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The crack length estimated during the non-destructive inspection is affected by sizing errors, i.e. the measured crack size is different from its true size.
FEA results show small frequency value for lower crack size.
The crack size is then computed using the standard relation between stiffness and crack size.
The crack size is computed using a standard relation between stiffness and crack size.
The magnitude of the jump depends on the crack size.
First 6 natural frequency and mode shapes were obtained for varying crack size.
The critical crack size can be achieved reasonably by repeating from (1) to (4).
A margin of 2 on crack size was chosen in establishing maximum allowable crack sizes.
Crack size effects were readily explained with a simple short crack model.
In our second analysis, crack size information was added and a similar model was fit.
The influences of initial crack size and outside diameter on the fatigue life were also investigated.
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