Free Oscillations of a Composite Structurally Orthotropic Cylindrical Shell Stiffened by Discretely Positioned Ring Ribs


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Resumo

A method for calculating the natural oscillations of a cylindrical shell of an orthotropic material is proposed. The shell is stiffened by a set of sufficiently densely positioned transverse-longitudinal ribs, the arrangement of which allows “smearing” and contains sparsely positioned discrete stiffening rings. The shell may have a closed or open cross section; it is considered to be loaded by external pressure and axial forces. The problem is reduced to a set of homogeneous algebraic equations the number of which is equal to twice the number of discrete ribs; the equation was obtained in explicit form. The comparison of the calculated and experimental data is provided.

Sobre autores

Yu. Solomonov

AO Moscow Institute of Thermal Technology

Email: alexbagd@yandex.ru
Rússia, Moscow, 127273

A. Bagdasar’yan

AO Moscow Institute of Thermal Technology

Autor responsável pela correspondência
Email: alexbagd@yandex.ru
Rússia, Moscow, 127273

V. Georgievskii

AO Moscow Institute of Thermal Technology

Email: alexbagd@yandex.ru
Rússia, Moscow, 127273

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