2019
DOI: 10.1016/j.engfailanal.2019.03.029
|View full text |Cite
|
Sign up to set email alerts
|

Effect of laser beam welded reinforcement on integral skin panel fatigue life

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
3
1
1

Citation Types

0
15
0

Year Published

2019
2019
2023
2023

Publication Types

Select...
6
3

Relationship

1
8

Authors

Journals

citations
Cited by 28 publications
(15 citation statements)
references
References 6 publications
0
15
0
Order By: Relevance
“…Numerical simulation of panels by using xFEM has been presented in more details in [8,9,33], whereas here only the most important results and findings will be shown for AA6156 T6 and crack length 2a = 14 mm. To start with, Fig.…”
Section: Numerical Simulation Of Fatigue Crack Growthmentioning
confidence: 99%
See 1 more Smart Citation
“…Numerical simulation of panels by using xFEM has been presented in more details in [8,9,33], whereas here only the most important results and findings will be shown for AA6156 T6 and crack length 2a = 14 mm. To start with, Fig.…”
Section: Numerical Simulation Of Fatigue Crack Growthmentioning
confidence: 99%
“…Extensive experimental study has been performed in GKSS, [5], using different panels, Fig. 3, followed by recent numerical simulation using xFEM, [3,[6][7][8][9]. Two different ways of improving panel performance were analysed, focused on the effect of stringers only and stringers and clips together, [6][7][8][9].…”
Section: Introductionmentioning
confidence: 99%
“…12, about a decade ago, as the world's largest passenger airliner, representing one of the finest achievements in the history of structural integrity. It was a long way to success, followed by occasional failures and extensive testing, [42][43][44][45][46][47][48][49]. Driving force was economy, but in this case, contrary to bridges that still need to be longer and longer, economy actually stopped further progress and even starts to jeopardize the existing achievement.…”
Section: Aeronautical Engineeringmentioning
confidence: 99%
“…Laser welding has been able to achieve the joining of many types of materials, and has many unmatched advantages of fusion welding processes [15][16][17]. For example, laser welding is used to weld aircraft skin and stringers [18,19]. Compared with riveted structure, the weight and cost of airplane is reduced dramatically.…”
Section: Introductionmentioning
confidence: 99%