Failure Modes of a Reticulated Dome in a Small Airplane Crash

Figure 11

Deformation development of the dome in 2-B. (a) 0.3 s of the whole structure, (b) 0.3 s of the main members, (c) 0.6 s of the whole structure, (d) 0.6 s of the main members, (e) 1 s of the whole structure, (f) 1 s of the main members, (g) 2.6 s of the whole structure, and (h) 2.6 s of the main members.

(a)

(b)

(c)

(d)

(e)

(f)

(g)

(h)