SVR Prediction Algorithm for Crack Propagation of Aviation Aluminum Alloy

Table 7

Partial test data of constant amplitude three-hole test specimen.

	A	B	C	D	E	F
5000	0	0	0	0	0	0
28000	0	0	0	0	0	0
28500	0	0	0	0.1	0	0
29000	0	0	0	0.2	0	0
29500	0	0	0	0.3	0	0
…
64250	3.4	2	8	7.2	2.8	6.6
64500	3.7	2	8	7.2	2.8	7.5
64750	4	2	8	7.2	2.8	7.6
64973	6.2	2	8	7.2	2.8	10.2
64976	17.2	2	8	7.2	2.8	16.8