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LICENTIATE THESIS - Luleå tekniska universitet

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Tensile strength [MPa]<br />

5<br />

4<br />

3<br />

2<br />

1<br />

0<br />

0 2 4 6 8<br />

Strain [‰]<br />

- 9 -<br />

Normailzed stress<br />

1<br />

0.8<br />

0.6<br />

0.4<br />

0.2<br />

0<br />

0 2 4 6 8<br />

Strain [‰]<br />

(a) (b)<br />

Figure 8 Results of the uniaxial tensile tests for series B. (a) Curves showing the<br />

strains of the COD-gauges that were exposed to the highest strain during each<br />

test. (b) The same curves as in (a) but with normalized stress in order to get a<br />

mean curve for the whole test series. The curve that has (+) is the mean curve<br />

used in Figure 10.<br />

Fatigue test<br />

In Figure 9 to Figure 13 some typical results from the fatigue tests are presented.<br />

In Figure 9 the tensile stress versus the strain is displayed for specimen B9. The<br />

specimen failed after 350 load cycles. In Figure 9 the plotted curve is the COD-gauge<br />

that was exposed to the highest strain.<br />

Tensile strength [MPa]<br />

4<br />

3<br />

2<br />

1<br />

0<br />

Load level A: 2.63 MPa<br />

load level B: 3.93 MPa<br />

0 0.2 0.4 0.6 0.8 1<br />

Strain [‰]<br />

Figure 9 Curve showing the tensile strength versus the strain development fro<br />

specimen B9. The specimen failed after 350 load cycles. The two load levels<br />

corresponds to 94% respectively 64% of the average peak load for the uniaxial<br />

tensile tests for the series.<br />

In Figure 10 the total strain versus the number of load cycles is displayed for specimen<br />

B9. In the figure this curve is compared to the average normalized stress-strain curve<br />

for series B.

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