Buckling of circular cylindrical shells subject to uniform lateral pressure

Buckling under the external pressure of cylindrical shells with variable thickness

“…In case of finite cylinders, we compare the buckling loads obtained from (34) with results of Vodenitcharova and Ansourian investigation, based on Flugge's stability equations in couple form (Vodenitcharova and Ansourian, 1996) for simply supported (S-S) shells, as shown in Table 1.…”

On the solution of the buckling problem of functionally graded truncated conical shells with mixed boundary conditions

“…(15) and (16), after integrating with respect to x and some operations, the expressions for non-dimensional critical lateral and hydrostatic pressures of FGM truncated conical shells, which the small and large ends satisfied the boundary conditions (2) and (3), respectively, are found. The resulting expressions will be similar to the expressions (19) and (20). For this case, instead of S 2 is written S 1 and the boundaries of integrals varied from 0 to 0 x in Eqs.…”

“….... (20) The minimum values of the non-dimensional critical uniform hydrostatic and lateral pressures are obtained by minimizing Eqs. (19) and (20), respectively, with respect to n and λ.…”

“…These books contain a brief summary of the buckling and vibration studies that have reported to date books [16,17]. A recent review on the progress of research on the buckling of conical shells can be found in [18][19][20][21].…”

Dynamic local and global buckling of cylindrical shells under axial impact

“…Lancaster et al [6] discussed new issues both for better understanding of buckling phenomena and for rational design of shells by engineers against buckling by experiments. A number of researchers [7][8][9][10][11] undertook numerical and experimental investigation for buckling and post-buckling behavior of thin-walled cylindrical steel shells with varying thickness subjected to uniform external pressure. Singer et al [12] presented the theory and experiment of post-buckling of shells under dynamic loads and further analyzed buckling of shells.…”