Experimental Modal Analysis
Sample preparation
For both the cases, delaminations have been introduced in two different layers of the 4-ply laminates. The laminates with delaminations in the middle layer (i.e. II interface) are designated as Type A and those with delamination in the offset layer (i.e. I interface as shown in Figure 37.2) are designated as Type B. The experiments are conducted on these composite plates in fixed-free boundary condition (more precisely C-F-F-F). Dynamic excitation is given at the center of the plate by an electro-dynamic shaker. Laminated composite plates used in experimental modal analysis are detailed in Table 37.2.
Table 37.2 Laminated composite plates used in experimental modal analysis
S.No. |
Ply configuration |
Type |
1 |
[0/0/0/0] |
Healthy |
Delam Type-I A & B |
Delam Type-II A & B |
2 |
[90/90/90/90] |
Healthy |
Delam Type-I A & B |
Delam Type-II A & B |
3 |
[0/90/0/90] |
Healthy |
Delam Type-I A & B |
The experiments are carried out on Polytec Scanning (PSV) Vibrometer in 3-D scan mode. The excitation details are provided in Table 37.3
Table 37.3 Detalis of the excitation signal used in 3-D scan mode
Excitation signal |
pseudo-random |
Frequency Range |
0-2000 Hz |
FFT lines |
1600 |
Window |
Rectangle |
Averages |
10 (complex) |
Velocity Decoder |
VD-08 Digital decoder
(velocity range 0-10 mm/s) |
|