Description
A quarter ring has a radius of 5" , a width of 1", and a thickness of 0.1". The quarter ring is supported symmetrically. Find the buckling load applied radially as shown.

File Name
Browse to drive
letter:\Users\Public\Public Documents\SOLIDWORKS\SOLIDWORKS
version\samples\Simulation
Examples\Verification\Buckling_2.SLDPRT and open the
file.
Shell Parameters
Shell thickness = 0.1" - Thin formulation.
Material Properties
Modulus of elasticity = 1 X 107 psi.
Results
|
|
Buckling Load (per arc length)
(lbs/in) |
Theory
|
26.66 |
SOLIDWORKS Simulation (Shell mesh)
|
High
|
26.66 |
Draft
|
26.67 |
The theoretical value is calculated from Donnell approximation as: P
cr = 4EI / R
3 = 26.66 lb/in, where:
- Pcr = Critical (buckling) force
- E = Modulus of elasticity
- I = Moment of inertia of the cross section of the shell
- R = Radius
The critical load from SOLIDWORKS Simulation
is calculated as:
Pcr = (Applied force)*(Buckling load factor)
Reference
Brush, D. O., and Almroth, B. O., "Buckling of Bars, Plates, and Shells," McGraw-Hill Inc., New York, 1975, p. 139.