β Scribed by Yu. S. Vorob'ev; S. I. Detistov
No coin nor oath required. For personal study only.
π SIMILAR VOLUMES
Free vibrations of thick rotating cross-ply laminated composite cylindrical shells are studied based on the "rst order shear deformation shell theory (FSDT). The governing equations of "ve degrees of freedom with consideration of Coriolis accelerations and rotary inertias are established. Analytical
The general equations of the vibrations of high speed rotating shells of revolution, with consideration of Coriolis accelerations and large deformations, are established by the method of linear approximation. In the general case, there are great difficulties in obtaining analytical solutions of the
The problems of the vibration of rotating cylindrical shells are solved by using nine-node super-parametric "nite element with shear and axial deformation and rotatory inertial. The non-linear plate-shell theory for large de#ection is used to handle the cylindrical shell before it reaches equilibriu