfection on load of buckling of composite cylindrical shell
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