Abstract
Based on a boundary layer theory of shell buckling, the semi-analytical solutions for nonlinear stability analysis of anisotropic laminated composite doubly-curved shells with rectangular planform subjected to lateral pressure are derived. A new shell model of arbitrary constant curvature and fibre stacking sequences but constant thickness is developed. The governing equations are based on an extended higher-order shear deformation shell theory with von Kármán-type of kinematic nonlinearity and including the effect on stiffness couplings. The nonlinear deformation and initial deflection of shells are both taken into account. The boundary layer equations of buckling for doubly-curved shells are introduced to match the asymptotic solutions satisfying the clamped or simply-supported boundary condition. The closed-form solutions for buckling and postbuckling analysis of an anisotropic shear deformable laminated doubly-curved panel are obtained by the two-step perturbation methods and the boundary layer theory for shell buckling, which is employed to determine interactive buckling loads and postbuckling equilibrium paths. At the same time, the internal quantitative relationship in the asymptotic sense between deflection and rotations of the normal to the middle surface is for the first time obtained. The influences of anisotropic lay-up, change in the stacking sequence, temperature variation, different types of elastic foundation and boundary condition on nonlinear stability behaviour are analysed and discussed. The study provides a good theoretical method for the load-carrying capacity design of composite shell structures.
Similar content being viewed by others
References
Yamada, S.: Buckling analysis for design of pressurized cylindrical shell panels. Eng. Struct. 19(5), 352–359 (1997). https://doi.org/10.1016/S0141-0296(96)00093-4
Han, B., Simitses, G.J.: Analysis of anisotropic laminated cylindrical shells subjected to destabilizing loads. Part II: Numer Results Compos. Struct. 19(2), 183–205 (1991). https://doi.org/10.1016/0263-8223(91)90022-Q
Reddy, J.N.: Exact solutions of moderately thick laminated shells. J. Eng. Mech. 110(5), 794–809 (1984). https://doi.org/10.1061/(ASCE)0733-9399(1984)110:5(794)
Fu, L., Waas, A.M.: Initial post-buckling behaviour of thick rings under uniform external hydrostatic pressure. J. Appl. Mech. 62(2), 338–345 (1995). https://doi.org/10.1115/1.2895936
Simitses, G.J.: Buckling of moderately thick laminated cylindrical shells: a review. Compos. B Eng. 27(6), 581–587 (1996). https://doi.org/10.1016/1359-8368(95)00013-5
Leissa, A.W., Chang, J.D.: Elastic deformation of thick, laminated composite shells. Compos. Struct. 35(2), 153–170 (1996). https://doi.org/10.1016/0263-8223(96)00028-1
Qatu, M.S.: Accurate equations for laminated composite deep thick shells. Int. J. Solids Struct. 36(19), 2917–2941 (1999). https://doi.org/10.1016/S0020-7683(98)00134-6
Amabili, M., Reddy, J.N.: A new non-linear higher-order shear deformation theory for large-amplitude vibrations of laminated doubly curved shells. Int. J. Nonlinear Mech. 45(4), 409–418 (2010). https://doi.org/10.1016/j.ijnonlinmec.2009.12.013
Bahadori, R., Najafizadeh, M.M.: Free vibration analysis of two-dimensional functionally graded axisymmetric cylindrical shell on Winkler-Pasternak elastic foundation by First-order Shear Deformation Theory and using Navier-differential quadrature solution methods. Appl. Math. Model. 39(16), 4877–4894 (2015). https://doi.org/10.1016/j.apm.2015.04.012
Ikeda, K., Murota, K.: Asymptotic and probabilistic approach to buckling of structures and materials. Appl. Mech. Rev. (2008). https://doi.org/10.1115/1.2939583
Caliri, M.F., Ferreira, A.J.M., Tita, V.: A review on plate and shell theories for laminated and sandwich structures highlighting the finite element method. Compos. Struct. 156, 63–77 (2016). https://doi.org/10.1016/j.compstruct.2016.02.036
Singh, V.K., Mahapatra, T.R., Panda, S.K.: Nonlinear flexural analysis of single/doubly curved smart composite shell panels integrated with PFRC actuator. Eur. J. Mech. A. Solids 60, 300–314 (2016). https://doi.org/10.1016/j.euromechsol.2016.08.006
Quan, T.Q., Cuong, N.H., Duc, N.D.: Nonlinear buckling and post-buckling of eccentrically oblique stiffened sandwich functionally graded double curved shallow shells. Aerosp. Sci. Technol. 90, 169–180 (2019). https://doi.org/10.1016/j.ast.2019.04.037
Mikhasev, G., Botogova, M.: Effect of edge shears and diaphragms on buckling of thin laminated medium-length cylindrical shells with low effective shear modulus under external pressure. Acta Mech. 228(6), 2119–2140 (2017). https://doi.org/10.1007/s00707-017-1825-4
Shahgholian, D., Safarpour, M., Rahimi, A.R., et al.: Buckling analyses of functionally graded graphene-reinforced porous cylindrical shell using the Rayleigh-Ritz method. Acta Mech. 231, 1887–1902 (2020). https://doi.org/10.1007/s00707-020-02813-5
Dastjerdi, S., Akgöz, B., Civalek, Ö., et al.: Eremeyevde: On the non-linear dynamics of torus-shaped and cylindrical shell structures. Int. J. Eng. Sci. 156, 103371 (2020). https://doi.org/10.1016/j.ijengsci.2020.103371
Phuong, N.T., Trung, N.T., Doan, C.V., et al.: Nonlinear thermomechanical buckling of FG-GRC laminated cylindrical shells stiffened by FG-GRC stiffeners subjected to external pressure. Acta Mech. 231, 5125–5144 (2020). https://doi.org/10.1007/s00707-020-02813-5
Shah, P.H., Batra, R.C.: Stress singularities and transverse stresses near edges of doubly curved laminated shells using TSNDT and stress recovery scheme. Eur. J. Mech. A. Solids 63, 68–83 (2017). https://doi.org/10.1016/j.euromechsol.2016.11.007
Panda, H.S., Sahu, S.K., Parhi, P.K.: Hygrothermal response on parametric instability of delaminated bidirectional composite flat panels. Eur. J. Mech. A. Solids 53, 268–281 (2015). https://doi.org/10.1016/j.euromechsol.2015.05.004
Ji, H.J., Li, L.F.: Numerical methods for thermally stressed shallow shell equations. J. Comput. Appl. Math. 362(15), 626–652 (2019). https://doi.org/10.1016/j.cam.2018.10.005
Carrera E., Brischetto S., Nali P.: Plates and Shells for Smart Structures: Classical and Advanced Theories for Modeling and Analysis. John Wiley & Sons, Ltd, (2011): i-xi. https://doi.org/10.1002/9781119950004
Weaver, P.M., Driesen, J.R., Roberts, P.: Anisotropic effects in the compression buckling of laminated composite cylindrical shells. Compos. Sci. Technol. 62(1), 91–105 (2002). https://doi.org/10.1016/S0266-3538(01)00186-5
Wong, K.F.W., Weaver, P.M.: Approximate solution for the compression buckling of fully anisotropic cylindrical shells. AIAA J. 43(12), 2639–2645 (2005). https://doi.org/10.2514/1.10924
Qatu, M.S.: Vibration of Laminated Shells and Plates. Academic Press, Oxford (2004)
Reddy, J.N.: Mechanics of Laminated Composite Plates and Shells: Theory and Analysis, 2nd edn. CRC Press, Boca Raton (2003)
Kolahchi, R., Zhu, S., Keshtegar, B., et al.: Dynamic buckling optimization of laminated aircraft conical shells with hybrid nanocomposite material. Aerosp. Sci. Technol. 98, 105656 (2020). https://doi.org/10.1016/j.ast.2019.105656
Paliwal, D.N., Pandey, R.K., Nath, T.: Free vibrations of circular cylindrical shell on Winkler and Pasternak foundations. Int. J. Press. Vessels Pip. 69(1), 79–89 (1996). https://doi.org/10.1016/0308-0161(95)00010-0
Reddy, J.N., Liu, C.F.: A higher-order shear deformation theory of laminated elastic shells. Int. J. Eng. Sci. 23(3), 319–330 (1985). https://doi.org/10.1016/0020-7225(85)90051-5
Li, Z., Lin, Z.: Non-linear buckling and postbuckling of shear deformable anisotropic laminated cylindrical shell subjected to varying external pressure loads. Compos. Struct. 92(2), 553–567 (2010). https://doi.org/10.1016/j.compstruct.2009.08.048
Li, Z., Liu, T., Yang, D.: Postbuckling behavior of shear deformable anisotropic laminated cylindrical shell under combined external pressure and axial compression. Compos. Struct. 198, 84–108 (2018). https://doi.org/10.1016/j.compstruct.2018.05.064
Batdorf S.B.: A simplified method of elastic-stability analysis for thin cylindrical shells[R]. NACA TR, 1947.
Redekop, D., Makhoul, E.: Use of the differential quadrature method for the buckling analysis of cylindrical shell panels. Struct. Eng. Mech. 10(5), 451–462 (2000). https://doi.org/10.12989/sem.2000.10.5.451
Shen, H.: Postbuckling of pressure-loaded shear deformable laminated cylindrical panels. Appl. Math. Mech. 24(4), 402–413 (2003). https://doi.org/10.1007/BF02439619
Budiansky, B.: Notes on nonlinear shell theory. J. Appl. Mech. 35(2), 393–401 (1968). https://doi.org/10.1115/1.3601208
Yuan, F.G., Hsieh, C.C.: Three-dimensional wave propagation in composite cylindrical shells. Compos. Struct. 42(2), 153–167 (1998). https://doi.org/10.1016/S0263-8223(98)00063-4
Wang, X., Lu, G., **ao, D.G.: Non-linear thermal buckling for local delamination near the surface of laminated cylindrical shell. Int. J. Mech. Sci. 44(5), 947–965 (2002). https://doi.org/10.1016/S0020-7403(02)00028-0
Acknowledgements
The work described in this paper is partially supported by the grants from the National Natural Science Foundation of China (Nos. 51775346, 52005334 and 51678360).
Author information
Authors and Affiliations
Corresponding author
Additional information
Publisher's Note
Springer Nature remains neutral with regard to jurisdictional claims in published maps and institutional affiliations.
Appendices
Appendix 1
In Eqs. (53)–(54)
In the above equations (with \(g_{ij}\) and \(g_{ijk}\) defined as in Li and Lin [29]),
for the case of curved edges clamped:
for the case of curved edges simply supported
Appendix 2
In Eq. (51)
Rights and permissions
About this article
Cite this article
Liu, T., Li, ZM. & Qiao, P. The closed-form solutions for buckling and postbuckling behaviour of anisotropic shear deformable laminated doubly-curved shells by matching method with the boundary layer of shell buckling. Acta Mech 232, 3277–3303 (2021). https://doi.org/10.1007/s00707-021-02952-3
Received:
Revised:
Accepted:
Published:
Issue Date:
DOI: https://doi.org/10.1007/s00707-021-02952-3