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Buckling loads of axially compressed internally pressurized cylindrical shell with a crack at various angles

Fig. 10. (A)–(D) Normalized axial buckling load, γ, of a lined cracked cylindrical shell under uniform internal pressure versus the normalized loading parameter, λ, for different liner to shell thickness ratios, (tp/t), at crack angles of alpha = 0, 30, 60 and 90 degrees.

From the same paper as the previous slide.

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