2017
DOI: 10.1111/ffe.12671
|View full text |Cite
|
Sign up to set email alerts
|

Fatigue crack growth of multiple interacting cracks: Analytical models and experimental validation

Abstract: This article deals with the fatigue propagation of multiple cracks in finite width holed panels, which are typical of aircraft structural components. Theoretical studies in the literature have been considered and critically analyzed. Some of them have been translated into analytical models and implemented in a computer code. To check the effectiveness of the used models, a fatigue testing campaign has been conducted on six different configurations of notches and cracks. The comparison between experimental resu… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
4

Citation Types

0
3
0

Year Published

2018
2018
2024
2024

Publication Types

Select...
7
1

Relationship

0
8

Authors

Journals

citations
Cited by 8 publications
(4 citation statements)
references
References 35 publications
0
3
0
Order By: Relevance
“…In their study, fatigue testing campaigns were performed on six different settings of notches and cracks, which include several interacting cracks around the holes. By comparison of the experimental results with those from the implemented models, a good agreement can be obtained [9]. Xu et al investigated a linearly independent higher-order extending numerical manifold method and its application to multiple crack growth simulations.…”
Section: Introductionmentioning
confidence: 90%
“…In their study, fatigue testing campaigns were performed on six different settings of notches and cracks, which include several interacting cracks around the holes. By comparison of the experimental results with those from the implemented models, a good agreement can be obtained [9]. Xu et al investigated a linearly independent higher-order extending numerical manifold method and its application to multiple crack growth simulations.…”
Section: Introductionmentioning
confidence: 90%
“…Galatolo [7] critically analyzed the theoretical research in the literature, transformed it into analytical models, and conducted fatigue tests to validate these models. And use the model to develop the PISA code for simulating crack propagation in aerospace metal components.…”
Section: Introductionmentioning
confidence: 99%
“…The SIF is calculated with the newly revised formula [ 4 ]. For a variety of different porous multicrack structures, the composite method is used to evaluate SIF by superimposing a set of appropriate elementary solutions to consider different geometric boundaries [ 5 ]. The integral mean is used to quantify the SIF at the crack tip [ 6 ].…”
Section: Introductionmentioning
confidence: 99%