Beam Problem 1 Solution first created 23/03/08 - last modified 23/03/08 Page Author: Ty Harness


The theoretical end deflection of a cantilever can be obtained from tables or derived from the bending moment equation.

$y(L) = (PL^3)/(3*E*I)$

Working in Newtons and mm

We need the second moment of area,I about the neutral axis:

$I = (b*d^3)/12 = 3.333*10^7 mm^4$

$E = 200 000 (MN)/m^2 = 200 000 N/(mm^2)$

$y(L) = (20*10^3*1000^3)/(3*200*10^3*3.333*10^7) = 1 mm$

I've chosen to use Prof. Rieg's Z88 Finite Elements Program because it's free and unlimited and ideal for student use. The theory behind FEM is beyond the scope of this tutorial but you can learn a great deal from the Z88 manual.

Using a Beam Element No. 13 we create a

General Structure Data File, Z88i1.txt which basically consists of : 2D Analysis, 5 Nodes, 4 Elements, 3DOF per node 15 in total.
Nodal co-ordinates, elements defined and adjacent elements. All elements 1 to 4 have the same properties Young's Modulus but this time working in metres = 2e11 N/m^2. Poisson's Ratio = 0.3 from tables, Area = 1e-2 m^2, I = 3.33e-5 m^4
2 5 4 15 1 0 1 0 Z88I1.TXT,produced by Ty
1 3 +0.00000E-000 +0.00000E+000 +0.00000E+000 node #1
2 3 +2.50000E-001 +0.00000E+000 +0.00000E+000 node #2
3 3 +5.00000E-001 +0.00000E+000 +0.00000E+000 node #3
4 3 +7.50000E-001 +0.00000E+000 +0.00000E+000 node #4
5 3 +1.00000E+000 +0.00000E+000 +0.00000E+000 node #5
1 13 element #1
1 2
2 13 element #2
2 3
3 13 element #3
3 4
4 13 element #4
4 5
1 4 +2.00000E+011 +3.00000E-001 1 +1.00000E-002 +0.00000E+000 +0.00000E+000 +3.33333E-005 +1.00000E-001 +0.00000E+000 +0.00000E+000

and the boundary conditions file Z88i2.txt: Node 1 has 3 DOF u,y,rotz all zero and the load applied to node 5 in the -y direction. More details on the exact formatting can be found within the Z88 manual.
4 Z88I2.TXT,produced by Ty
1 1 2 +0.00000E+000
1 2 2 +0.00000E+000
1 3 2 +0.00000E+000
5 2 1 -2.00000E+004



Copy the txt files to z88com directory and then launch z88com.

run the z88F
run the z88D nodal stress processor.
run the z88E nodal force processor.


run the z88P to plot the deflection.

text here
Figure 1 - Screen Shot of the Z88 plot program


The nodal results can be found in z88o4.txt file:
output file Z88O2.TXT : displacements, computed by Z88F V10
*************

Knoten U(1) U(2) U(3) U(4) U(5) U(6)

1 +0.0000000E+000 +0.0000000E+000 +0.0000000E+000
2 +0.0000000E+000 -8.5937586E-005 -6.5625066E-004
3 +0.0000000E+000 -3.1250031E-004 -1.1250011E-003
4 +0.0000000E+000 -6.3281313E-004 -1.4062514E-003
5 +0.0000000E+000 -1.0000010E-003 -1.5000015E-003

It's node 5 we're interested in and the displacement in the y direction is U(2) =1 mm.


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