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.

(a)

(b)

(c)

(d)

(e)

(f)

(g)

(h)