Navigation:  Dynamic >

F-01 (Simple 2D Frame Vibration)

Previous pageReturn to chapter overviewNext page

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

 

F-01 (Simple 2D Frame Vibration)1

 

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:

F-01 (Simple 2D Frame Vibration)2

Mode Shape 1

F-01 (Simple 2D Frame Vibration)3

Mode Shape 2

F-01 (Simple 2D Frame Vibration)4

Mode Shape 3

F-01 (Simple 2D Frame Vibration)5

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