The dynamic stress intensity factor histories for a half plane crack in an otherwise unbounded elastic body are analyzed. The crack is subjected to a traction distribution consisting of two pairs of suddenly-applied shear point loads, at a distance L away from the crack tip. The exact expression for
A semi-infinite-crack model for determining mode I stress intensity factors using crack surface displacements
โ Scribed by S. W. Ng; K. J. Lau
- Publisher
- Springer Netherlands
- Year
- 1996
- Tongue
- English
- Weight
- 739 KB
- Volume
- 76
- Category
- Article
- ISSN
- 1573-2673
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โฆ Synopsis
A semi-infinite-crack model is used to supplement the conic section simulation method for determining stress intensity factors of finite cracked bodies under mode I loadings. The actual displaced crack surface profile is found by finite element analysis. For each crack surface segment between two neighbouring nodes, a set of model parameters is found by using the displacements of these two nodes. A stress intensity factor estimate is then calculated from the closed-form formula associated with the model. It is found that near-tip crack surface displacements produce model parameters that are sufficient for quantifying the stress intensity factor. The semiinfinite-crack model can be used either as a stand alone model or in conjunction with the ellipse simulation procedure to form a systematic approach. It is shown that this model can be applied to different geometries and loadings with excellent accuracy.
๐ SIMILAR VOLUMES
The stress-intensity factors for a semi-infinite plane crack with a wavy front are determined when the crack faces are subjected to normal and shearing tractions. The results are derived using asymptotic methods and are valid to O(e 2) where E = A/X ~ 1; A is the amplitude and ~ is the wavelength of