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Study on bi-stable behaviors of un-stressed thin cylindrical shells based on the extremal principle

  • Wu, Yaopeng (School of Civil Engineering, Xi'an University of Architecture and Technology) ;
  • Lu, Erle (School of Civil Engineering, Xi'an University of Architecture and Technology) ;
  • Zhang, Shuai (School of Civil Engineering, Xi'an University of Architecture and Technology)
  • Received : 2017.08.15
  • Accepted : 2018.09.26
  • Published : 2018.11.10

Abstract

Bi-stable structure can be stable in both its extended and coiled forms. For the un-stressed thin cylindrical shell, the strain energy expressions are deduced by using a theoretical model in terms of only two parameters. Based on the principle of minimum potential energy, the bi-stable behaviors of the cylindrical shells are investigated. The results indicate that the isotropic cylindrical shell does not have the second stable configuration and laminated cylindrical shells with symmetric or antisymmetric layup of fibers have the second stable state under some confined conditions. In the case of antisymmetric laminated cylindrical shell, the analytical expressions of the stability are derived based on the extremal principle, and the shell can achieve a compact coiled configuration without twist deformation in its second stable state. In the case of symmetric laminated cylindrical shell, the explicit solutions for the stability conditions cannot be deduced. Numerical results show that stable configuration of symmetric shell is difficult to achieve and symmetric shell has twist deformation in its second stable form. In addition, the roll-up radii of the antisymmetric laminated cylindrical shells are calculated using the finite element package ABAQUS. The results show that the value of the roll-up radii is larger from FE simulation than from theoretical analysis. By and large, the predicted roll-up radii of the cylindrical shells using ABAQUS agree well with the theoretical results.

Keywords

Acknowledgement

Supported by : China's National Natural Science Foundation, Shaanxi Province Department of Education, Building Safety and Built Environment, Xi'an University of Architecture and Technology

References

  1. Daynes, S., Potter, K.D. and Weaver, P.M. (2008), "Bistable prestressed buckled laminates", Compos. Sci. Technol., 68(15-16), 3431-3437. https://doi.org/10.1016/j.compscitech.2008.09.036
  2. Li, H., Dai, F., Weaver, P.M. and Du, S. (2014), "Bistable hybrid symmetric laminates", Compos. Struct., 116, 782-792. https://doi.org/10.1016/j.compstruct.2014.05.030
  3. Zhang, Z., Wu, H.L., He, X.Q., Wu, H.P., Bao, Y.M. and Chai, G.Z. (2013), "The bistable behaviors of carbon-fiber/epoxy antisymmetric composite shells", Compos.: Part B, 7, 190-199.
  4. Zhang, Z., Wu, H.P., Ye, G.F., Wu, H.L., He, X.Q. and Chai, G.Z. (2014), "Systematic experimental and numerical study of bistable snap processes for anti-symmetric cylindrical shells" Compos. Struct., 112, 368-377. https://doi.org/10.1016/j.compstruct.2014.02.030
  5. Zhang, Z., Zhang, Z., Wu, H.P., Wu, H.L., Chen, D.D. and Chai, G.Z. (2015), "Thermal effect and active control on bistable behavior of anti-symmetric composite shells with temperaturedependent properties", Compos. Struct., 124, 263-271. https://doi.org/10.1016/j.compstruct.2015.01.024
  6. Galletly, D.A. and Guest, S.D. (2004a), "Bistable composite slit tubes. I. A beam model", Int. J. Sol. Struct., 41(16-17), 4517-4533. https://doi.org/10.1016/j.ijsolstr.2004.02.036
  7. Galletly, D.A. and Guest, S.D. (2004b), "Bi-stable composite slit tubes. II. A shell model", Int. J. Sol. Struct., 41(16-17), 4503-4516. https://doi.org/10.1016/j.ijsolstr.2004.02.037
  8. Kebadze, E., Guest, S.D. and Pellegrino, S. (2004), "Bistable prestressed shell structures", Int. J. Sol. Struct., 41(11-12), 2801-2820. https://doi.org/10.1016/j.ijsolstr.2004.01.028
  9. Guest, S.D. and Pellegrino, S. (2006), "Analytical models for bistable cylindrical shells", Proceedings of the Royal Society A, 462(2067), 839-854.
  10. He, X.Q. (2011), "Bi-stable character of laminated cylindrical shells", Proc. Eng., 14, 616-621. https://doi.org/10.1016/j.proeng.2011.07.077
  11. Kumar, S. (2010), "Analysis of impact response and damage in laminated composite cylindrical shells undergoing large deformations", Struct. Eng. Mech., 35(3), 349-364. https://doi.org/10.12989/sem.2010.35.3.349
  12. Aghajari, S., Showkati, H. and Abedi, K. (2011), "Experimental investigation on the buckling of thin cylindrical shells with twostepwise variable thickness under external pressure", Struct. Eng. Mech., 39(6), 849-860. https://doi.org/10.12989/sem.2011.39.6.849
  13. Guo, Z.X., Han, X.P, Guo, M.Q. and Han, Z.J. (2015), "Buckling analysis of filament wound composite cylindrical shell for considering the filament undulation and crossover", Struct. Eng. Mech., 55(2), 399-411. https://doi.org/10.12989/sem.2015.55.2.399
  14. Javed, S., Viswanathan, K.K. and Aziz, Z.A. (2016), "Free vibration analysis of composite cylindrical shells with nonuniform thickness walls", Steel Compos. Struct., 20(5), 1087-1102. https://doi.org/10.12989/scs.2016.20.5.1087
  15. Dogan, A. and Arslan, H.M. (2012), "Investigation of the effect of shell plan-form dimensions on mode-shapes of the laminated composite cylindrical shallow shells using SDSST and FEM", Steel Compos. Struct., 12(4), 303-324. https://doi.org/10.12989/scs.2012.12.4.303
  16. Ali, M.M.B. and Mohammad, H.R. (2016), "Axial buckling response of fiber metal laminate circular cylindrical shells", Struct. Eng. Mech., 57(1), 45-63. https://doi.org/10.12989/sem.2016.57.1.045
  17. Dogan, A., Arslan, H.M. and Yerli H.R. (2010), "Effects of anisotropy and curvature on free vibration characteristics of laminated composite cylindrical shallow shells", Struct. Eng. Mech., 35(4) 493-510. https://doi.org/10.12989/sem.2010.35.4.493
  18. Patel, S.N., Bisagni, C. and Datta, P.K. (2011), "Dynamic buckling analysis of a composite stiffened cylindrical shell", Struct. Eng. Mech., 37(5), 509-527. https://doi.org/10.12989/sem.2011.37.5.509