scispace - formally typeset
Journal ArticleDOI

Growth rate models for short surface cracks in AI 2219-T851

TLDR
In this article, the authors measured the fatigue propagation of short Mode I surface cracks in Al 2219-T851 and compared the measured rates with values predicted from crack growth models, with an underlying assumption that slip responsible for early propagation does not extend in significant amounts beyond the next grain boundary.
Abstract
Rates of fatigue propagation of short Mode I surface cracks in Al 2219-T851 are measured as a function of crack length and of the location of the surface crack tips relative to the grain boundaries. The measured rates are then compared to values predicted from crack growth models. The crack growth rate is modeled with an underlying assumption that slip responsible for early propagation does not extend in significant amounts beyond the next grain boundary in the direction of crack propagation. Two models that contain this assumption are combined: 1) cessation of propagation into a new grain until a mature plastic zone is developed; 2) retardation of propagation by crack closure stress, with closure stress calculated from the location of a crack tip relative to the grain boundary. The transition from short to long crack growth behavior is also discussed.

read more

Citations
More filters
Journal ArticleDOI

Propagation of short fatigue cracks

TL;DR: In this paper, the authors examined the micro-structural properties of short fatigue cracks in terms of fracture mechanics, microstructure, and environment, and compared their propagation behavior with those of long cracks.
Journal ArticleDOI

A geometric model for fatigue crack closure induced by fracture surface roughness

TL;DR: In this article, a geometric model is presented for crack closure induced by fracture surface roughness, specifically addressing the contribution from both Mode I and Mode II crack tip displacements in addition to considering the nature of the fracture surface morphology.
Journal ArticleDOI

Crack deflection: Implications for the growth of long and short fatigue cracks

TL;DR: In this paper, a simple elastic deflection model is developed to estimate the growth rates of nonlinear fatigue cracks subjected to various degrees of deflection, by incorporating changes in the effective driving force and in the apparent propagation rates.
Journal ArticleDOI

Modelling of small fatigue crack growth interacting with grain boundary

TL;DR: In this paper, the slip band at the tip of a small fatigue crack interacting with grain boundaries is modelled for four cases: a slip band not reaching the grain boundary, a slip-band blocked by the boundary, slip band propagated into an adjacent grain, and then blocked by a second grain boundary.
Journal ArticleDOI

The effect of solidification rate on the growth of small fatigue cracks in a cast 319-type aluminum alloy

TL;DR: In this paper, the authors investigated the effect of solidification rate on the growth behavior of small fatigue cracks in a 319-type aluminum alloy, a common Al-Si-Cu alloy used in automotive castings.
References
More filters
Journal ArticleDOI

Prediction of non propagating cracks

TL;DR: In this paper, an explanation for non propagating fatigue cracks is presented based on the criterion that once the value of a particular strain intensity factor reduces to the threshold value for the material the crack should stop.
Journal ArticleDOI

Fatigue Crack Propagation of Short Cracks

TL;DR: In this article, the average growth rate for very short cracks considerably exceed those given by conventional stress intensity-crack growth laws fitted to long crack data, by introducing an effective crack length U into the solutions for intensity factors and the J integral method of analysis, and therefore the value of k can be obtained once the threshold stress intensity factor and the fatigue limit are known.
Journal ArticleDOI

Initiation of fatigue cracks in commercial aluminium alloys and the subsequent propagation of very short cracks

TL;DR: In this paper, the authors observed the initiation of fatigue cracks at a plane polished surface and the subsequent growth of very short cracks [0.006 mm (0.00025 in.)-0.5 mm(0.02 in.) deep].
Journal ArticleDOI

A Relation between the Critical Alternating Propagation Stress and Crack Length for Mild Steel

N. E. Frost
TL;DR: In this paper, it was found that the relation between this critical alternating stress σ and the crack length l was given by σ3l = constant, and by means of this relation it was possible to correlate a wide variety of hitherto unrelated notch fatigue data.
Related Papers (5)