Abstract:
The stability of equilibrium of a layered composite circular conical truncated shell loaded with uniform external pressure is investigated. A parametric analysis of the critical pressure intensities is carried out with allowance for the transverse shear, the moment character of the subcritical state of equilibrium, and the subcritical strains.
Citation:
A. N. Andreev, “Stability of a multilayered composite conical shell under uniform external pressure”, Prikl. Mekh. Tekh. Fiz., 40:4 (1999), 198–207; J. Appl. Mech. Tech. Phys., 40:4 (1999), 730–738
This publication is cited in the following 4 articles:
Mostafa Talebitooti, “Analytical and finite-element solutions for the buckling of composite sandwich conical shell with clamped ends under external pressure”, Arch Appl Mech, 87:1 (2017), 59
A.H. Sofiyev, N. Kuruoglu, “On the solution of the buckling problem of functionally graded truncated conical shells with mixed boundary conditions”, Composite Structures, 123 (2015), 282
A.H. Sofiyev, “On the vibration and stability of clamped FGM conical shells under external loads”, Journal of Composite Materials, 45:7 (2011), 771
A.H. Sofiyev, Z. Zerin, A. Korkmaz, “The stability of a thin three-layered composite truncated conical shell containing an FGM layer subjected to non-uniform lateral pressure”, Composite Structures, 85:2 (2008), 105