Since its inception, acoustic emission has held great promise as a too
l for detection and evaluation of damage in structures. Of particular
concern is the occurrence of fatigue manifested by the processes of cr
ack initiation followed by crack growth to failure. Early research rel
ated acoustic emission parameters to physical variables, including loa
d, stress, pressure etc. causing damage. In this paper, relationships
relating acoustic emission to fatigue crack growth are developed. Acou
stic emission equations, similar to Paris' law, are derived which allo
w determination of the stress intensity factor and the crack growth ra
te. These principles are embodied in a second-generation system which
automatically and continuously determines these parameters. The approa
ch is applied in the laboratory as well as to structures including bri
dges, air frames and transmission towers for electrical power.