Wing Structural Bending is a mechanical deformation phenomenon in aerospace engineering wherein a wing structure experiences axial displacement due to aerodynamic and inertial loads acting perpendicular to its longitudinal axis, distinguished from other forms of structural deformation by its primary mode of flexural response in flight conditions.
14
Publications
456
Citations
36
Authors
13
Institutions
Publications per year
2017–2026
2
Parents
Publications
14
1–5 of 14
Authors
36
- FH
2
h-index
- RT
2
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- ES
2
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- RK
2
h-index
- SA
1
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1–5 of 36
Institutions
13
University of Florida
Gainesville, United States
2 h-index
2 publications
104 citations
Virginia Tech
Blacksburg, United States
2 h-index
9 publications
472 citations
Tohoku University
Sendai, Japan
1 h-index
1 publications
33 citations
Universidade de São Paulo
São Paulo, Brazil
1 h-index
4 publications
72 citations
University of Calgary
Calgary, Canada
1 h-index
1 publications
10 citations
Integrity Systems (United States)
Leesburg, United States
1 h-index
1 publications
22 citations
Italian Aerospace Research Centre
Capua, Italy
1 h-index
3 publications
51 citations
Northrop Grumman (Germany)
Freiburg, Germany
1 h-index
2 publications
62 citations
1–8 of 13
Venues
- Journal of Aircraft
5 publications · 143 citations
5
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- International Journal of Engineering and Advanced Technology
1 publications · 19 citations
1
h-index
- Journal of Experimental Biology
1 publications · 129 citations
1
h-index
- Journal of the Brazilian Society of Mechanical Sciences and Engineering
1 publications · 18 citations
1
h-index
- 46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
Conference · 1 publications · 31 citations
1
h-index
1–5