Wing Damage Tolerance is a structural engineering concept that denotes the inherent capability of a wing structure to sustain specified levels of damage, such as cracks, corrosion, or impact-induced defects, without catastrophic failure, thereby maintaining acceptable load-carrying capacity and structural integrity throughout its operational life under expected loading conditions.
8
Publications
166
Citations
18
Authors
13
Institutions
Publications per year
2017–2026
1
Parents
Publications
8
1–5 of 8
Authors
18
- AA
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1–5 of 18
Institutions
13
Langley Research Center
Hampton, United States
2 h-index
2 publications
24 citations
Defence Science and Technology Group
Canberra, Australia
1 h-index
1 publications
21 citations
Monash University
Melbourne, Australia
1 h-index
2 publications
42 citations
Bell Helicopter Textron (Canada)
Mirabel, Canada
1 h-index
3 publications
66 citations
University of Oklahoma
Norman, United States
1 h-index
2 publications
52 citations
Lockheed Martin (United States)
Bethesda, United States
1 h-index
1 publications
26 citations
Illinois Institute of Technology
Chicago, United States
1 h-index
1 publications
10 citations
James S. McDonnell Foundation
St Louis, United States
1 h-index
1 publications
18 citations
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Venues
- Aircraft Systems and Technology Meeting
1 publications · 18 citations
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- AIAA Journal
1 publications · 32 citations
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- Structural and Multidisciplinary Optimization
1 publications · 26 citations
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- Journal of Aircraft
1 publications · 10 citations
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- International Journal of Fatigue
1 publications · 21 citations
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