Stability and rational design of the «barrelogive» type strengthened shell structures under combined loading
DOI:
https://doi.org/10.15587/1729-4061.2020.209228Keywords:
shell, barrel-ogive structure, external pressure, axial compression, intermediate framesAbstract
This paper reports a study into the stability of a shell structure of the barrel-ogive type, supported by the discretely arranged intermediate frames, under the joint action of the uniform external pressure and axial compressive efforts.
A case of the sinusoidal approximation of the meridian of the middle surface of shell compartments has been considered.
Governing differential equations have been built to study the stability of a compound shell structure taking into consideration the curvature radii of the "barrel" and "ogive" compartments under the joint action of axial compression and uniform external pressure. A finite difference method has been used to integrate the fourth-order governing equations with variable coefficients. It is shown that an increase in the meridian curvature parameter exceeding 4 % leads, in some cases that involve the loading by axial forces, to an increase in the critical external pressure by 1.5‒2 times.
The effect of stabilizing the growth of critical pressure with an increase in the rigidity of the frames is illustrated for the different values of the meridian curvature and the number of supporting elements. A given effect makes it possible to draw conclusions about the possibility of determining the rational rigidity characteristics of the structure.
The effect of increasing critical pressure in the presence of a compressive force in the shells of the positive Gauss curvature, which is the result of internal stretching efforts in the circumference direction, has been investigated. In this case, a generatrix deviation from the ideal shape leads to an increase in wavenumbers in the circumferential direction while the stability is lost, which indicates an increase in the critical pressure. A further increase in the axial compression of the structure leads to the emergence of annular compressive efforts, which is a consequence of the reduction in the critical stresses of external pressureReferences
- Bai, X., Tang, R., Zan, Y., Li, J. (2019). Stability analysis of a cylindrical shell with axially symmetric defects under axial compression based on the reduction stiffness method. Ocean Engineering, 193, 106584. doi: https://doi.org/10.1016/j.oceaneng.2019.106584
- Bai, X., Xu, W., Ren, H., Li, J. (2017). Analysis of the influence of stiffness reduction on the load carrying capacity of ring-stiffened cylindrical shell. Ocean Engineering, 135, 52–62. doi: https://doi.org/10.1016/j.oceaneng.2017.02.034
- Tafreshi, A., Bailey, C. G. (2007). Instability of imperfect composite cylindrical shells under combined loading. Composite Structures, 80(1), 49–64. doi: https://doi.org/10.1016/j.compstruct.2006.02.031
- Teng, J. G., Barbagallo, M. (1997). Shell restraint to ring buckling at cone-cylinder intersections. Engineering Structures, 19 (6), 425–431. doi: https://doi.org/10.1016/s0141-0296(96)00087-9
- Schmidt, H. (2018). Two decades of research on the stability of steel shell structures at the University of Essen (1985–2005): Experiments, evaluations, and impact on design standards. Advances in Structural Engineering, 21 (16), 2364–2392. doi: https://doi.org/10.1177/1369433218756273
- Zhao, Y., Teng, J. G. (2003). A stability design proposal for cone–cylinder intersections under internal pressure. International Journal of Pressure Vessels and Piping, 80 (5), 297–309. doi: https://doi.org/10.1016/s0308-0161(03)00048-6
- Iqbal, M. A., Tiwari, G., Gupta, P. K. (2016). Energy dissipation in thin metallic shells under projectile impact. European Journal of Mechanics - A/Solids, 59, 37–57. doi: https://doi.org/10.1016/j.euromechsol.2016.03.004
- Amabili, M. (2018). Nonlinear vibrations and stability of laminated shells using a modified first-order shear deformation theory. European Journal of Mechanics - A/Solids, 68, 75–87. doi: https://doi.org/10.1016/j.euromechsol.2017.11.005
- Akimov, D. V., Gryshchak, V. Z., Gomenyuk, S. I., Larionov, I. F., Klimenko, D. V., Sirenko, V. N. (2016). Finite-Element Analysis and Experimental Investigation on the Strength of a Three-Layer Honeycomb Sandwich Structure of the Spacecraft Adapter Module. Strength of Materials, 48 (3), 379–383. doi: https://doi.org/10.1007/s11223-016-9775-y
- Degtyarenko, P. G., Grishchak, V. Z., Grishchak, D. D., Dyachenko, N. M. (2019). To equistability problem of the reinforced shell structure under combined loading. Space Science and Technology, 25 (6 (121)), 3–14. doi: https://doi.org/10.15407/knit2019.06.003
- Degtyarev, M. A., Shapoval, A. V., Gusev, V. V., Avramov, K. V., Sirenko, V. N. (2019). Structural Optimization of Waffle Shell Sections in Launch Vehicles. Strength of Materials, 51 (2), 223–230. doi: https://doi.org/10.1007/s11223-019-00068-7
- Degtyarenko, P. G., Gristchak, V. Z., Gristchak, D. D., Dyachenko, N. M. (2020). Statement and basic solution equationsof the stability problem for the shell-designed type "barrel-revived" under external pressure. Problems of Computational Mechanics and Strength of Structures, 1 (30), 33–52. doi: https://doi.org/10.15421/4219025
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