
Length = 6.0; Height = 0.2; Depth = 0.1; E = 1.0E7: Poisson's ratio = 0.3.
This is a straight cantilever beam solved with solid and shell elements. Three models (rectangular, parallelogram, trapezoidal) are made with each element's type to investigate the effect of distorted elements with a high aspect ratio.
Six types of elements are used for this problem. They are tria-shell, quad-shell, and hexa-solid elements, each with 1st and 2nd order. Four loading cases are used for each model; extension, in-plane bending, transverse bending, and twist. For the extension and bending load cases, unit loads are applied in a consistent fashion over all of the nodes at the tip of the beam. For the twist load cases, a unit moment is applied at the tip.
Theoretical solutions for the deflections at the tip, computed by beam theory, are as follows.
|
Load Type |
Component |
Value |
|
extension |
UX |
0.00003 |
|
in-plane bending |
UZ |
0.1081 |
|
transverse bending |
UY |
0.4321 |
|
twist |
ROTX |
0.03208 |
All results are normalized with the target value.
MacNeal, R.H., and Harder, R.L., A Proposed Standard Set of Problems to Test Finite Element Accuracy, Finite Elements in Analysis and Design, 1 (1985) 3-20.