Civil Engineering Reference
In-Depth Information
Figure 7.6 Stress (von Mises) contours at failure of composite girder G1 (enlarged 10
times).
2000
1800
1600
1400
1200
1000
800
600
400
Test
FE
200
0
0
20
40
60
80
100
120
Midspan deflection (mm)
Figure 7.7 Load-midspan deflection of composite girder G1 obtained experimentally
and numerically.
Figure 7.7 . It can be shown that generally good agreement was achieved
between experimental and numerical relationships. The ultimate failure load
observed in the test [ 7.29 ] was 1743.7 kN at a deflection of 95.6 mm, while
the ultimate failure load predicted from the finite element analysis was
1765.5 kN at a deflection of 97.7 mm. The finite element failure load
was 1.3% higher than that observed in the test.
 
 
 
 
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