Wing Buckling Analysis
Wing Buckling Analysis is a structural engineering methodology that assesses the critical load conditions under which a wing's components lose stability through sudden deformation, distinguishing itself from general structural analyses by focusing specifically on elastic instability mechanisms in thin-walled aerospace structures.
32
Publications
746
Citations
79
Authors
32
Institutions
Publications per year
2017–2026
5
Parents
32
Structural optimization for joined-wing synthesis
John W. Gallman, Ilan M. Kroo · Journal of Aircraft · 1996 · 72 citations
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Virginia Tech
Blacksburg, United States
4 h-index
13 publications
253 citations

Riga Technical University
Riga, Latvia
2 h-index
5 publications
162 citations

University of Bath
Bath, United Kingdom
2 h-index
3 publications
48 citations

Ames Research Center
Mountain View, United States
2 h-index
3 publications
248 citations
University of Florida
Gainesville, United States
2 h-index
9 publications
194 citations

San Diego State University
San Diego, United States
2 h-index
5 publications
104 citations
Airbus (United Kingdom)
Bristol, United Kingdom
2 h-index
6 publications
186 citations
Stanford University
Stanford, United States
2 h-index
2 publications
160 citations
1–8 of 32
6 publications · 236 citations
6
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AST · 3 publications · 79 citations
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Repository · 2 publications · 30 citations
2
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1 publications · 27 citations
1
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1 publications · 13 citations
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