112 On Various Boundary Conditions to Control the Progressive Buckling Modes of Cylindrical Shells

2000 ◽  
Vol 2000.6 (0) ◽  
pp. 23-24
Author(s):  
Noriaki OKAMOTO ◽  
Noritaka HORIE
1975 ◽  
Vol 97 (1) ◽  
pp. 175-181 ◽  
Author(s):  
J. R. Vinson

Methods of analysis are presented for very thick-walled cylindrical, isotropic shells subjected to axially symmetric lateral and in-plane loads. These methods are developed for shells with ratios of wall thickness to mean radius as large as 0.5, as well as being applicable for thin classical shells which involve Love’s First Approximation. The present methods are elasticity solutions and employ no shell theory assumptions. Explicit solutions are presented for the shell subject to in-plane loads and laterally distributed loads which are constant or varying linearly axially for various boundary conditions at the ends.


2014 ◽  
Vol 04 (11) ◽  
pp. 315-331 ◽  
Author(s):  
Muhammad Nawaz Naeem ◽  
Awais Gul Khan ◽  
Shahid Hussain Arshad ◽  
Abdul Ghafar Shah ◽  
Madiha Gamkhar

Author(s):  
A. Grigorenko ◽  
M. Borysenko ◽  
O. Boychuk

The natural frequencies and the corresponding vibration modes of open cylindrical shells with an elliptical cross-section and variable thickness are analyzed. Various opening angle of the shell along both the minor and major axes are allowed and various boundary conditions are considered. The numerical solutions are obtained using the finite element package FEMAP with the NASTRAN solver. A number of lowfrequency vibrations are investigated in terms of their dependence on the opening angle along major and minor axes of the shell. The vibration forms for the first ten frequencies with different boundary conditions at the same opening angles are shown.


Sign in / Sign up

Export Citation Format

Share Document