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Mechanics of Composite Materials

Erschienen in:

20.07.2021

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

verfasst von: Y. D. Li, H. B. Luo, Y. Yan, J. X. Ye, F. L. Guo

Erschienen in: Mechanics of Composite Materials | Ausgabe 3/2021

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Abstract

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

Vorheriger Artikel Modeling the Curing Kinetics of an Epoxy Binder with Disturbed Stoichiometry for a Composite Material of Aerospace Purpose

Nächster Artikel Effect of Mixing Conditions and Montmorillonite Content on the Mechanical Properties of a Chloroprene Rubber

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Titel: Experimental and Finite-Element Analysis of Metal-Inserted Filament-Wound Composite Tubes
verfasst von: Y. D. Li
H. B. Luo
Y. Yan
J. X. Ye
F. L. Guo
Publikationsdatum: 20.07.2021
Verlag: Springer US
Erschienen in: Mechanics of Composite Materials / Ausgabe 3/2021
Print ISSN: 0191-5665
Elektronische ISSN: 1573-8922
DOI: https://doi.org/10.1007/s11029-021-09961-2

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