Objective
To verify the behavior of beam element vibration
Problem Description
A right-angle frame [Ref 1] vibrates under its own weight as shown below.
Material properties: E = 2e11 Pa, ν = 0.29, ρ = 7860 Kg/m3
Section properties: square section 100 x 100 mm
Finite Element Model
50 beam elements
Model type: 2D Frame (shear deformation considered)
Results
The mode frequencies are given by [Ref 1]
Unit: mode frequency - Hz
Mode Frequency |
ENERCALC 3D |
[Ref 1] |
Mode 1 |
3.331 |
3.315 |
Mode 2 |
35.07 |
35.08 |
Mode 3 |
70.60 |
70.77 |
Mode 4 |
122.6 |
122.7 |
Mode 5 |
225.7 |
226.0 |
Mode 6 |
269.0 |
269.4 |
Mode 7 |
395.7 |
396.6 |
Mode 8 |
420.7 |
420.8 |
Mode 9 |
552.2 |
552.3 |
Mode 10 |
650.1 |
649.6 |
First Four Mode Shapes:
Mode Shape 1 |
Mode Shape 2 |
Mode Shape 3 |
Mode Shape 4 |
Comments
The vibration frequencies given by ENERCALC 3D are very close to the referenced values.
Reference
[1]. Cook, Malkus, Plesha, Witt, “Concept and Applications of Finite Element Analysis” 4th Edition, pp436, John Wiley & Sons, Inc., 2002