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Periods of Fatigue-Crack Propagation

It is important to stress that there is an initial time of fatigue when only a surface crack is initiated but the crack embryo cannot yet grow. It is preferable to term this time as an incubation period of fatigue. [Pg.267]

It is appropriate to divide the total number of cycles to the fatigue fracture Nf into three terms  [Pg.267]

The higher the amplitude of alternating stress the smaller the critical crack size. At large Njncub Ngj. With this condition the initiation of a crack is a very [Pg.267]

We have derived [83] the equation for the length of the fatigue-crack embryo. [Pg.267]

E - the curve of fracture for the Ti + 6AI + 4V alloy, test data [87] D - calculated values of T incub for the same alloy. [Pg.268]


See other pages where Periods of Fatigue-Crack Propagation is mentioned: [Pg.267]    [Pg.267]    [Pg.267]    [Pg.269]   


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