Figure 6
From: Safety Assessment of Aircraft Fuel Tank Access Cover under the Impact Load by Tire Fragments
Comparisons of simulation and experimental results: (a) impact angle = 30°, velocity = 135 m/s (SG1-2), (b) impact angle = 30°, velocity = 135 m/s (SG3-4), (c) impact angle = 90°, velocity = 100 m/s (SG1-2) and (d) impact angle = 90°, velocity = 100 m/s (SG3-4)