Aircraft Wing Optimization
Aircraft Wing Optimization is a computational engineering methodology that systematically enhances wing design parameters to achieve optimal aerodynamic, structural, and aeroelastic performance under defined operational constraints.
130
Publications
4.6K
Citations
333
Authors
124
Institutions
Publications per year
2017–2026
45
Parents
130
1–5 of 130
333
8
h-index
Langley Research Center, United States
5 publications · 536 citations
5
h-index
5
h-index
4
h-index
4
h-index
1–5 of 333
124

Langley Research Center
Hampton, United States
9 h-index
14 publications
1.7K citations
University of Michigan
Ann Arbor, United States
9 h-index
15 publications
626 citations
Virginia Tech
Blacksburg, United States
6 h-index
22 publications
576 citations
Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR)
Cologne, Germany
5 h-index
7 publications
159 citations

University of Bristol
Bristol, United Kingdom
5 h-index
15 publications
444 citations
Office National d'Études et de Recherches Aérospatiales
Palaiseau, France
4 h-index
19 publications
796 citations

Delft University of Technology
Delft, The Netherlands
4 h-index
6 publications
126 citations
Stanford University
Stanford, United States
4 h-index
6 publications
185 citations
1–8 of 124
11 publications · 352 citations
11
h-index
AST · 12 publications · 767 citations
11
h-index
10 publications · 489 citations
10
h-index
7 publications · 453 citations
7
h-index
3 publications · 86 citations
3
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1–5