Established Numerical Techniques for the Structural Analysis of a Regional Aircraft Landing Gear

Figure 28

Numerical frames of the drop test simulation: (a) t1 = 0 ms; (b) t2 = 50 ms; (c) t3 = 80 ms; (d) t4 = 120 ms; (e) t5 = 170 ms; (f) t6 = 210 ms; (g) t7 = 340 ms; (h) t8 = 350 ms.

(a)

(b)

(c)

(d)

(e)

(f)

(g)

(h)