Residual Strength and Fatigue Lifetime of ... - Solid Mechanics
Residual Strength and Fatigue Lifetime of ... - Solid Mechanics
Residual Strength and Fatigue Lifetime of ... - Solid Mechanics
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H250 Specimen<br />
H100 Specimen<br />
H45 Specimen<br />
z<br />
y<br />
x<br />
50<br />
480<br />
Wood Wood insert<br />
insert Release Teflon film film<br />
Foam<br />
Foam<br />
core<br />
core<br />
Figure 5.2: Manufactured STT specimens <strong>and</strong> a drawing <strong>of</strong> STT specimens including<br />
dimensions (mm).<br />
At the centre <strong>of</strong> the specimens steel plates were glued to the top <strong>and</strong> bottom face sheets with<br />
epoxy. Using the steel plates the top <strong>and</strong> bottom faces were fixed to the actuator <strong>of</strong> the testing<br />
machine <strong>and</strong> the test rig respectively by four bolts. The test rig consists <strong>of</strong> welded steel pr<strong>of</strong>iles<br />
<strong>of</strong> a wall thickness <strong>of</strong> 6 mm, see Figure 5.3. The wood reinforced ends <strong>of</strong> the specimens were<br />
clamped to the test rig by square section steel pr<strong>of</strong>iles using four bolts. Furthermore, a 4 Mpix<br />
Digital Image Correlation (DIC) measurement system (ARAMIS 4M) as shown in Figure 5.4<br />
was used to monitor 2D surface strains to locate the crack tip continuously during the<br />
experiments. The crack tip can be located by the strain concentration at the loaded crack tip,<br />
which is visible in the DIC strain contours. Finally, a servo-hydraulic Instron actuator with a<br />
maximum capacity <strong>of</strong> 100kN was used to load the STT specimens. However, a smaller 25 kN<br />
load cell was mounted on the actuator to increase the accuracy <strong>of</strong> the load measurements, see<br />
Figure 5.5.<br />
92<br />
1000<br />
860<br />
(Width 65mm)