Wing Bending Loads
Wing Bending Loads is a structural engineering concept referring to the internal resistive forces and moments generated along the span of a wing that counteract the external aerodynamic and inertial loads causing flexural deformation about the wing’s lateral axis.
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1.2K
Citations
73
Authors
33
Institutions
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2017–2026
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University of Florida
Gainesville, United States
2 h-index
2 publications
140 citations

Armstrong Flight Research Center
Edwards, United States
2 h-index
3 publications
93 citations
Virginia Tech
Blacksburg, United States
2 h-index
14 publications
1.1K citations

University of Bristol
Bristol, United Kingdom
2 h-index
2 publications
67 citations
Politecnico di Torino
Turin, Italy
2 h-index
3 publications
83 citations

Nanjing University of Aeronautics and Astronautics
Nanjing, China
2 h-index
3 publications
45 citations
Technion – Israel Institute of Technology
Haifa, Israel
2 h-index
2 publications
37 citations

Shanghai Ocean University
Shanghai, China
1 h-index
7 publications
301 citations
1–8 of 33
5 publications · 192 citations
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Repository · 3 publications · 102 citations
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Repository · 2 publications · 355 citations
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1 publications · 26 citations
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1 publications · 15 citations
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