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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)

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