Fuselage Fatigue
Fuselage Fatigue is a structural degradation phenomenon characterized by the progressive development of microcracks and material failure in the fuselage of an aircraft under repeated cyclic loading, distinguishing it from static failure modes by its time-dependent accumulation of damage.
23
Publications
762
Citations
54
Authors
22
Institutions
Publications per year
2017–2026
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Civil Aviation University of China
Tianjin, China
3 h-index
14 publications
206 citations
Georgia Institute of Technology
Atlanta, United States
2 h-index
5 publications
151 citations
Technion – Israel Institute of Technology
Haifa, Israel
2 h-index
2 publications
38 citations
AGH University of Krakow
Krakow, Poland
1 h-index
4 publications
360 citations

University of Electronic Science and Technology of China
Chengdu, China
1 h-index
1 publications
16 citations
National Research Council Canada
Ottawa, Canada
1 h-index
3 publications
96 citations
Universidade de Brasília
Brasília, Brazil
1 h-index
3 publications
63 citations

Lawrence Livermore National Laboratory
Livermore, United States
1 h-index
1 publications
24 citations
1–8 of 22
10 publications · 441 citations
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Repository · 2 publications · 55 citations
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IJDM · 1 publications · 14 citations
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1 publications · 31 citations
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1 publications · 15 citations
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