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Certificate of Registration Media number Эл #ФС77-53688 of 17 April 2013. ISSN 2308-6033. DOI 10.18698/2308-6033
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Impact Interaction of a Detached Aircraft Engine Bladewith a Multilayer Panel Made of Polymer Composite

Published: 02.06.2026

Authors: Vestyak V.A., Martirosov M.I., Zanina E.A.

Published in issue: #6(174)/2026

DOI:

Category: Mechanics | Chapter: Mechanics of Deformable Solid Body

    explicit method, Smoothed Particle Hydrodynamics (SPH), polymer composite materials, finite element method (FEM), impact, discrete sources, aircraft engineering, aircraft engine blade, stringer panel, LS-DYNA software package
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