Description
A cylindrical shell of thickness 3" is covered at both ends with rigid diaphragms to allow displacement only along its axial direction. At the cylinder mid-span, a load of 1 lb is applied as shown in the figure below. Determine the radial deflection at the point where the load is applied. The radius and length of the cylinder are 300" and 600" respectively.

File Name
Browse to drive
letter:\Users\Public\Public Documents\SOLIDWORKS\SOLIDWORKS
version\samples\Simulation
Examples\Verification\Static_11.SLDPRT and open the
file.
Shell Parameters
Shell thickness = 3" - Thin formulation.
Meshing Parameters
Use a Global Size of 25 in.
Material Properties
Modulus of elasticity = 3 X 106 psi, Poisson's ratio = 0.3.
Modeling Hints
Due to symmetry, only one-eighth of the cylinder is modeled. To simulate the rigid diaphragm, translations in the radial and circumferential directions and rotations about the axial direction are all set to zero.
Results
|
Theory |
SOLIDWORKS Simulation |
Radial deflection (UX), in |
1.8248e-5 |
1.852e-5 |
Reference
Dvorkin, E. N., and Bathe, K. J., “A Continuum Mechanics Based Four Node Shell Element for General Nonlinear Analysis,” Engineering Computations, 1, 77-78, 1984.