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

Table 3

Basic performance parameters of the test system.

Device	Type	Basic performance parameter
Air cannon	AC-050	50 mm caliber, launching ice balls with a maximum speed of 320 ms^−1
Dynamic force sensor	KD3005C	Maximum range 40 kN; Sampling frequency not less than 100 kHz
High-speed camera	V1212	>30,000 FPS at pixels
Data-acquisition system	DongHua	Sampling frequency 1 MHz