Numerical analysis of the behavior of a three-layer honeycomb panel with interlayer defects under action of dynamic load

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Abstract

The aim of the work is to study the effect of interlayer defects of the bundle type on the behavior of a rectangular flat three-layer panel with a honeycomb filler under the influence of a dynamic impact load. Methods. The problem was solved numerically using the finite element method in the Simcenter Femap and LS-DYNA (Livermore Software Technology Corp.) software complexes. For this purpose, a geometric model of a panel with a honeycomb placeholder was developed. Based on the geometric model, a finite element model of the panel was created using three-dimensional finite elements. In the software complexes, the finite element model was calculated under specified boundary conditions, then the stress fields and fracture indices in the panel were determined, taking into account and without taking into account damage. Results. The stress fields in the panel are numerically determined with and without defects. The fields of the failure indices of the panel layers under the impact load are investigated using various failure criteria (Puck, Hashin, LaRC03 (Langley Research Center)) of polymer composite materials. The analysis of the influence of a defect on the behavior of a honeycomb panel under the impact load is carried out.

About the authors

Aleksandr L. Medvedskiy

Central Aerohydrodynamic Institute; Moscow Aviation Institute (National Research University)

Author for correspondence.
Email: mdv66@mail.ru
ORCID iD: 0000-0002-9199-229X

Doctor of Physical and Mathematical Sciences, Docent, First Deputy General Director

1 Zhukovskogo St, bldg 1, Zhukovsky, 140180, Russian Federation; 4 Volokolamskoe Shosse, Moscow, 125993, Russian Federation

Mikhail I. Martirosov

Moscow Aviation Institute (National Research University)

Email: michaelmartirosov@yandex.ru
ORCID iD: 0000-0001-8662-9667

Candidate of Technical Sciences, Docent, Department 902 “Resistance of Materials, Dynamics and Strength of Machines”, Institute No. 9 “General Engineering Training”

4 Volokolamskoe Shosse, Moscow, 125993, Russian Federation

Anton V. Khomchenko

Moscow Aviation Institute (National Research University); Irkut Corporation

Email: khomchenkoanton@yandex.ru
ORCID iD: 0000-0001-6640-011X

postgraduate student, Department 903 “Advanced Materials and Technologies for Aerospace Purposes”, Institute No. 9 “General Engineering Training” ; principal design engineer

4 Volokolamskoe Shosse, Moscow, 125993, Russian Federation; 68 Leningradsky Prospekt, Moscow, 125315, Russian Federation

Darina V. Dedova

Irkut Corporation

Email: darina.dedova98@gmail.com
ORCID iD: 0000-0003-2488-1335

design engineer

68 Leningradsky Prospekt, Moscow, 125315, Russian Federation

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Copyright (c) 2021 Medvedskiy A.L., Martirosov M.I., Khomchenko A.V., Dedova D.V.

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