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Free Vibrational Characteristics of Sandwich Cylindrical Shells Containing a Zero Poisson's Ratio Cellular Core

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Abstract

Purpose

Cellular configurations with ZPR more suitable for cylindrical sandwich shell in which the structure needs undergo pure cylindrical bending. To date, research in the vibration response of cylindrical sandwich shell is still a challenging task. This article proposes one method for free vibration analysis of sandwich cylindrical shells consisting of elastic-isotropic skin and a zero Poisson's ratio cellular core was proposed.

Method

The free vibration characteristics of the sandwich cylindrical shells has been studied using classical thin shell theory. Theoretical models of the effective mechanical performances of the cellular core are established by homogenization methods. The accuracies of theoretical predictions are validated by the finite element method and comparing with others from some available literatures.

Results and Conclusions

Based on the theoretical predictions, the influences on effective mechanical performances of the cellular core and natural frequencies of the sandwich cylindrical shell caused by geometric parameters are evaluated in detail. These geometrical parameters provide different contributions to the effective mechanical properties and dynamic response, which can lead to separate designs for improving their dynamic characteristics.

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Data availability

The datasets generated during and/or analysed during the current study are available from the corresponding author on reasonable request.

References

  1. Ren F, Liu H (2022) Strain induced low frequency broad bandgap tuning of the multiple re-entrant star shaped honeycomb with negative poisson’s ratio. J Vib Eng Technol. https://doi.org/10.1007/s42417-022-00547-3

    Article  Google Scholar 

  2. Zhang J, Dong B, Zhang W (2021) Dynamic crushing of gradient auxetic honeycombs. J Vib Eng Technol 9:421–431. https://doi.org/10.1007/s42417-020-00236-z

    Article  Google Scholar 

  3. Chang LL, Shen X, Dai YK, Wang TX, Zhang L (2020) Investigation on the mechanical properties of topologically optimized cellular structures for sandwiched morphing skins. Compos Str 250:112555. https://doi.org/10.1016/j.compstruct.2020.112555

    Article  Google Scholar 

  4. Vaishali KS, Kumar RR, Dey S (2022) Sensitivity analysis of random frequency responses of hybrid multi-functionally graded sandwich shells. J Vib Eng Technol. https://doi.org/10.1007/s42417-022-00612-x

    Article  Google Scholar 

  5. Khaire N, Tiwari G, Rathod S, Iqbal MA, Topa A (2022) Perforation and energy dissipation behaviour of honeycomb core cylindrical sandwich shell subjected to conical shape projectile at high velocity impact. Thin-Walled Str 171:108724. https://doi.org/10.1016/j.tws.2021.108724

    Article  Google Scholar 

  6. Song L, Yin Z, Wang T, Shen X, Wu J, Su M, Wang HJ (2021) Nonlinear mechanics of a thin-walled honeycomb with zero Poisson’s ratio. Mech Based Des Str Mech. https://doi.org/10.1080/15397734.2021.1987262

    Article  Google Scholar 

  7. Qiu C, Guan Z, Jiang S, Li Z (2017) A method of determining effect elastic properties of honeycomb cores based on equal strain energy. Chin J Aeronaut 30:766–799. https://doi.org/10.1016/j.cja.2017.02.016

    Article  Google Scholar 

  8. Dai G, Zhang W (2009) Cell size effect analysis of the effective Young’s modulus of sandwich core. Comput Mater Sci 46:744–748. https://doi.org/10.1016/j.commatsci.2009.04.033

    Article  Google Scholar 

  9. Yazdanparast R, Rafiee R (2022) Developing a homogenization approach for estimation of in-plan effective elastic moduli of hexagonal honeycombs. Eng Anal Bound Elem 117:202–211. https://doi.org/10.1016/j.enganabound.2020.04.012

    Article  MathSciNet  Google Scholar 

  10. Gonella S, Ruzzene M (2008) Homogenization and equivalent in-plane properties of two-dimensional periodic lattices. Int J Solids Str 45:1897–1915. https://doi.org/10.1016/j.ijsolstr.2008.01.002

    Article  Google Scholar 

  11. Gibson LJ, Ashby MF, Schajer GS, Robertson CI (1982) The mechanics of two-dimensional cellular materials. Proc R Soc Lond A 382:25–42. https://doi.org/10.1098/rspa.1982.0087

    Article  ADS  Google Scholar 

  12. Olympio KR, Gandhi F (2010) Zero Poisson’s ratio cellular honeycombs for flex skins undergoing one-dimensional morphing. J Intell Mater Syst Str 21:1737–1753. https://doi.org/10.1177/1045389X09355664

    Article  Google Scholar 

  13. Yu XL, Zhou J, Liang HY, Jiang ZY (2018) Wu L L (2018) Mechaincal metamaterials associated with stiffness, rigidity and compressibility: A brief review. Prog Mater Sci 94:114–173. https://doi.org/10.1016/j.pmatsci.2017.12.003

    Article  Google Scholar 

  14. Zhong R, Ren X, Zhang XY, Luo C, Zhang Y, Xie YM (2022) Mechanical properties of concrete composites with anxetic single and layered honeycomb structures. Constr Build Mater 322:126453. https://doi.org/10.1016/j.conbuildmat.2022.126453

    Article  Google Scholar 

  15. Liu W, Li H, Zhang J, Li H (2018) Elastic properties of a novel cellular structure with trapezoidal beams. Aerosp Sci Technol 75:315–328. https://doi.org/10.1016/j.ast.2018.01.020

    Article  Google Scholar 

  16. Gong X, Huang J, Scarpa F, Liu Y, Leng J (2015) Zero Poisson’s ratio cellular structure for two-dimensional morphing application. Compos Str 134:384–392. https://doi.org/10.1016/j.compstruct.2015.08.048

    Article  Google Scholar 

  17. Feng N, Tie YH, Wang SB, Guo JX, Hu ZG (2022) Mechanical performance of 3D-printing annular honeycomb with tailorable Poisson’s ratio. Mech Adv Mater Str. https://doi.org/10.1080/15376494.2022.2083733

    Article  Google Scholar 

  18. Tornabene F (2016) Gennral higher-order layer-wise theory for free vibrations of doubly-curved laminated composite shells and panels. Mech Adv Mater Str 23:1046–1067. https://doi.org/10.1080/15376494.2015.1121522

    Article  CAS  Google Scholar 

  19. Huang J, Zhang Q, Scarpa F, Liu Y, Leng J (2016) Bending and benchmark of zero Poisson’s ratio cellular structures. Compos Struct 152:729–736. https://doi.org/10.1016/j.compstruct.2016.05.078

    Article  Google Scholar 

  20. Neville RM, Mobti A, Hazra K, Scarpa F, Remillat C, Farrow IR (2014) Transverse stiffness and strength of Kirigami zero-v PEEK honeycombs. Compos Str 114:30–40. https://doi.org/10.1016/j.compstruct.2014.04.001

    Article  Google Scholar 

  21. Reissner E (1945) The effect of transverse shear deformation on the bending of elastic plates. J Appl Mech-Trans ASME 12:68–77. https://doi.org/10.1115/1.4009435

    Article  MathSciNet  Google Scholar 

  22. Reddy JN (1984) A simple Higher-order theory for laminated composite plates. J Appl Mech-Trans ASME 51:745–752. https://doi.org/10.1115/1.3167719

    Article  Google Scholar 

  23. Wang P, Chalal H, Abed-Meraim A (2017) Quadratic prismatic and hexahedral solid-shell elements for geometic nonlinear analysis of laminated composite structures. Compos Str 172:280–296. https://doi.org/10.1016/j.compstruct.2017.03.091

    Article  Google Scholar 

  24. Duc ND, Thang PT (2015) Nonlinear response of inperfect eccentrically stiffened ceramic-metal-ceramic Sigmoid Functionally Graded Material (S-FGM) thin circular cylindrical shells surrounded on elastic foundations under uniform radial load. Mech Adv Mater Str 22:1031–1038. https://doi.org/10.1016/j.compstruct.2013.11.015

    Article  Google Scholar 

  25. Qin ZY, Pang XJ, Safaei B, Chu FL (2019) Free vibration analysis of rotating functionally graded CNT reinforced composite cylindrical shells with arbitray boundary conditions. Compos Str 220:847–860. https://doi.org/10.1016/j/compstruct.2019.04.06

    Article  Google Scholar 

  26. Pang FZ, Li HC, Chen HL, Shan YH (2021) Free vibration analysis of combined composite laminated cylindrical and spherical shells with arbitray boundary conditions. Mech Adv Mater Str 28:182–199. https://doi.org/10.1080/15376494.2018.1553258

    Article  Google Scholar 

  27. Eipakchi H, Nasrekani FM (2020) Vibrational behavior of composite cylindrical shells with auxetic honeycombs core layer subjected to a moving pressure. Compos Struct 254:112847. https://doi.org/10.1016/j.compstruct.2020.112847

    Article  Google Scholar 

  28. Lan L, Sun J, Hong F, Wang D, Zhang Y, Fu M (2020) Nonlinear constitutive relations of thin-walled honeycomb structure. Mech Mater 149:103556. https://doi.org/10.1016/j.mechmat.2020.103556

    Article  Google Scholar 

  29. Gibson LJ, Ashby MF (1997) Cellular solid: structure and properties. Cambridge University Press

    Book  Google Scholar 

  30. Young WC (2002) Cark's formulas for stress and strain. McGraw-Hill Education, New York https://doi.org/10.1115/1.3423917

  31. Becus GA (2019) Homogenization and random evolutions: Applications to the mechanics of composite materials. Q appl Math 37:209–210. https://doi.org/10.1090/qam/548985

    Article  MathSciNet  Google Scholar 

  32. Hamidreza E, Nasrekani FM, Ahmadi S (2020) An analytical approach for vibration behavior of viscoelastic cylindrical shells under internal moving pressure. Acta Mech 231:3405–3418. https://doi.org/10.1007/s00707-020-02719-2

    Article  MathSciNet  Google Scholar 

  33. Sadd MH (2007) Elastic theory, application, and numeric. Academic Press

    Google Scholar 

  34. Pham HC, Pham TL, Nguyen VN, Nguyen DD (2019) Geometrically nonlinear dynamic response of eccentrically stiffened circular cylindrical shells with negativePoisson’s ratio in auxetic honeycombs core layer. Int J Mech Sci 152:443–453. https://doi.org/10.1016/j.ijmecsci.2018.12.052

    Article  Google Scholar 

  35. Rao SS (2007) Vibration of continuous system. New Jersey, USA: John Willey & Sons

  36. Pradhan SC, Loy CT, Lam KY, Reddy JN (2000) Vibration characteristics of functionally graded cylindrical shells under various boundary conditions. Appl Acoust 61:111–129. https://doi.org/10.1016/S0003-682X(99)00063-8

    Article  Google Scholar 

  37. Loy CT, Lam KY (1997) Vibration of cylindrical shells with ring support. Int J Mech Sci 39:455–471. https://doi.org/10.1016/S0020-7403(96)00035-5

    Article  Google Scholar 

  38. Bubert EA, Woods BKS, Lee K, Kothera CS, Wereley NM (2010) Design and fabrication of a passive 1D morphing aircraft skin. J Int Mater Syst Struct 21:1699–1717. https://doi.org/10.1177/1045389X10378777

    Article  Google Scholar 

  39. Farshidianfar A, Farshidianfar MH, Crocker MJ, Smith WO (2011) The vibration analysis of long cylindrical shells using acoustical excitation. J Sound Vibr 330:3381–3399. https://doi.org/10.1016/j.jsv.2011.02.002

    Article  ADS  Google Scholar 

  40. Oliazadeh P, Farshidianfar MH, Farshidianfar A (2013) Exact analysis of resonance frequency and mode shapes of isotropic and laminated composite cylindrical shells; Part I: analytical studies. J Mech Sci Technol 27:3635–3643. https://doi.org/10.1007/s12206-013-0905-1

    Article  Google Scholar 

  41. Flügge W (1973) Stresses in Shells. Second Springer, Berlin

    Book  Google Scholar 

  42. Dinh GN, Nguyen DT, Vu NVH, Dao HB (2020) Vibration of cylindrical shells made of three layers W-Cu composite containing heavy water using Flügge-Lur’e-Bryrne theory. Thin-Walled Struct 146:106414. https://doi.org/10.1016/j.tws.2019.106414

    Article  Google Scholar 

  43. Singal RK, Williams K (1988) A theoretical and experimental study of vibrations of thick circular cylindrical shells and rings. J Vib Acoust 110:533–537. https://doi.org/10.1115/1.3269562

    Article  Google Scholar 

  44. Blevins RD (1987) Formulas for natural frequency and mode shape. Robert E. Krieger Publishing Co., FL

    Google Scholar 

  45. Li Y, Yao W, Wang T (2020) Free flexural vibration of thin-walled honeycomb sandwich cylindrical shells. Thin-walled Struct 157:107032. https://doi.org/10.1016/j.tws.2020.107032

    Article  Google Scholar 

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Acknowledgements

This work was supported by the National Natural Science Foundation of China under Grant No. 12111540251, the National Natural Science Foundation of China under Grant No. 11872207, Aeronautical Science Foundation of China under Grant No. 20180952007, Foundation of National Key Laboratory on Ship Vibration and Noise under Grant No. 614220400307, and the National Key Research and Development Program of China under Grant NO. 2019YFA708904.

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Correspondence to Zhiyong Yin.

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The authors declare that they have no known competing financial interests or personal relationships that could have appeared to influence the work reported in this paper. All data included in this study are available upon request by contact with the corresponding author.

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Song, L., Wang, T., Yin, Z. et al. Free Vibrational Characteristics of Sandwich Cylindrical Shells Containing a Zero Poisson's Ratio Cellular Core. J. Vib. Eng. Technol. 12, 1603–1620 (2024). https://doi.org/10.1007/s42417-023-00928-2

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