2016
DOI: 10.1016/j.tafmec.2016.01.009
|View full text |Cite
|
Sign up to set email alerts
|

Effective local stress intensity factor criterion for prediction of crack growth trajectory under mixed mode fracture conditions

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2
2
1

Citation Types

0
12
0

Year Published

2016
2016
2024
2024

Publication Types

Select...
7

Relationship

0
7

Authors

Journals

citations
Cited by 34 publications
(12 citation statements)
references
References 53 publications
0
12
0
Order By: Relevance
“…By employing the SIF results determined in Eqs and , the fatigue growth of a semi‐elliptical surface flaw in a plate is examined through a two‐parameter theoretical model based on the Paris' law. According to such a model, the crack semi‐axes a and b grow, after one cyclic loading, to a new configuration described by the following expression: x2b12+y2a12=1, where a 1 and b 1 are the semi‐axes of the surface flaw after one loading cycle (Fig.…”
Section: Numerical Calculation and Results Analysismentioning
confidence: 99%
See 2 more Smart Citations
“…By employing the SIF results determined in Eqs and , the fatigue growth of a semi‐elliptical surface flaw in a plate is examined through a two‐parameter theoretical model based on the Paris' law. According to such a model, the crack semi‐axes a and b grow, after one cyclic loading, to a new configuration described by the following expression: x2b12+y2a12=1, where a 1 and b 1 are the semi‐axes of the surface flaw after one loading cycle (Fig.…”
Section: Numerical Calculation and Results Analysismentioning
confidence: 99%
“…Because both modes I and II occur during fatigue crack propagation, the Paris' law must take into account an equivalent SIF, which can be obtained from energetic considerations: Keff(),,ξζ=KI2(),,ξζ+2KII2(),,ξζ, where K I (∂, ξ , ζ ) is evaluated by the Eq. discussed above, and K II (∂, ξ , ζ ) is computed through Eq.…”
Section: Numerical Calculation and Results Analysismentioning
confidence: 99%
See 1 more Smart Citation
“…Many proposed elemental life assessment models neither needs additional material properties nor pre‐existing cracks for defining fatigue damage mechanism in MD laminates. However, non‐destructive assessment of residual life using experimental data still possesses a substantial challenge for researchers . The combined use of experimental residual stiffness, energy dissipation, and matrix crack density computation approach as explained in this paper provides a comparative life monitoring approach for any stacking sequence.…”
Section: Introductionmentioning
confidence: 99%
“…However, non-destructive assessment of residual life using experimental data still possesses a substantial challenge for researchers. [56][57][58][59] The combined use of experimental residual stiffness, energy dissipation, and matrix crack density computation approach as explained in this paper provides a comparative life monitoring approach for any stacking sequence. Here, the computation of normalised stiffness and energy parameter requires load-displacement data whereas the evaluation of matrix crack density needs optical image processing.…”
Section: Introductionmentioning
confidence: 99%