Table 3.
Reference | DI Time-Based | DI Frequency-Based | Remark |
---|---|---|---|
[99] | Coefficient of CWT, Z = Where A = Fraction of the total energy of the CWT that lies at the centred frequency B = Fraction of the total energy of the CWT that lies at the higher frequency C = Fraction of the total energy of the CWT that lies at the lower frequency |
Thickness reduction in a thin plate | |
[58] | Peak amplitude coefficient, Where A1 = amplitude of the fundamental wave and A2 = amplitude of the second harmonic |
Fatigue crack propagation in aluminium pipe | |
[27] | The beat wavelength, KA0 and Ks0 are the wavenumbers of the fundamental symmetric and antisymmetric |
Monitored thickness reduction due to general corrosion activity | |
[90] |
Awel = Peak amplitude at the weld Awel = Peak amplitude from a direct source |
The severity of damage in the fluid-filled pipe | |
[101] |
fd = the spectral signal frequency response at damage state fbL = the spectral signal frequency response at the undamaged state |
Corrosion severity detection in pipeline | |
[59] |
for i,j = 1~6 where: DIij(fex) = Damage signal differential = Baseline signal when pairing the i-th PZT actuator and the j-th PZT sensor at a given excitation frequency (fex). = damage signals when the corrosion damage was present at the targeted position of the plate. |
Corrosion detection and severity in the plate Aluminium | |
[61] | Spectral density, Where|| = spectral magnitude of the fundamental frequency || = Spectral magnitude of the second harmonic frequency |
Microscale crack detection in a plate structure |