Numerical and Experimental Verification of Spherically Layered Ice Model for Analysis on Hail Impacting Aviation Structures

Figure 13

Impact test and measurement system: (1) compressed air chamber, (2) launch valve, (3) quick-load device, (4) barrier, (5) sabot separator, (6) automatic injection control system, (7) computer, (8) high-speed data-acquisition system, (9) light, and (10) high-speed camera.