Structural Engineering and Mechanics

Techno-Press (테크노프레스)
권호 표지
DOI QR코드

DOI QR Code

Axial buckling response of fiber metal laminate circular cylindrical shells

  • Bidgoli, Ali M. Moniri (Faculty of Mechanical Engineering, College of Engineering, University of Tehran) ;
  • Heidari-Rarani, Mohammad (Department of Mechanical Engineering, Faculty of Engineering, University of Isfahan)
  • Received : 2014.09.22
  • Accepted : 2015.12.02
  • Published : 2016.01.10
⟨ Previous Next ⟩

Abstract

Fiber metal laminates (FMLs) represent a high-performance family of hybrid materials which consist of thin metal sheets bonded together with alternating unidirectional fiber layers. In this study, the buckling behavior of a FML circular cylindrical shell under axial compression is investigated via both analytical and finite element approaches. The governing equations are derived based on the first-order shear deformation theory and solved by the Navier solution method. Also, the buckling load of a FML cylindrical shell is calculated using linear eigenvalue analysis in commercial finite element software, ABAQUS. Due to lack of experimental and analytical data for buckling behavior of FML cylindrical shells in the literature, the proposed model is simplified to the full-composite and full-metal cylindrical shells and buckling loads are compared with the available results. Afterwards, the effects of FML parameters such as metal volume fraction (MVF), composite fiber orientation, stacking sequence of layers and geometric parameters are studied on the buckling loads. Results show that the FML layup has the significant effect on the buckling loads of FML cylindrical shells in comparison to the full-composite and full-metal shells. Results of this paper hopefully provide a useful guideline for engineers to design an efficient and economical structure.

Keywords

References

  1. Botelho, E.C., Silva, R.A., Pardini, L.C. and Rezende, M.C. (2006), "A review on the development and properties of continuous fiber/epoxy/aluminum hybrid composites for aircraft structures", Mater Res., 9, 247-256. https://doi.org/10.1590/S1516-14392006000300002
  2. Carrillo, J.G. and Cantwell, W.J. (2007), "Scaling effects in the tensile behavior of fiber-metal laminates", Compos. Sci. Technol., 67, 1684-1693. https://doi.org/10.1016/j.compscitech.2006.06.018
  3. Fan, H.G., Chen, Z.P., Feng, W.Z., Zhou, F., Shen, X.L., Cao, G.W. (2015), "Buckling of axial compressed cylindrical shells with stepwise variable thickness", Struct. Enging. Mech., 54(1), 87-103. https://doi.org/10.12989/sem.2015.54.1.087
  4. Heidari-Rarani, M., Khalkhali-Sharifi, S.S., Shokrieh, M.M. (2014), "Effect of ply stacking sequence on buckling behavior of E-glass/epoxy laminated composites", Comput. Mater. Sci., 89, 89-96. https://doi.org/10.1016/j.commatsci.2014.03.017
  5. Hosseini Hashemi, S.H., Atashipour, S.R., Fadaee, M. and Girhammar, U.A. (2012), "An exact closed form procedure for free vibration analysis of laminated spherical shell panels based on Sanders theory", Arch. Appl. Mech., 82, 985-1002. https://doi.org/10.1007/s00419-011-0606-0
  6. Kardomateas, G.A. (1996), "Benchmark three dimensional elasticity solutions for the buckling of thick orthotropic cylindrical shells", Compos. Part B, 27, 569-580. https://doi.org/10.1016/1359-8368(95)00011-9
  7. Khalili, S.M.R., Malekzadeh, K., Davar, A. and Mahajan, P. (2010), "Dynamic response of pre-stressed fibre metal laminate (FML) circular cylindrical shells subjected to lateral pressure pulse loads", Compos. Struct., 92, 1308-1317. https://doi.org/10.1016/j.compstruct.2009.11.012
  8. Khdeir, A.A., Reddy, J.N. and Frederick, D.A. (1989), "study of bending, vibration and buckling of cross-ply circular cylindrical shells with various shell theories", Int. J. Eng. Sci., 27, 1337-1351. https://doi.org/10.1016/0020-7225(89)90058-X
  9. Krishnakumar, S. (1994), "Fiber metal laminates-the synthesis of metals and composites", Mater Manuf. Pr., 9, 295-354. https://doi.org/10.1080/10426919408934905
  10. Li, X. and Chen, Y. (2002), "Transient dynamic response analysis of orthotropic circular cylindrical shell under external hydrostatic pressure", J. Sound Vib., 257, 967-976. https://doi.org/10.1006/jsvi.2002.5259
  11. Mandal, P. and Calladine, C.R. (2000), "Buckling of thin cylindrical shells under axial compression", Int. J. Solid. Struct., 37, 4509-4525. https://doi.org/10.1016/S0020-7683(99)00160-2
  12. Nam, H.W., Jung, S.W., Jung, C.K. and Han, K.S. (2003), "A model of damage initiation in singly oriented ply fiber metal laminate under concentrated loads", J. Compos. Mater, 37, 269-281. https://doi.org/10.1177/0021998303037003497
  13. Payeganeh, G.H., Ghasemi, F.A. and Malekzadeh, K. (2010), "Dynamic responseof fiber metal laminates (FMLs) subjected to low-velocity impact", Thin Wall Struct., 48, 62-70. https://doi.org/10.1016/j.tws.2009.07.005
  14. Reddy, J.N. (2003), Mechanics of laminated composite plates and shells: theory and analysis, CRC Press, New York.
  15. Sadd, M.H., (2009), Elasticity Theory, Applications and Numerics, Elsevier Inc, USA.
  16. Shen Shen, H. and Xiang, Y. (2008), "Buckling and post buckling of anisotropic laminated cylindrical shells under combined axial compression and torsion", Compos. Struct., 84, 375-386. https://doi.org/10.1016/j.compstruct.2007.10.002
  17. Shi, G. and Xiong, Y. (2000), "Probabilistic buckling analysis of fiber metal laminates under shear loading condition", Adv. Eng. Softw., 31, 519-527. https://doi.org/10.1016/S0965-9978(00)00013-2
  18. Silvestre, N. (2008), "Buckling behaviour of elliptical cylindrical shells and tubes under compression", Int. J. Solid. Struct., 45, 4427-4447. https://doi.org/10.1016/j.ijsolstr.2008.03.019
  19. Sinmazcelik, T., Avcu, E., Ozgur Bora, M. and Coban, O. (2011), "A review: Fibre metal laminates, background, bonding types and applied test methods", Mater. Des., 32, 3671-3685. https://doi.org/10.1016/j.matdes.2011.03.011
  20. Tahir, Z.R. and Mandal, P. (2012), "A new perturbation technique in numerical study on buckling of composite shells under axial compression", World Acad. Sci. Eng. Technol., 70, 10-27.
  21. Topal, U. and Uzman, V. (2009), "Thermal buckling load optimization of angle-ply laminated cylindrical shells", Mater. Des., 30, 532-536. https://doi.org/10.1016/j.matdes.2008.05.052
  22. Tvergaard, V. and Needleman, A. (2000), "Buckling localization in a cylindrical panel under axial compression", Int. J. Solid. Struct., 37, 6825-6842. https://doi.org/10.1016/S0020-7683(99)00316-9
  23. Ugural, A.C. (1981), Stresses in plate and shells, McGraw-Hill, USA.
  24. Ungbhakorn, V. and Singhatanadgid, P. (2003), "Similitude and physical modeling for buckling and vibration of symmetric cross-ply laminated circular cylindrical shells", J. Compos. Mater., 37, 1697-1712. https://doi.org/10.1177/002199803035191
  25. Vinson, J.R. (1993), The mechanical behaviour of shells composed of isotropic and composite materials, Kluwer academic publishers, Dordrecht (Boston, London).
  26. Vlot, A., Alderliesten, R., Hooijmeijer, P., de Kanter, J., Sinke, J. and Ypma, M. (2002), "Fibre metal laminates: a state of the art", Int. J. Mater. Prod. Technol., 17, 79-98. https://doi.org/10.1504/IJMPT.2002.001301
  27. Vlot, A. and Gunnink, J.W. (2001), Fibre metal laminates-an introduction, Kluwer Academic Publishers, Dordrecht, Boston, London.

Cited by

  1. Stress and free vibration analysis of piezoelectric hollow circular FG-SWBNNTs reinforced nanocomposite plate based on modified couple stress theory subjected to thermo-mechanical loadings 2017, https://doi.org/10.1177/1077546317706887
  2. Free vibration analysis of micro and nano fiber-metal laminates circular cylindrical shells based on modified couple stress theory pp.1537-6532, 2020, https://doi.org/10.1080/15376494.2018.1472337
  3. Buckling behavior of composite cylindrical shells with cutout considering geometric imperfection vol.30, pp.4, 2019, https://doi.org/10.12989/scs.2019.30.4.305