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Iterative-Analytical Model of Nonlinear Deformation and Fracture of Multilayer Composite Panels

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Safety in Aviation and Space Technologies

Part of the book series: Lecture Notes in Mechanical Engineering ((LNME))

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Abstract

This work is devoted to the issues of numerical modeling of the processes of occurrence and propagation of cracks and delamination zones in spatial multilayer systems. To simulate the processes of delamination and destruction of composite structures, an iterative-analytical theory is used. A special eight-node isoparametric multilayer finite element has been developed and numerically implemented. Nonlinear problems are solved on the basis of the developed universal algorithm, which includes an iterative-analytical method of variable approximations. Comparison of the results of numerical solutions of test problems with analytical solutions of the data indicates their good agreement. Numerical modeling of the process of propagation of main cracks and delamination zones of a nine-layer metal-composite plate with a central hole has been performed. The developed methods make it possible to reliably estimate the change in the stress–strain state of multilayer structures depending on the accumulation of damage during their operation and can be used in the development of information support systems for the life cycle of multilayer aircraft panels.

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Authors and Affiliations

  1. National Technical University of Ukraine “Igor Sikorsky Kyiv Polytechnic Institute”, Prospect Peremohy 37, Kyiv, 03056, Ukraine

    Aleksandr Gondlyakh, Andrey Chemeris, Aleksandr Kolosov, Aleksandr Sokolskiy & Valeriy Scherbina

  2. Institute of Particle Process Engineering, Technical University of Kaiserslautern, 67653, Kaiserslautern, Germany

    Sergiy Antonyuk

Authors
  1. Aleksandr Gondlyakh
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  2. Andrey Chemeris
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  3. Aleksandr Kolosov
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  4. Aleksandr Sokolskiy
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  5. Valeriy Scherbina
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  6. Sergiy Antonyuk
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Editor information

Editors and Affiliations

  1. North Minzu University, Yinchuan, China

    Andrii Bieliatynskyi

  2. Peter the Great St.Petersburg Polytechnic University, St. Petersburg, Russia

    Vera Breskich

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Gondlyakh, A., Chemeris, A., Kolosov, A., Sokolskiy, A., Scherbina, V., Antonyuk, S. (2022). Iterative-Analytical Model of Nonlinear Deformation and Fracture of Multilayer Composite Panels. In: Bieliatynskyi, A., Breskich, V. (eds) Safety in Aviation and Space Technologies. Lecture Notes in Mechanical Engineering. Springer, Cham. https://doi.org/10.1007/978-3-030-85057-9_4

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  • DOI: https://doi.org/10.1007/978-3-030-85057-9_4

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  • Publisher Name: Springer, Cham

  • Print ISBN: 978-3-030-85056-2

  • Online ISBN: 978-3-030-85057-9

  • eBook Packages: EngineeringEngineering (R0)

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