Work

Stress-strain State Investigation of Adhesive Layer in Sandwich Structure of Flying Vehicle

Year: 2025

Type: dataset

Abstract: The studies of theoretical modeling of sandwich shell (SS) and experimental sandwich beam (SB) are presented in this paper.The displacements of adhesive layers are computed in the whole SS.The Hamilton's principle is used to derive the equations of equilibrium, which contains 6 differential equations with 16 orders.

DOI: 10.54985/peeref.2503a3758320

Authors: Vladimir N. Kobelev, Huang Song-Jeng, Vladimir V. Kobelev

Institution: Moscow State Aviation Technological University

Language: English

Topic: Composite Structure Analysis and Optimization

Subfield: Mechanics of Materials

Field: Engineering

Domain: Physical Sciences

Open Access status: gold

OpenAlex ID: W4408191036

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