Research Article

Online Structural Health Monitoring of Rotating Machinery via Ultrasonic Guided Waves

Table 1

Relative amplitudes of L(0,4) and L(0,6) without and with crack when the rotor is at rest.

ā€‰Without crackWith crack

ā€‰L(0,4)L(0,6)L(0,4)L(0,6)
10.2070.4020.2180.438
20.2120.4330.1740.372
30.1950.4780.2190.531
40.2340.4390.2050.369