Module 5: Experimental Modal Analysis for SHM
  Lecture 37: Velocity and displacement measurement
 

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)