Theoretical estimation of fatigue limit of notches under axial push-pull loading was made with an emphasis on the formation of non-propagating crack. A critical notch radius and a critical stress concentration factor were determined so as to distinguish notch fatigue limits with crack initiation and
Prediction of non propagating cracks
โ Scribed by M.H. El Haddad; T.H. Topper; K.N. Smith
- Publisher
- Elsevier Science
- Year
- 1979
- Tongue
- English
- Weight
- 943 KB
- Volume
- 11
- Category
- Article
- ISSN
- 0013-7944
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โฆ Synopsis
Ah&act-An explanation for non propagating fatigue cracks is presented based on the criterion that once the value of a particular strain intensity factor reduces lo the threshold value for the material the crack should stop. Predicted lengths of these cracks based on solutions for the intensity factor are in good agreement with the experimental data Intensity factor trends for cracks in notches pn shown to vary from an initial decrease to a minimum value followed by an increase and eventual convergence with the trend for the equivalent long crack for sharp notches to the blunt notch curves that continuously increased during their approach to the long crack trend. The type of trend exhibited by a given notch depends both on notch geometry and notch size. In blunt notches the maximum value of the threshold stress for crack propagation is at initiation. However, for sharp notches the peak value of the threshold stress vs crack length curves shifts to a finite length. Stresses above the initiation level but below this peak stress kvel result in fatigue cracks which start but do not propagate to failure. Predicted values of the fatigue limit stresses for a variety of sizes in a circular and an elliptical notch are in good agreement with experimental results.
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