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A unified and exact solution method is developed for the free vibration analysis of composite laminated cylindrical shells with general elastically restrained boundaries and arbitrary lamination schemes.
When simple structures, such as beams, with longitudinally restrained boundaries vibrate with a large displacement amplitude in flexure, an in-plane strain is induced.
In this paper, an accurate solution is developed for the vibration and damping characteristics of a three-layered passive constrained layer damping (PCLD) cylindrical shell with general elastically restrained boundaries.
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Finally, the influence of the elastically restrained boundary conditions on the natural frequencies is investigated.
This work presents a method to find accurate vibration frequencies of beams with generally restrained boundary conditions using Fourier series.
The relation between problems with elastically restrained boundary conditions and those with tip-mass boundary conditions is explored.
In this investigation, the in-plane vibration problems are solved for plates with general elastically restrained boundary conditions.
The influence of the tangency coefficient and the elastically restrained boundary conditions on the elastic instability of an uniform Bernoulli-Euler beam is investigated.
In this study, the frequency equations for calculating the natural frequencies of the beams with generally restrained boundary conditions by both translational and rotational springs are derived in the matrix form using Fourier sine series.
In this paper a systematic development of the solution theory for the non-uniform Bernoulli-Euler beam vibration, including both forced and free vibrations, with general elastically restrained boundary conditions, is presented.
The influences of the tangency coefficient, the slenderness ratio and the elastically restrained boundary conditions on the elastic instability and the critical load of a Timoshenko beam are investigated.
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CEO of Professional Science Editing for Scientists @ prosciediting.com