Analysis of Free Vibrations of a Skew Orthotropic Composite Panel

The free vibrations and stability of layered skew composite panels symmetrical in thickness are considered. The panel is modeled by a plate that has the shape of a parallelogram in plan view, each edge of which can have an independent way of fastening. The solution of the problem of transverse vibra...

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Published in:Journal of machinery manufacture and reliability 2022-10, Vol.51 (5), p.406-418
Main Authors: Azikov, N. S., Zinin, A. V.
Format: Article
Language:English
Subjects:
Axial loads
Boundary conditions
Composite materials
Engineering
Free vibration
Laminates
Machines
Manufacturing
Multilayers
Panels
Processes
Reliability
Resonant frequencies
Ritz method
Stability
Strength
Transverse oscillation
Wear Resistance of Machines and Structures
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description The free vibrations and stability of layered skew composite panels symmetrical in thickness are considered. The panel is modeled by a plate that has the shape of a parallelogram in plan view, each edge of which can have an independent way of fastening. The solution of the problem of transverse vibrations and stability is carried out in displacements by the Ritz method. The values of the natural frequencies and the critical compression forces of skew layered composite panels with different boundary conditions depending on the geometry of the element, boundary conditions, and levels of the axial load are obtained.
doi_str_mv 10.3103/S105261882205003X
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source Springer Nature
subjects Axial loads
Boundary conditions
Composite materials
Engineering
Free vibration
Laminates
Machines
Manufacturing
Multilayers
Panels
Processes
Reliability
Resonant frequencies
Ritz method
Stability
Strength
Transverse oscillation
Wear Resistance of Machines and Structures
title Analysis of Free Vibrations of a Skew Orthotropic Composite Panel
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