2005
DOI: 10.1016/j.tws.2005.03.006
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Reduced stiffness buckling of sandwich cylindrical shells under uniform external pressure

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Cited by 30 publications
(8 citation statements)
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“…It is clear that we have 3 × N × Q algebraic equations at boundary and domain grid points. The value of the buckling pressure is obtained by solving the standard eigenvalue equation presented in the partitioned form as: (25) can be treated as a conventional eigenvalue problem to obtain the buckling pressure and the corresponding mode shapes of the system.…”
Section: The Calculation Of Buckling Loadmentioning
confidence: 99%
See 1 more Smart Citation
“…It is clear that we have 3 × N × Q algebraic equations at boundary and domain grid points. The value of the buckling pressure is obtained by solving the standard eigenvalue equation presented in the partitioned form as: (25) can be treated as a conventional eigenvalue problem to obtain the buckling pressure and the corresponding mode shapes of the system.…”
Section: The Calculation Of Buckling Loadmentioning
confidence: 99%
“…An approximate analytical solution for the buckling of the composite sandwich cylindrical shell with clamped ends under uniform external pressure has been presented by Lopatin and Morozov [19]. Ohga et al [25] have applied the reduced stiffness lower bound method to solve the buckling problem of the sandwich cylindrical shell with simply supported ends. Stability of long cylindrical sandwich shells with different facings subjected to a lateral external pressure has been carried out by Birman and Simitres [6].…”
Section: Introductionmentioning
confidence: 99%
“…This geometry is reinforced with carbon nanotube, and the material properties of the nanocomposite plates are estimated through the Mori-Tanaka approach. Ohga et al [21] analyzed the reduced stiffness buckling of the sandwich cylindrical shells under uniform external pressure and solved with FE method. Polit et al [22] studied the elastic stability and bending of FG graphene-reinforced porous nanocomposite curved beams applying HSDT with thickness stretch effect.…”
Section: Introductionmentioning
confidence: 99%
“…Kardomateas and Simitses [2002; studied analytically the buckling of long sandwich cylindrical shells under external pressure. Ohga et al [2005] studied, both numerically and analytically, the reduced stiffness buckling of sandwich cylindrical shells under uniform external pressure. Sato and Patel [2007] and Sato et al [2008] studied the buckling behavior of a PIP system under hydrostatic pressure and developed a simplified solution for estimating a PIP system's buckling capacity.…”
Section: Introductionmentioning
confidence: 99%