2022
DOI: 10.1016/j.ijfatigue.2022.107162
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The effects of welded clips on fatigue crack growth in AA6156 T6 panels

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Cited by 8 publications
(8 citation statements)
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“…Here, we focus on some new results in numerical analyses of FCG in integral skin‐stringer panel produced by means of laser beam welding (LBW). Except for the good agreement of numerical and experimental results, one should notice significant effect of Paris law coefficient on remaining life, 112 and the fact that the fatigue life obtained on the basis of calculated SIFs along the crack fronts on LBW skin‐stringer panels was significantly longer than experimentally measured life 111 …”
Section: Case Study 5: Aircraft Componentsmentioning
confidence: 77%
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“…Here, we focus on some new results in numerical analyses of FCG in integral skin‐stringer panel produced by means of laser beam welding (LBW). Except for the good agreement of numerical and experimental results, one should notice significant effect of Paris law coefficient on remaining life, 112 and the fact that the fatigue life obtained on the basis of calculated SIFs along the crack fronts on LBW skin‐stringer panels was significantly longer than experimentally measured life 111 …”
Section: Case Study 5: Aircraft Componentsmentioning
confidence: 77%
“…This approach was presented in literature, 90 where XFEM results for FCG in the case of the base panel (without stringers and welded clips) were verified by experimental measurements. Afterward, two additional issues were covered, the effect of mesh size (1, 2 and 4 mm), as described in literature, 110,111 and the effect of clips on fatigue life. 112,113 Here, we focus on some new results in numerical analyses of FCG in integral skin-stringer panel produced by means of laser beam welding (LBW).…”
Section: Case Study 5a: Optimization Of Wing Sparmentioning
confidence: 99%
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