Wing Divergence Analysis is a computational aeroelastic method that identifies the critical flight conditions at which a wing structure becomes dynamically unstable due to the coupling of aerodynamic forces and elastic deformation, distinguishing itself from related analyses by focusing specifically on the onset of divergence instability in lifting surfaces.
14
Publications
824
Citations
27
Authors
10
Institutions
Publications per year
2017–2026
1
Parents
Publications
14
1–5 of 14
Authors
27
- LL
2
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- TA
2
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- LP
1
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- RH
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1–5 of 27
Institutions
10
Virginia Tech
Blacksburg, United States
5 h-index
8 publications
663 citations
Langley Research Center
Hampton, United States
3 h-index
7 publications
149 citations
University College London
London, United Kingdom
1 h-index
2 publications
358 citations
Massachusetts Institute of Technology
Cambridge, United States
1 h-index
2 publications
230 citations
Stanford University
Stanford, United States
1 h-index
1 publications
20 citations
Northwestern Polytechnical University
Xi'an, China
1 h-index
2 publications
44 citations
Tel Aviv University
Tel Aviv, Israel
1 h-index
1 publications
49 citations
Technion – Israel Institute of Technology
Haifa, Israel
1 h-index
1 publications
40 citations
1–8 of 10
Venues
- Journal of Aircraft
6 publications · 375 citations
6
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- AIAA Journal
2 publications · 165 citations
2
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- Journal of the aeronautical sciences. [REQUEST TITLE]
1 publications · 20 citations
1
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- NASA Technical Reports Server (NASA)
Repository · 1 publications · 17 citations
1
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- University of North Texas Digital Library (University of North Texas)
Repository · 1 publications · 35 citations
1
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