Development of a Component Head Injury Criteria (HIC ... - FAA
Development of a Component Head Injury Criteria (HIC ... - FAA
Development of a Component Head Injury Criteria (HIC ... - FAA
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Figure 48. Simulation Sequence <strong>of</strong> Foam Deformation and its Relative Motion With Rigid<br />
Surface for NHCT Test H03316<br />
Figure 49 shows a comparison <strong>of</strong> the resulting head acceleration pr<strong>of</strong>ile <strong>of</strong> the NHCT and the<br />
corresponding MADYMO model, which are similar. The resulting output parameters are<br />
tabulated in table 13. A very significant correlation <strong>of</strong> the outputs and hence conformation <strong>of</strong> a<br />
high-fidelity model can be noted. A similar validation sequence for this model was carried out in<br />
section 6.1 for NHCT test 01057-82.<br />
80<br />
70<br />
H03316-43DEG<br />
MADYMO-43DEG<br />
60<br />
Acc('g')<br />
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40<br />
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10<br />
0<br />
-100 -50 0 50 100 150 200<br />
Time (msec)<br />
Figure 49. <strong>Head</strong> Acceleration Pr<strong>of</strong>ile for Actual Test and Simulation<br />
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