LARGE AMPLITUDE VIBRATIONS OF CIRCULAR CYLINDRICAL SHELLS
β Scribed by M. Ganapathi; T.K. Varadan
- Publisher
- Elsevier Science
- Year
- 1996
- Tongue
- English
- Weight
- 450 KB
- Volume
- 192
- Category
- Article
- ISSN
- 0022-460X
No coin nor oath required. For personal study only.
β¦ Synopsis
By using a C0 continuous, QUAD-4 shear flexible shell element, based on the field consistency principle, the non-linear free flexural vibrations of thin circular cylindrical shells have been studied. The formulation is general in the sense that it includes anisotropy, transverse shear deformation, in-plane and rotary inertia effects. Primarily, an attempt is made to clarify the existing controversies in the prediction of the non-linear behaviour of isotropic circular cylindrical shells through a finite element formulation with dynamic response analysis. The non-linear governing equations are solved by using a Wilson-u numerical integration scheme with u = 1β’4. For each time step, modified Newton-Raphson iterations are employed to achieve equilibrium at the end of that time step. Detailed numerical results are presented for various parameters for the isotropic shell. The present study also brings out the participation of the axisymmetric contraction mode with the asymmetric mode.
π SIMILAR VOLUMES
The non-linear response of empty and #uid-"lled circular cylindrical shells to harmonic excitations is investigated. Both modal and point excitations have been considered. The model is suitable to study simply supported shells with and without axial constraints. Donnell's non-linear shallow-shell th
The e!ects of large vibration amplitudes on the "rst and second coupled radial-circumferential mode shapes of isotropic circular cylindrical shells of in"nite length are examined. A theoretical model based on Hamilton's principle and spectral analysis developed previously for clamped}clamped beams a
A shallow shell theory is presented for the geometrically non-linear analysis of moderately thick isotropic spherical shells. Effects of transverse shear deformation and rotatory inertia are included in the governing equations of motion by means of tracing constants. When these effects are ignored,