Research Article
Failure Modes of a Reticulated Dome in a Small Airplane Crash
Figure 9
Deformation development of the dome in 2-A. (a) 0.03 s of the whole structure, (b) 0.03 s of the main members, (c) 0.15 s of the whole structure, (d) 0.15 s of the main members, (e) 0.6 s of the whole structure, (f) 0.6 s of the main members, (g) 1.5 s of the whole structure, and (h) 1.5 s of the main members.
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