Technical Papers
Apr 17, 2020

Mixed Finite-Element Formulation Based on Refined Sinusoidal Model for Buckling of Layered Beams

Publication: Journal of Aerospace Engineering
Volume 33, Issue 4

Abstract

In the last 3 decades, sinusoidal theory has been increasingly utilized to research mechanical behaviors of layered composite and sandwich structures. Nevertheless, the existing sinusoidal model will encounter trouble in precisely yielding the buckling loads of layered structures composed of layers with different material properties. Thus, a refined sinusoidal model is offered for the buckling analysis of composite and sandwich structures that can simulate the zigzag effect of the in-plane displacement and meet the free conditions of transverse shear stresses on the surfaces. In the light of the elegant sinusoidal model, a three-node beam element has been constructed to work out the discrete eigenvalue equation coming from the stability behavior. Making use of a mixed variational theorem from the literature, the finite-element formulation can meet beforehand the continuous conditions of transverse stress at the interfaces. The three-dimensional finite element method (3D-FEM) results are utilized to evaluate the precision and efficiency of the proposed approach through a numerical example. The proposed finite-element formulation can produce satisfactory results with lower calculational cost, and some interesting conclusions are presented. However, the results for stability of layered structures made of plies with different material properties will be overestimated by utilizing the models violating the continuous prerequisite of interlaminar stresses.

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Data Availability Statement

All data, models, and code generated or used during the study appear in the published article.

Acknowledgments

The work described in this paper was supported by the National Natural Sciences Foundation of China (Nos. 11402152 and 11572204), and the Natural Science Foundation in Shaanxi Province (No. 2019JQ-909).

References

Ali, J., K. Bhaskar, and T. Varadan. 1999. “A new theory for accurate thermal/mechanical flexural analysis of symmetrically laminated plates.” Compos. Struct. 45 (3): 227–232. https://doi.org/10.1016/S0263-8223(99)00028-8.
Anand, V., S. Natarajan, K. Ramajeyathilagam, and M. Ganapathi. 2014. “Assessment of certain higher-order structural models based on global approach for bending analysis of curvilinear composite laminates.” Compos. Struct. 118 (Dec): 548–559. https://doi.org/10.1016/j.compstruct.2014.07.045.
Ansari, M. I., and A. Kumar. 2019. “Flexural analysis of functionally graded CNT-reinforced doubly curved singly ruled composite truncated cone.” J. Aerosp. Eng. 32 (2): 04018154. https://doi.org/10.1061/(ASCE)AS.1943-5525.0000988.
Carrera, E. 2000. “An assessment of mixed and classical theories for the thermal stress analysis of orthotropic multilayered plates.” J. Therm. Stresses 23 (9): 797–831. https://doi.org/10.1080/014957300750040096.
Carrera, E. 2002. “Temperature profile influence on layered plates response considering classical and advanced theories.” AIAA J. 40 (9): 1885–1896. https://doi.org/10.2514/2.1868.
Carrera, E. 2003. “Historical review of zig-zag theories for multilayered plates and shells.” Appl. Mech. Rev. 56 (3): 287–308. https://doi.org/10.1115/1.1557614.
Carrera, E. 2004. “On the use of the Murakami’s zig-zag function in the modeling of layered plates and shells.” Comput. Struct. 82 (7–8): 541–554. https://doi.org/10.1016/j.compstruc.2004.02.006.
Chaubey, A. K., I. Jha, A. Kumar, M. D. Demirbas, and S. Dey. 2018. “Dual-axis buckling of laminated composite skew hyperbolic paraboloids with openings.” J. Braz. Soc. Mech. Sci. Eng. 40 (10): 490. https://doi.org/10.1007/s40430-018-1406-z.
Cinefra, M., M. Petrolo, G. Li, and E. Carrera. 2017. “Variable kinematic shell elements for composite laminates accounting for hygrothermal effects.” J. Therm. Stresses 40 (12): 1523–1544. https://doi.org/10.1080/01495739.2017.1360165.
Cinefra, M., S. Valvano, and E. Carrera. 2016. “Thermal stress analysis of laminated structures by a variable kinematic MITC9 shell element.” J. Therm. Stresses 39 (2): 121–141. https://doi.org/10.1080/01495739.2015.1123591.
Dafedar, J. B., and Y. M. Desai. 2004. “Stability of composite and sandwich struts by mixed formulation.” J. Eng. Mech. 130 (7): 762–770. https://doi.org/10.1061/(ASCE)0733-9399(2004)130:7(762).
Demasi, L. 2005. “Refined multilayered plate elements based on Murakami zig-zag functions.” Compos. Struct. 70 (3): 308–316. https://doi.org/10.1016/j.compstruct.2004.08.036.
Gherlone, M., A. Tessler, and M. Di Sciuva. 2011. “C0 beam elements based on the refined zigzag theory for multilayered composite and sandwich laminates.” Compos. Struct. 93 (11): 2882–2894. https://doi.org/10.1016/j.compstruct.2011.05.015.
Hu, H. C. 1955. On some variational principle in the theory of elasticity and plasticity. 33–54. Beijing: Scientia Sinica.
Iurlaro, L., M. Gherlone, M. Di Sciuva, and A. Tessler. 2015. “Refined zigzag theory for laminated composite and sandwich plates derived from Reissner’s mixed variational theorem.” Compos. Struct. 133 (Dec): 809–817. https://doi.org/10.1016/j.compstruct.2015.08.004.
Kant, T., and H. S. Patil. 1991. “Buckling loads of sandwich columns with a higher-order theory.” J. Reinf. Plast. Compos. 10 (1): 102–109. https://doi.org/10.1177/073168449101000107.
Kapuria, S., P. C. Dumir, and N. K. Jain. 2004. “Assessment of zigzag theory for static loading, buckling, free and forced response of composite and sandwich beams.” Compos. Struct. 64 (3–4): 317–327. https://doi.org/10.1016/j.compstruct.2003.08.013.
Kumar, A., A. Chakrabarti, and P. Bhargava. 2013. “Vibration of laminated composites and sandwich shells based on higher order zigzag theory.” Eng. Struct. 56 (Nov): 880–888. https://doi.org/10.1016/j.engstruct.2013.06.014.
Makhecha, D., M. Ganapathi, and B. Patel. 2001. “Dynamic analysis of laminated composite plates subjected to thermal/mechanical loads using an accurate theory.” Compos. Struct. 51 (3): 221–236. https://doi.org/10.1016/S0263-8223(00)00133-1.
Murakami, H. 1986. “Laminated composite plate theory with improved in-plane response.” J. Appl. Mech. 53 (3): 661–666. https://doi.org/10.1115/1.3171828.
Pagano, N. J. 1970. “Exact solutions for rectangular bi-directional composites.” J. Compos. Mater. 4 (1): 20–34. https://doi.org/10.1177/002199837000400102.
Patel, B. P., M. Ganapathi, and D. P. Makhecha. 2002. “Hygrothermal effects on the structural behaviour of thick composite laminates using higher-order theory.” Compos. Struct. 56 (1): 25–34. https://doi.org/10.1016/S0263-8223(01)00182-9.
Rah, K., W. Van Paepegem, A. M. Habraken, and J. Degrieck. 2012. “A mixed solid-shell element for the analysis of laminated composites.” Int. J. Numer. Methods Eng. 89 (7): 805–828. https://doi.org/10.1002/nme.3263.
Reddy, J. N. 1984. “A simple higher-order theory for laminated composite plates.” J. Appl. Mech. 51 (4): 745–752. https://doi.org/10.1115/1.3167719.
Reissner, E. 1984. “On a certain mixed variational theorem and a proposed application.” Int. J. Numer. Methods Eng. 20 (7): 1366–1368. https://doi.org/10.1002/nme.1620200714.
Robaldo, A. 2006. “Finite element analysis of the influence of temperature profile on thermoelasticity of multilayered plates.” Comput. Struct. 84 (19–20): 1236–1246. https://doi.org/10.1016/j.compstruc.2006.01.022.
Sayyad, A. S., and Y. M. Ghugal. 2017. “Bending, buckling and free vibration of laminated composite and sandwich beams: A critical review of literature.” Compos. Struct. 171 (Jul): 486–504. https://doi.org/10.1016/j.compstruct.2017.03.053.
Sayyad, A. S., and Y. M. Ghugal. 2018. “Effect of thickness stretching on the static deformations, natural frequencies, and critical buckling loads of laminated composite and sandwich beams.” J. Braz. Soc. Mech. Sci. Eng. 40 (6): 296. https://doi.org/10.1007/s40430-018-1222-5.
Sze, K. Y., R. G. Chen, and Y. K. Cheung. 1998. “Finite element model with continuous transverse shear stress for composite laminates in cylindrical bending.” Finite Elem. Anal. Des. 31 (2): 153–164. https://doi.org/10.1016/S0168-874X(98)00056-0.
Tessler, A. 2015. “Refined zigzag theory for homogeneous, laminated composite and sandwich beams derived from Reissner’s mixed variational principle.” Meccanica 50 (10): 2621–2648. https://doi.org/10.1007/s11012-015-0222-0.
Thai, H. T., and D. H. Choi. 2013. “Efficient higher-order shear deformation theories for bending and free vibration analysis of functionally graded plates.” Arch. Appl. Mech. 83 (12): 1755–1771. https://doi.org/10.1007/s00419-013-0776-z.
Toledano, A., and H. Murakami. 1987. “A higher-order laminated plate theory with improved in-plane response.” Int. J. Solids Struct. 23 (1): 111–131. https://doi.org/10.1016/0020-7683(87)90034-5.
Touratier, M. 1991. “An efficient standard plate theory.” Int. J. Eng. Sci. 29 (8): 901–916. https://doi.org/10.1016/0020-7225(91)90165-Y.
Versino, D., M. Gherlone, and M. Di Sciuva. 2014. “Four-node shell element for doubly curved multilayered composites based on the refined zigzag theory.” Compos. Struct. 118 (Dec): 392–402. https://doi.org/10.1016/j.compstruct.2014.08.018.
Vo, T. P., H. T. Thai, and F. Inam. 2013. “Axial-flexural coupled vibration and buckling of composite beams using sinusoidal shear deformation theory.” Arch. Appl. Mech. 83 (4): 605–622. https://doi.org/10.1007/s00419-012-0707-4.
Wang, Y., and D. Wu. 2017. “Free vibration of functionally graded porous cylindrical shell using a sinusoidal shear deformation theory.” Aerosp. Sci. Technol. 66 (Jul): 83–91. https://doi.org/10.1016/j.ast.2017.03.003.
Washizu, K. 1955. On some variational principle in the theory of elasticity and plasticity. Cambridge, MA: Massachusetts Institute of Technology.
Wu, Z., and W. J. Chen. 2008. “An assessment of several displacement-based theories for the vibration and stability analysis of laminated composite and sandwich beams.” Compos. Struct. 84 (4): 337–349. https://doi.org/10.1016/j.compstruct.2007.10.005.
Yang, W. L., and D. He. 2018. “Bending, free vibration and buckling analysis of anisotropic layered micro-plates based on a new size-dependent model.” Compos. Struct. 189 (Apr): 137–147. https://doi.org/10.1016/j.compstruct.2017.09.057.
Zamani, A., and M. R. Bidgoli. 2017. “Vibration analysis of concrete foundations retrofit with NFRP layer resting on soil medium using sinusoidal shear deformation theory.” Soil Dyn. Earthquake Eng. 103 (Dec): 141–150. https://doi.org/10.1016/j.soildyn.2017.09.018.
Zenkour, A. M. 2012. “Hygrothermal effects on the bending of angle-ply composite plates using a sinusoidal theory.” Compos. Struct. 94 (12): 3685–3696. https://doi.org/10.1016/j.compstruct.2012.05.033.
Zenkour, A. M. 2014. “Simplified theory for hygrothermal response of angle-ply composite plates.” AIAA J. 52 (7): 1466–1473. https://doi.org/10.2514/1.J052631.
Zhao, D. L., Z. Wu, and X. H. Ren. 2019. “New sinusoidal higher-order theory including the zig-zag function for multilayered composites.” J. Aerosp. Eng. 32 (3): 04019009. https://doi.org/10.1061/(ASCE)AS.1943-5525.0000994.

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Go to Journal of Aerospace Engineering
Journal of Aerospace Engineering
Volume 33Issue 4July 2020

History

Received: Jul 26, 2019
Accepted: Nov 6, 2019
Published online: Apr 17, 2020
Published in print: Jul 1, 2020
Discussion open until: Sep 17, 2020

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Ren Xiaohui
Professor, School of Mechanical Engineering, Xi’ an Aeronautical Univ., Xian 710065, China.
Professor, School of Aeronautics, Northwestern Polytechnical Univ., Xian 710072, China (corresponding author). Email: [email protected]

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