cross section crash boxes
cross section crash boxes
cross section crash boxes
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Figure 3.23. Experiment and coupled FEM/SPH simulation of the deformed<br />
shapes of bitubular polystyrene foam filling arrangements, filling<br />
only between two tubes (BPH) and filling the inner hole with<br />
polystyrene foam (BPE).. ........................................................................... 58<br />
Figure 3.24. Deformation modes of empty and foam filled monotubal and<br />
bitubal square <strong>section</strong>s. .............................................................................. 59<br />
Figure 3.25. The variation of SEA values of steel conical tubes with wall<br />
thickness at three different semi apical angle (θ) and with three<br />
different foam filler density. ....................................................................... 59<br />
Figure 3.26. The simulated collapse modes of (a) hollow ,(b) foam-filled (0.103<br />
g cm -3 ), (c) 2x2 multi-cell, (d) foam-filled hollow (0.206 g cm -3 )<br />
(left: cut-open view right: general view) and (e) 3x3 multi-cell<br />
column (left: front view right: general view). ............................................ 60<br />
Figure 3.27. SEA values of empty and foam filled single, double and triplecell<br />
square Al <strong>section</strong>s ...................................................................................... 61<br />
Figure 3.28. The variation of the energy-absorbing effectiveness factor of<br />
6060T4 Al circular tube with Al foam filler density: o: t=1.40-1.42<br />
mm, : t=1.97-2.01 mm, : t=2.35-2.46 mm ............................................ 62<br />
Figure 3.29. a) Aluminum foam filled single and double hat <strong>section</strong>s with<br />
various filler lengths and b) the variation of SEA values with foam<br />
filler length. ................................................................................................ 62<br />
Figure 4.1. As-received Alulight Al foam panels. ........................................................ 66<br />
Figure 4.2. a) Aluminum foam panel cutting and b) the removed dense <strong>section</strong>s........ 66<br />
Figure 4.3. Pictures of a) foam compression test samples and b) foam sample<br />
between compression test platens. ............................................................. 67<br />
Figure 4.4. Crash box structure and <strong>crash</strong> zone. ........................................................... 68<br />
Figure 4.5. The processing stages of the tested <strong>crash</strong> <strong>boxes</strong>. ....................................... 68<br />
Figure 4.6. Technical drawings of the tested <strong>crash</strong> <strong>boxes</strong>. ........................................... 70<br />
Figure 4.7. The method of trigger mechanism formation on the outer surfaces<br />
of the <strong>boxes</strong>. ............................................................................................... 71<br />
Figure 4.8. a) Experimental <strong>crash</strong> box specimens with and without montage<br />
plate and b) <strong>cross</strong> <strong>section</strong> view of the <strong>boxes</strong> of three different wall<br />
thicknesses. ................................................................................................. 71<br />
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