OS-V: 1205 Twisted Cantilever Beam (Explicit Results)
MacNeal-Harder TestA twisted cantilever beam solved with solid and shell elements using Explicit Analysis. A twisted beam model is made with each element type to investigate the effect of distorted elements with a high aspect ratio.
Model Files
Before you begin, copy the file(s) used in this problem
to your working directory.
Benchmark Model
As shown in Figure 1, the beam is constrained in x, y and z directions for translational motion. The end of the beam has Force Load applied. Four types of elements are used for this problem. In-plane bending is used for all the elements.
Analytical result computed by beam theory for deflection is Uy = 1.754E-04.
- Material Properties
- Value
- Young's modulus
- 29E+06 psi
- Poisson's ratio
- 0.22
- Density
- 1E-04 lbm/in3
Results
Explicit Analysis results are shown in comparison with the reference result.
Element Type | Analytical Result | OptiStruct Explicit Analysis Results | |
---|---|---|---|
Absolute Value | Normalized Value | ||
CQUAD4 | 1.754E-03 | 1.895E-03 | 1.0804 |
CTRIA3 | 1.802E-03 | 1.0274 | |
CHEXA8 | 1.793E-03 | 1.022 | |
CTETRA10 | 1.790E-03 | 1.020 |
Reference
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.