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Experimental and Finite-Element Analysis of Metal-Inserted Filament-Wound Composite Tubes

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Mechanics of Composite Materials Aims and scope

To meet the aviation and aerospace requirements for detachability and load-carrying capacity, a novel connecting structure — a carbon-fiber-filament-wound composite tube with grooved metal inserts has been developed. The tensile behavior of the structure was investigated experimentally and by the finite-element method. The finite-element method was used to simulate the damage process. The failure load of the structure was found to be 37% higher than that of an ordinary bonded tube without grooved metal inserts. A stress analysis showed that the structural failure was not caused by the failure of adhesive, but was determined by the tensile strength of the ±30° wound layers and the shear strength of interlayer

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Authors and Affiliations

  1. School of Aeronautic Science and Engineering, Beihang University, Beijing, 100191, China

    Y. D. Li, Y. Yan & J. X. Ye

  2. Aerospace Information Research Institute, Chinese Academy of Sciences, Beijing, 100094, China

    H. B. Luo

  3. Shenyuan Honors College, Beihang University, Beijing, 100191, China

    J. X. Ye

  4. College of Aerospace Engineering, Chongqing University, Chongqing, 400044, China

    F. L. Guo

Authors
  1. Y. D. Li
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  2. H. B. Luo
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  3. Y. Yan
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  4. J. X. Ye
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  5. F. L. Guo
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Correspondence to H. B. Luo.

Additional information

Russian translation published in Mekhanika Kompozitnykh Materialov, Vol. 57, No. 3, pp. 535-552, May-June, 2021.

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Li, Y.D., Luo, H.B., Yan, Y. et al. Experimental and Finite-Element Analysis of Metal-Inserted Filament-Wound Composite Tubes. Mech Compos Mater 57, 373–386 (2021). https://doi.org/10.1007/s11029-021-09961-2

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  • DOI: https://doi.org/10.1007/s11029-021-09961-2

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