STRESS-STRAIN STATE INVESTIGATION OF ADHESIVE LAYER IN SANDWICH STRUCTURE OF FLYING VEHICLE

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.

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Published
2025-03-06
DOI
https://doi.org/10.54985/peeref.2503a3758320
Primary Topic
Mechanical Engineering and Vibrations Research
Type
article
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STRESS-STRAIN STATE INVESTIGATION OF ADHESIVE LAYER IN SANDWICH STRUCTURE OF FLYING VEHICLE

Vladimir Kobelev, Huang Song-Jeng
Mechanical Engineering and Vibrations Research
article

STRESS-STRAIN STATE INVESTIGATION OF ADHESIVE LAYER IN SANDWICH STRUCTURE OF FLYING VEHICLE

Vladimir Kobelev, Huang Song-Jeng
article en

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.

Moscow State Aviation Technological University (RU)
Mechanical Engineering and Vibrations Research
DOIOpen Access PDFOpenAlex
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STRESS-STRAIN STATE INVESTIGATION OF ADHESIVE LAYER IN SANDWICH STRUCTURE OF FLYING VEHICLE — Vladimir Kobelev, Huang Song-Jeng · (2025) | TGRS Research Map | TGRS