Fuselage Damage Tolerance
Fuselage Damage Tolerance is a structural engineering concept that denotes the inherent capability of a fuselage to sustain specified levels of damage, such as cracks or impact-induced defects, without catastrophic failure and within acceptable safety limits throughout its operational life.
19
Publications
547
Citations
75
Authors
21
Institutions
Publications per year
2017–2026
2
Parents
19
1–5 of 19
75
3
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Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR), Germany
1 publications · 19 citations
1
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1
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1
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1
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1–5 of 75
21

Langley Research Center
Hampton, United States
3 h-index
4 publications
64 citations
Lockheed Martin (United States)
Bethesda, United States
2 h-index
2 publications
37 citations
Office National d'Études et de Recherches Aérospatiales
Palaiseau, France
1 h-index
2 publications
240 citations
Fraunhofer Institute for Manufacturing Technology and Advanced Materials
Bremen, Germany
1 h-index
2 publications
38 citations
Sikorsky Aircraft Corporation (United States)
Huntsville, United States
1 h-index
1 publications
17 citations
Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR)
Cologne, Germany
1 h-index
11 publications
209 citations
Airbus (Germany)
Hamburg, Germany
1 h-index
1 publications
19 citations

Commonwealth Scientific and Industrial Research Organisation
Canberra, Australia
1 h-index
2 publications
240 citations
1–8 of 21
Repository · 4 publications · 88 citations
4
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2 publications · 47 citations
2
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1 publications · 19 citations
1
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Repository · 1 publications · 28 citations
1
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MSF · Book series · 1 publications · 33 citations
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